{"id":1399,"date":"2023-09-29T17:48:43","date_gmt":"2023-09-29T09:48:43","guid":{"rendered":"https:\/\/cathayvista.top\/?p=1399"},"modified":"2024-12-09T10:21:21","modified_gmt":"2024-12-09T02:21:21","slug":"turbofan-zhen","status":"publish","type":"post","link":"https:\/\/cathayvista.top\/index.php\/2023\/09\/29\/turbofan-zhen\/","title":{"rendered":"\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a \/ Turbofan &#8211; \uff08\u5168\u6587\uff09\u4e2d\u82f1\u6587\u8bcd\u6761\u878d\u5408"},"content":{"rendered":"\n<blockquote class=\"wp-block-quote is-layout-flow wp-block-quote-is-layout-flow\">\n<p class=\"has-small-font-size\">\u4e2d\u6587\u8bcd\u6761\u539f\u6587\u94fe\u63a5\uff08\u65e0\u6cd5\u4ece\u4e2d\u56fd\u5185\u5730\u8bbf\u95ee\uff09\uff1a<a href=\"https:\/\/zh.wikipedia.org\/wiki\/%E6%B8%A6%E8%BC%AA%E6%89%87%E7%99%BC%E5%8B%95%E6%A9%9F\" target=\"_blank\" rel=\"noreferrer noopener\">\u70b9\u51fb\u8fd9\u91cc\u8bbf\u95ee<\/a>\u3002 <br>\u82f1\u6587\u8bcd\u6761\u539f\u6587\u94fe\u63a5\uff08\u65e0\u6cd5\u4ece\u4e2d\u56fd\u5185\u5730\u8bbf\u95ee\uff09\uff1a<a href=\"https:\/\/en.wikipedia.org\/wiki\/Turbofan\" target=\"_blank\" rel=\"noreferrer noopener\">\u70b9\u51fb\u8fd9\u91cc\u8bbf\u95ee<\/a>\u3002<\/p>\n\n\n\n<p class=\"has-small-font-size\">\u672c\u6587\u57fa\u4e8e\u82f1\u6587\u8bcd\u6761\u7684\u7ebf\u7d22\uff0c\u5e76\u8865\u5145\u90e8\u5206\u6765\u81ea\u4e2d\u6587\u8bcd\u6761\u7684\u5185\u5bb9\uff1b\u5728\u4e2d\u82f1\u6587\u5185\u5bb9\u5b8c\u5168\u76f8\u540c\u7684\u6bb5\u843d\uff0c\u4f7f\u7528\u539f\u6709\u7684\u4e2d\u6587\u7248\u672c\u66ff\u6362\u82f1\u6587\u7248\u672c\uff0c\u5176\u4ed6\u90e8\u5206\u82f1\u6587\u8bcd\u6761\u5219\u7531\u8fbd\u89c2\u7ffb\u8bd1\u3002<\/p>\n\n\n\n<p class=\"has-small-font-size\">\u8fbd\u89c2\u642c\u8fd0\u65f6\u8fdb\u884c\u4e86\u5fc5\u8981\u7684\u5408\u89c4\u5316\u5904\u7406\uff0c\u4ee5\u4f7f\u5176\u80fd\u591f\u5728\u4e2d\u56fd\u5185\u5730\u4e0a\u4f20\u3002<\/p>\n\n\n\n<p class=\"has-small-font-size\"><a href=\"https:\/\/cathayvista.top\/index.php\/wikipedia-intro\/\" data-type=\"link\" data-id=\"https:\/\/cathayvista.top\/index.php\/wikipedia-intro\/\" target=\"_blank\" rel=\"noreferrer noopener\">\u7ef4\u57fa\u767e\u79d1\uff08Wikipedia\uff09\u662f\u7f8e\u56fd\u7ef4\u57fa\u5a92\u4f53\u57fa\u91d1\u4f1a\u7684\u4e92\u8054\u7f51\u767e\u79d1\u9879\u76ee\uff08\u70b9\u51fb\u8fd9\u91cc\u4e86\u89e3\u66f4\u591a\uff09<\/a>\uff0c\u5176\u5185\u5bb9\u53ef\u80fd\u53d7\u5230\u7acb\u573a\u3001\u4fe1\u606f\u6765\u6e90\u7b49\u56e0\u7d20\u5f71\u54cd\uff0c\u8bf7\u5ba2\u89c2\u770b\u5f85\u3002\u6b63\u6587\u5185\u5bb9\u4e0d\u4ee3\u8868\u8bd1\u8005\u89c2\u70b9\u3002<\/p>\n\n\n\n<p class=\"has-small-font-size\">\u8fbd\u89c2\u63d0\u4f9b\u7684\u7ffb\u8bd1\u4ec5\u4f9b\u53c2\u8003\u3002<strong>\u6587\u4e2d\u53ef\u80fd\u5305\u542b\u65e0\u6cd5\u4ece\u4e2d\u56fd\u5927\u9646\u8bbf\u95ee\u7684\u94fe\u63a5\u3002<\/strong><\/p>\n<cite>\u6587\u4e2d\u53ef\u80fd\u5305\u542b\u65e0\u6cd5\u4ece\u4e2d\u56fd\u5185\u5730\u8bbf\u95ee\u7684\u94fe\u63a5\u3002 \u8fbd\u89c2\u6240\u642c\u8fd0\u7684\u8bcd\u6761\u4e0e\u539f\u7ef4\u57fa\u767e\u79d1\u8bcd\u6761\u540c\u6837\u9075\u5faa<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/653887754\" target=\"_blank\" rel=\"noreferrer noopener\">CC-BY-SA 4.0\u534f\u8bae<\/a>\uff0c\u5728\u7b26\u5408\u534f\u8bae\u8981\u6c42\u7684\u60c5\u51b5\u4e0b\u60a8\u53ef\u4ee5\u514d\u8d39\u4f7f\u7528\u5176\u5185\u5bb9\uff08\u5305\u62ec\u5546\u7528\uff09\u3002\u56fe\u7247\u548c\u89c6\u9891\u53ef\u80fd\u9075\u5faa\u4e0d\u540c\u7684\u534f\u8bae\uff0c\u6211\u4eec\u4f1a\u5728\u6587\u4e2d\u5177\u4f53\u4f4d\u7f6e\u6807\u660e\uff1b<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/666846485\">\u534f\u8bae\u6587\u672c\u8bf7\u70b9\u51fb\u8fd9\u91cc\u8bbf\u95ee\u3002<\/a><\/cite><\/blockquote>\n\n\n\n<p><em>Not to be confused with <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Propfan\" target=\"_blank\" rel=\"noreferrer noopener\">propfan<\/a> or <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turboprop\" target=\"_blank\" rel=\"noreferrer noopener\">turboprop<\/a>.<\/em><br><em>\u4e0d\u8981\u4e0e\u87ba\u65cb\u6868\u98ce\u6247\u6216\u6da1\u8f6e\u87ba\u65cb\u6868\u53d1\u52a8\u673a\u6df7\u6dc6\u3002<\/em><\/p>\n\n\n\n<p><em>This article is about the mechanism used in jets. For the turbo like air pressure blower sometimes misnamed Turbo fan, see <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Centrifugal_fan\" target=\"_blank\" rel=\"noreferrer noopener\">Centrifugal fan<\/a>.<\/em><br><em>\u672c\u6587\u4ecb\u7ecd\u7684\u662f\u55b7\u6c14\u673a\u4e2d\u4f7f\u7528\u7684\u673a\u5236\u3002 \u5bf9\u4e8e\u6da1\u8f6e\u5f0f\u7a7a\u6c14\u538b\u529b\u9f13\u98ce\u673a\u6709\u65f6\u88ab\u9519\u8bef\u547d\u540d\u4e3a\u201c\u6da1\u8f6e\u98ce\u6247\u201d\uff0c\u8bf7\u53c2\u9605\u201c\u79bb\u5fc3\u98ce\u6247\u201d\u3002<\/em><\/p>\n\n\n\n<h2 class=\"wp-block-heading\" id=\"h_659034614_0\">0. \u6982\u8ff0<\/h2>\n\n\n\n<p class=\"has-vivid-cyan-blue-color has-text-color has-link-color wp-elements-ee0a5df688effa2d905f4e9e9ab2e276\">\u8fbd\u89c2\u6ce8\uff1a\u6b64\u6807\u9898\u662f\u6211\u4eec\u5728\u642c\u8fd0\u3001\u6574\u5408\u8fc7\u7a0b\u4e2d\u6dfb\u52a0\u7684\u3002<\/p>\n\n\n<div class=\"wp-block-image\">\n<figure class=\"aligncenter\"><img decoding=\"async\" src=\"https:\/\/pic2.zhimg.com\/80\/v2-026234c7e6470b4d77d0ed783a0af97d_720w.webp\" alt=\"\"\/><\/figure>\n<\/div>\n\n\n<div class=\"wp-block-buttons is-layout-flex wp-block-buttons-is-layout-flex\">\n<div class=\"wp-block-button\"><a class=\"wp-block-button__link wp-element-button\" href=\"https:\/\/www.zhihu.com\/pin\/1849397981536731137\">\u56fe0-1\u548c0-2\uff08\u53d1\u5e03\u4e8e\u77e5\u4e4e\u60f3\u6cd5\uff09<\/a><\/div>\n<\/div>\n\n\n\n<p><strong>\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a<\/strong>\uff08\u82f1\u8bed\uff1a<strong>Turbofan Engine<\/strong>\uff0c\u4ea6\u79f0<strong>\u6da1\u6247\u53d1\u52a8\u673a<\/strong>\u6216\u8005<strong>\u5185\u5916\u51fd\u55b7\u6c14\u53d1\u52a8\u673a<\/strong>\uff09\u662f\u4e00\u79cd\u71c3\u6c14\u6da1\u8f6e\u5f0f<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E8%2588%25AA%25E7%25A9%25BA%25E5%258F%2591%25E5%258A%25A8%25E6%259C%25BA\" target=\"_blank\" rel=\"noreferrer noopener\">\u822a\u7a7a\u53d1\u52a8\u673a<\/a>\uff0c\u4e3b\u8981\u7279\u70b9\u662f\u5176\u9996\u7ea7\u6247\u53f6\u7684\u9762\u79ef\u8f83<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E6%25B8%25A6%25E8%25BC%25AA%25E5%2599%25B4%25E5%25B0%2584%25E7%2599%25BC%25E5%258B%2595%25E6%25A9%259F\" target=\"_blank\" rel=\"noreferrer noopener\">\u6da1\u8f6e\u55b7\u6c14\u53d1\u52a8\u673a<\/a>\u5927\u4e0a\u8bb8\u591a\u3002\u7ecf\u8fc7\u6da1\u8f6e\u55b7\u6c14\u53d1\u52a8\u673a\u7684\u7a7a\u6c14\u901a\u9053\u79f0\u4e3a\u5185\u6db5\u9053\uff0c\u7a7a\u6c14\u5728\u55b7\u6c14\u53d1\u52a8\u673a\u71c3\u70e7\u540e\u83b7\u5f97\u673a\u68b0\u80fd\uff0c\u5916\u4fa7\u7684\u7a7a\u6c14\u901a\u9053\u79f0\u4e3a\u5916\u6db5\u9053\uff0c\u7531\u5185\u542b\u7684\u6da1\u8f6e\u9a71\u52a8\u9996\u7ea7<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E5%25A2%259E%25E5%25A3%2593%25E6%2589%2587%25E8%2591%2589\" target=\"_blank\" rel=\"noreferrer noopener\">\u589e\u538b\u6247\u53f6<\/a>\u63a8\u52a8\u7a7a\u6c14\uff0c\u589e\u538b\u6247\u53f6\u540c\u65f6\u5177\u6709<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E8%259E%25BA%25E6%2597%258B%25E6%25A7%25B3\" target=\"_blank\" rel=\"noreferrer noopener\">\u87ba\u65cb\u6868<\/a>\u548c\u538b\u7f29\u7a7a\u6c14\u7684\u4f5c\u7528\uff0c\u80fd\u5c06\u90e8\u5206\u5438\u5165\u7684\u7a7a\u6c14\u901a\u8fc7\u55b7\u6c14\u53d1\u52a8\u673a\u7684\u5916\u56f4\u63d0\u4f9b\u76f4\u63a5\u63a8\u529b\uff0c\u63a8\u529b\u5373\u7531\u5185\u5916\u6db5\u9053\u5171\u540c\u4ea7\u751f\u3002<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E6%25B8%25A6%25E8%25BC%25AA%25E6%2589%2587%25E7%2599%25BC%25E5%258B%2595%25E6%25A9%259F%23cite_note-1\" target=\"_blank\" rel=\"noreferrer noopener\">[1]<\/a><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E6%25B8%25A6%25E8%25BC%25AA%25E6%2589%2587%25E7%2599%25BC%25E5%258B%2595%25E6%25A9%259F%23cite_note-stuffworks-2\" target=\"_blank\" rel=\"noreferrer noopener\">[2]<\/a>\u53ef\u540c\u65f6\u5177\u6709<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E6%25B8%25A6%25E8%25BC%25AA%25E8%259E%25BA%25E6%2597%258B%25E6%25A7%25B3\" target=\"_blank\" rel=\"noreferrer noopener\">\u6da1\u8f6e\u87ba\u65cb\u6868<\/a>\u4e0e<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E6%25B8%25A6%25E8%25BC%25AA%25E5%2599%25B4%25E5%25B0%2584%25E5%25BC%2595%25E6%2593%258E\" target=\"_blank\" rel=\"noreferrer noopener\">\u6da1\u8f6e\u55b7\u6c14<\/a><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E6%25B8%25A6%25E8%25BC%25AA%25E5%2599%25B4%25E5%25B0%2584%25E7%2599%25BC%25E5%258B%2595%25E6%25A9%259F\" target=\"_blank\" rel=\"noreferrer noopener\">\u53d1\u52a8\u673a<\/a>\u7684\u63a8\u529b\u4f9b\u7ed9\u3002<\/p>\n\n\n\n<p>The <strong>turbofan<\/strong> or <strong>fanjet<\/strong> is a type of <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Airbreathing_jet_engine\" target=\"_blank\" rel=\"noreferrer noopener\">airbreathing jet engine<\/a> that is widely used in <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Aircraft_engine\" target=\"_blank\" rel=\"noreferrer noopener\">aircraft propulsion<\/a>. The word &#8220;turbofan&#8221; is a combination of the preceding generation engine technology of the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbojet\" target=\"_blank\" rel=\"noreferrer noopener\">turbojet<\/a>, and a reference to the additional fan stage added. It consists of a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Gas_turbine_engine\" target=\"_blank\" rel=\"noreferrer noopener\">gas turbine engine<\/a> which achieves <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Mechanical_energy\" target=\"_blank\" rel=\"noreferrer noopener\">mechanical energy<\/a> from combustion,<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-stuffworks-1\" target=\"_blank\" rel=\"noreferrer noopener\">[1]<\/a> and a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Ducted_fan\" target=\"_blank\" rel=\"noreferrer noopener\">ducted fan<\/a> that uses the mechanical energy from the gas turbine to force air rearwards. Thus, whereas all the air taken in by a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbojet\" target=\"_blank\" rel=\"noreferrer noopener\">turbojet<\/a> passes through the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Combustion_chamber\" target=\"_blank\" rel=\"noreferrer noopener\">combustion chamber<\/a> and turbines, in a turbofan some of that air bypasses these components. A turbofan thus can be thought of as a turbojet being used to drive a ducted fan, with both of these contributing to the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Thrust\" target=\"_blank\" rel=\"noreferrer noopener\">thrust<\/a>.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\u6216\u98ce\u6247\u55b7\u6c14\u53d1\u52a8\u673a\u662f\u4e00\u79cd\u5e7f\u6cdb\u7528\u4e8e\u98de\u673a\u63a8\u8fdb\u7684\u5438\u6c14\u5f0f\u55b7\u6c14\u53d1\u52a8\u673a\u3002 \u201c\u6da1\u8f6e\u98ce\u6247\u201d\u4e00\u8bcd\u662f\u4e0a\u4e00\u4ee3\u6da1\u8f6e\u55b7\u6c14\u53d1\u52a8\u673a\u6280\u672f\u7684\u7ec4\u5408\uff0c\u5e76\u5f15\u7528\u4e86\u9644\u52a0\u7684\u98ce\u6247\u7ea7\u3002 \u5b83\u7531\u4e00\u4e2a\u4ece\u71c3\u70e7\u4e2d\u83b7\u5f97\u673a\u68b0\u80fd\u7684\u71c3\u6c14\u6da1\u8f6e\u53d1\u52a8\u673a[1]\u548c\u4e00\u4e2a\u5229\u7528\u71c3\u6c14\u6da1\u8f6e\u673a\u7684\u673a\u68b0\u80fd\u8feb\u4f7f\u7a7a\u6c14\u5411\u540e\u63a8\u52a8\u7684\u6db5\u9053\u98ce\u6247\u7ec4\u6210\u3002 \u56e0\u6b64\uff0c\u6da1\u8f6e\u55b7\u6c14\u53d1\u52a8\u673a\u5438\u5165\u7684\u6240\u6709\u7a7a\u6c14\u90fd\u4f1a\u7a7f\u8fc7\u71c3\u70e7\u5ba4\u548c\u6da1\u8f6e\u673a\uff0c\u800c\u5728\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\u4e2d\uff0c\u90e8\u5206\u7a7a\u6c14\u4f1a\u7ed5\u8fc7\u8fd9\u4e9b\u90e8\u4ef6\u3002 \u56e0\u6b64\uff0c\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\u53ef\u4ee5\u88ab\u8ba4\u4e3a\u662f\u7528\u4e8e\u9a71\u52a8\u6db5\u9053\u98ce\u6247\u7684\u6da1\u8f6e\u55b7\u6c14\u53d1\u52a8\u673a\uff0c\u4e24\u8005\u90fd\u6709\u52a9\u4e8e\u63a8\u529b\u3002<\/p>\n\n\n\n<p>\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\u5916\u89c2\u4e0a\u4f3c\u4e4e\u662f\u66f4\u7c97\u7684\u53d1\u52a8\u673a\uff0c\u5b9e\u9645\u4e0a\u53ea\u6709\u4e2d\u5fc3\u662f\u55b7\u6c14\u53d1\u52a8\u673a\uff0c\u5176\u4ed6\u5168\u662f\u6247\u98ce\u63a8\u8fdb\uff0c\u56e0\u4e3a\u5e76\u975e\u53ea\u4f9d\u9760\u6da1\u8f6e\u55b7\u6c14\u76f4\u63a5\u71c3\u6cb9\u71c3\u70e7\u51fa\u9ad8\u538b\u7a7a\u6c14\u63d0\u4f9b\u63a8\u529b\uff0c\u6240\u4ee5\u5355\u4f4d\u63a8\u529b\u5c0f\u65f6\u8017\u6cb9\u7387\u6bd4\u7eaf\u6da1\u8f6e\u55b7\u6c14\u4f73\uff0c\u4f46\u87ba\u65cb\u6247\u53f6\u901f\u5ea6\u8d8a\u5feb\u7684\u63a8\u529b\u91cd\u91cf\u6bd4\u8017\u635f\u529f\u7387\u8f83\u5927\uff0c\u6bd4\u8f83\u7eaf\u6da1\u8f6e\u55b7\u6c14\uff0c<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E8%25B6%2585%25E9%259F%25B3%25E9%2580%259F\" target=\"_blank\" rel=\"noreferrer noopener\">\u8d85\u97f3\u901f<\/a>\u98de\u884c\u65f6\u5176\u53d7\u5230<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E9%2582%258A%25E7%2595%258C%25E5%25B1%25A4\" target=\"_blank\" rel=\"noreferrer noopener\">\u9644\u9762\u5c42<\/a>\u5f71\u54cd\u4f7f\u5176\u4f4e\u6c14\u538b\u9ad8\u7a7a\u4e0e\u8d85\u97f3\u901f\u4e0b\u63a8\u529b\u91cd\u91cf\u4e0d\u4f73\u3002\u4e8e\u662f\u4e4e\uff0c\u6da1\u6247\u53d1\u52a8\u673a\u6700\u9002\u5408\u98de\u884c\u901f\u5ea6\u4e3a\u6bcf\u5c0f\u65f6400\u81f32,000<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E5%2585%25AC%25E9%2587%258C\" target=\"_blank\" rel=\"noreferrer noopener\">\u516c\u91cc<\/a>\u65f6\u4f7f\u7528\uff0c\u6545\u6b64\u73b0\u5728\u591a\u6570\u7684<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E5%2599%25B4%25E5%25B0%2584%25E6%25A9%259F\" target=\"_blank\" rel=\"noreferrer noopener\">\u55b7\u6c14\u673a<\/a>\u53d1\u52a8\u673a\u90fd\u662f\u91c7\u7528\u6da1\u6247\u53d1\u52a8\u673a\u4f5c\u4e3a\u52a8\u529b\u6765\u6e90\u3002<\/p>\n\n\n\n<p>The ratio of the mass-flow of air bypassing the engine core to the mass-flow of air passing through the core is referred to as the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Bypass_ratio\" target=\"_blank\" rel=\"noreferrer noopener\">bypass ratio<\/a>. The engine produces thrust through a combination of these two portions working together; engines that use more <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Propelling_nozzle\" target=\"_blank\" rel=\"noreferrer noopener\">jet thrust<\/a> relative to fan thrust are known as <em>low-bypass turbofans<\/em>, conversely those that have considerably more fan thrust than jet thrust are known as <em>high-bypass<\/em>. Most commercial aviation jet engines in use today are of the high-bypass type,<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-Hall-2\" target=\"_blank\" rel=\"noreferrer noopener\">[2]<\/a><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-HackerBurghardt2009-3\" target=\"_blank\" rel=\"noreferrer noopener\">[3]<\/a> and most modern military fighter engines are low-bypass.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-Verma2013-4\" target=\"_blank\" rel=\"noreferrer noopener\">[4]<\/a><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-Magill-5\" target=\"_blank\" rel=\"noreferrer noopener\">[5]<\/a> <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Afterburner\" target=\"_blank\" rel=\"noreferrer noopener\">Afterburners<\/a> are used on low-bypass turbofan engines with bypass and core mixing before the afterburner.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u7ed5\u8fc7\u53d1\u52a8\u673a\u6838\u5fc3\u7684\u7a7a\u6c14\u8d28\u91cf\u6d41\u91cf\u4e0e\u901a\u8fc7\u6838\u5fc3\u7684\u7a7a\u6c14\u8d28\u91cf\u6d41\u91cf\u4e4b\u6bd4\u79f0\u4e3a\u6db5\u9053\u6bd4\u3002 \u53d1\u52a8\u673a\u901a\u8fc7\u8fd9\u4e24\u4e2a\u90e8\u5206\u4e00\u8d77\u5de5\u4f5c\u6765\u4ea7\u751f\u63a8\u529b\uff1b \u76f8\u5bf9\u4e8e\u98ce\u6247\u63a8\u529b\u4f7f\u7528\u66f4\u591a\u55b7\u5c04\u63a8\u529b\u7684\u53d1\u52a8\u673a\u88ab\u79f0\u4e3a\u4f4e\u6db5\u9053\u6bd4\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\uff0c\u76f8\u53cd\uff0c\u90a3\u4e9b\u98ce\u6247\u63a8\u529b\u6bd4\u55b7\u5c04\u63a8\u529b\u5927\u5f97\u591a\u7684\u53d1\u52a8\u673a\u88ab\u79f0\u4e3a\u9ad8\u6db5\u9053\u6bd4\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\u3002 \u5f53\u4eca\u4f7f\u7528\u7684\u5927\u591a\u6570\u5546\u7528\u822a\u7a7a\u55b7\u6c14\u53d1\u52a8\u673a\u90fd\u662f\u9ad8\u6db5\u9053\u6bd4\u7c7b\u578b\uff0c[2][3]\uff0c\u5927\u591a\u6570\u73b0\u4ee3\u519b\u7528\u6218\u6597\u673a\u53d1\u52a8\u673a\u90fd\u662f\u4f4e\u6db5\u9053\u6bd4\u53d1\u52a8\u673a\u3002[4][5] \u52a0\u529b\u71c3\u70e7\u5ba4\u7528\u4e8e\u4f4e\u65c1\u901a\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\uff0c\u5728\u52a0\u529b\u71c3\u70e7\u5ba4\u4e4b\u524d\u5177\u6709\u65c1\u8def\u548c\u6838\u5fc3\u6df7\u5408\u3002<\/p>\n\n\n\n<p>\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\u7684<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E6%25B6%25B5%25E9%2581%2593%25E6%25AF%2594\" target=\"_blank\" rel=\"noreferrer noopener\">\u6db5\u9053\u6bd4<\/a>\u662f\u5355\u4f4d\u65f6\u95f4\u5185\u4e0d\u7ecf\u8fc7\u71c3\u70e7\u5ba4\u7684\u7a7a\u6c14\u8d28\u91cf\uff0c\u4e0e\u901a\u8fc7\u71c3\u70e7\u5ba4\u7684\u7a7a\u6c14\u8d28\u91cf\u7684\u6bd4\u4f8b\u3002\u6db5\u9053\u6bd4\u4e3a\u96f6\u7684\u6da1\u6247\u53d1\u52a8\u673a\u5373\u662f\u6da1\u8f6e\u55b7\u6c14\u53d1\u52a8\u673a\uff0c\u65e9\u671f\u7684\u6da1\u6247\u53d1\u52a8\u673a\u548c\u73b0\u4ee3\u6218\u6597\u673a\u4f7f\u7528\u7684\u6da1\u6247\u53d1\u52a8\u673a\u6db5\u9053\u6bd4\u90fd\u8f83\u4f4e\uff0c\u4f8b\u5982\u4e16\u754c\u4e0a\u7b2c\u4e00\u6b3e\u5b9e\u7528\u6da1\u6247\u53d1\u52a8\u673a\uff0c<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E5%258B%259E%25E6%2596%25AF%25E8%2590%258A%25E6%2596%25AF\" target=\"_blank\" rel=\"noreferrer noopener\">\u7f57\u5c14\u65af\u00b7\u7f57\u4f0a\u65af<\/a>\u7684<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E5%258B%259E%25E6%2596%25AF%25E8%2590%258A%25E6%2596%25AF%25E5%25BA%25B7%25E5%25A8%2581\" target=\"_blank\" rel=\"noreferrer noopener\">\u5eb7\u5a01\u578b<\/a>\u6db5\u9053\u6bd4\u53ea\u67090.3\uff0c\u73b0\u4ee3\u591a\u6570<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E6%25B0%2591%25E8%2588%25AA%25E6%25A9%259F\" target=\"_blank\" rel=\"noreferrer noopener\">\u6c11\u7528\u98de\u673a<\/a>\u4e3a\u4e86\u7701\u6cb9\uff0c\u53d1\u52a8\u673a\u7684\u6db5\u9053\u6bd4\u8d8a\u6765\u8d8a\u5927\uff0c\u901a\u5e38\u90fd\u57285\u4ee5\u4e0a\uff0c\u8ddf\u4f7f\u7528\u87ba\u65cb\u6868\u98de\u884c\u5176\u5b9e\u662f\u5dee\u4e0d\u591a\u3002\u6db5\u9053\u6bd4\u9ad8\u7684\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\u8017\u6cb9\u8f83\u5c11\uff0c\u4f46\u63a8\u529b\u5374\u4e0e\u6da1\u8f6e\u55b7\u6c14\u53d1\u52a8\u673a\u76f8\u5f53\uff0c\u4e14\u8fd0\u8f6c\u65f6\u8fd8\u5b81\u9759\u5f97\u591a\u3002<\/p>\n\n\n\n<p>\u81f3\u4e8e\u6218\u6597\u673a\u4f7f\u7528\u4f4e<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E6%25B6%25B5%25E9%2581%2593%25E6%25AF%2594\" target=\"_blank\" rel=\"noreferrer noopener\">\u6db5\u9053\u6bd4<\/a>\u53d1\u52a8\u673a\uff0c\u4e3b\u8981\u662f\u56e0\u4e3a\u622a\u9762\u79ef\u4e0e\u5e38\u7528\u98de\u884c\u901f\u5ea6\u4e0e\u6c11\u7528\u98de\u673a\u4e0d\u540c\u3002\u9ad8\u6db5\u9053\u6bd4\u7684\u53d1\u52a8\u673a\u622a\u9762\u79ef\u8fc7\u5927\u5728\u8d85\u97f3\u901f\u7684\u65f6\u5019\u963b\u529b\u8fc7\u5927\uff0c\u53e6\u5916\u5728\u8d85\u97f3\u901f\u7684\u72b6\u51b5\u4e0b\u6548\u7387\u4e5f\u4f1a\u6bd4\u7eaf\u6da1\u8f6e\u55b7\u6c14\u751a\u81f3\u4e8e\u4f4e\u6db5\u9053\u6bd4\u8bbe\u8ba1\u8fd8\u4f4e\uff0c\u6240\u4ee5\u6218\u6597\u673a\u7686\u4f7f\u7528\u4f4e\u6db5\u9053\u6bd4\u53d1\u52a8\u673a\uff08\u6db5\u9053\u6bd4\u7686\u4f4e\u4e8e1\uff09\u3002\u53ea\u5728\u8d85\u97f3\u901f\u98de\u884c\u7684<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E5%258D%2594%25E5%2592%258C%25E5%25BC%258F%25E5%25AE%25A2%25E6%25A9%259F\" target=\"_blank\" rel=\"noreferrer noopener\">\u534f\u548c\u5f0f\u5ba2\u673a<\/a>\uff0c\u56e0\u4e3a\u957f\u65f6\u95f4\u5904\u4e8e\u8d85\u97f3\u901f\u72b6\u6001\uff0c\u4e3a\u4e86\u63d0\u5347\u6548\u7387\u4e0e\u964d\u4f4e\u6210\u672c\uff0c\u5c31\u662f\u4f7f\u7528\u7eaf\u6da1\u8f6e\u55b7\u6c14\u800c\u65e0\u6db5\u9053\u6bd4\u7684\u53d1\u52a8\u673a\uff0c\u662f\u5c11\u6570\u771f\u6b63\u5229\u7528\u55b7\u6c14\u98de\u884c\u7684\u98de\u673a\u3002<\/p>\n\n\n\n<p>Modern turbofans have either a large single-stage fan or a smaller fan with several stages. An early configuration combined a low-pressure turbine and fan in a single rear-mounted unit.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u73b0\u4ee3\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\u8981\u4e48\u5177\u6709\u5927\u578b\u5355\u7ea7\u98ce\u6247\uff0c\u8981\u4e48\u5177\u6709\u8f83\u5c0f\u7684\u591a\u7ea7\u98ce\u6247\u3002 \u65e9\u671f\u7684\u914d\u7f6e\u5c06\u4f4e\u538b\u6da1\u8f6e\u673a\u548c\u98ce\u6247\u7ec4\u5408\u5728\u4e00\u4e2a\u540e\u7f6e\u5355\u5143\u4e2d\u3002<\/p>\n\n\n\n<h2 class=\"wp-block-heading\" id=\"h_659034614_1\">1. \u539f\u7406 | Principles<\/h2>\n\n\n\n<div class=\"wp-block-buttons is-layout-flex wp-block-buttons-is-layout-flex\">\n<div class=\"wp-block-button\"><a class=\"wp-block-button__link wp-element-button\" href=\"https:\/\/www.zhihu.com\/pin\/1849397642280452096\">\u56fe1-1\uff08\u53d1\u5e03\u4e8e\u77e5\u4e4e\u60f3\u6cd5\uff09<\/a><\/div>\n<\/div>\n\n\n\n<p><strong>\u4e3b\u8981\u7ec4\u6210\u90e8\u5206<\/strong><\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E8%25BF%259B%25E6%25B0%2594%25E9%2581%2593\" target=\"_blank\" rel=\"noreferrer noopener\">\u8fdb\u6c14\u9053<\/a><\/li>\n\n\n\n<li>\u98ce\u6247\u603b\u6210\n<ul class=\"wp-block-list\">\n<li>\u4f4e\u538b\u538b\u6c14\u673a\uff08Low pressure compressor\uff09<\/li>\n\n\n\n<li>\u9ad8\u538b\u538b\u6c14\u673a\uff08High pressure compressor\uff09<\/li>\n<\/ul>\n<\/li>\n\n\n\n<li><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E7%2587%2583%25E7%2583%25A7%25E5%25AE%25A4\" target=\"_blank\" rel=\"noreferrer noopener\">\u71c3\u70e7\u5ba4<\/a><\/li>\n\n\n\n<li>\u9ad8\u538b\u6da1\u8f6e\uff08High pressure turbine\uff09<\/li>\n\n\n\n<li>\u4f4e\u538b\u6da1\u8f6e\uff08Low pressure turbine\uff09<\/li>\n\n\n\n<li><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E5%25BE%258C%25E7%2587%2583%25E5%2599%25A8\" target=\"_blank\" rel=\"noreferrer noopener\">\u52a0\u529b\u71c3\u70e7\u5ba4<\/a><\/li>\n\n\n\n<li><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/zh.wikipedia.org\/wiki\/%25E5%2596%25B7%25E5%2598%25B4\" target=\"_blank\" rel=\"noreferrer noopener\">\u55b7\u7ba1<\/a><\/li>\n<\/ul>\n\n\n\n<p>The turbofan was invented to improve the fuel consumption of the turbojet. It achieves this by pushing more air, thus increasing the mass and lowering the speed of the propelling jet compared to that of the turbojet. This is done mechanically by adding a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Ducted_fan\" target=\"_blank\" rel=\"noreferrer noopener\">ducted fan<\/a> rather than using viscous forces<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-6\" target=\"_blank\" rel=\"noreferrer noopener\">[6]<\/a> by adding an ejector, as first envisaged by Whittle.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-7\" target=\"_blank\" rel=\"noreferrer noopener\">[7]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u6da1\u6247\u53d1\u52a8\u673a\u7684\u53d1\u660e\u662f\u4e3a\u4e86\u6539\u5584\u6da1\u55b7\u53d1\u52a8\u673a\u7684\u71c3\u6cb9\u6d88\u8017\u3002\u5b83\u901a\u8fc7\u589e\u52a0\u63a8\u8fdb\u6c14\u6d41\u7684\u8d28\u91cf\uff0c\u4ece\u800c\u964d\u4f4e\u63a8\u8fdb\u55b7\u6d41\u7684\u901f\u5ea6\uff0c\u4ee5\u6b64\u8fbe\u5230\u8282\u7701\u71c3\u6599\u7684\u76ee\u7684\u3002\u4e0e\u6da1\u55b7\u53d1\u52a8\u673a\u76f8\u6bd4\uff0c\u6da1\u6247\u53d1\u52a8\u673a\u901a\u8fc7\u589e\u52a0\u4e00\u4e2a\u5185\u7f18\u98ce\u6247\u6765\u5b9e\u73b0\u8fd9\u4e00\u70b9\uff0c\u800c\u4e0d\u662f\u901a\u8fc7\u589e\u52a0\u55b7\u5c04\u5668\u6765\u5229\u7528\u9ecf\u6027\u529b[6]\uff0c\u8fd9\u662f\u7531Whittle\u9996\u5148\u8bbe\u60f3\u7684\u65b9\u5f0f[7]\u3002<\/p>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Frank_Whittle\" target=\"_blank\" rel=\"noreferrer noopener\">Frank Whittle<\/a> envisioned flight speeds of 500 mph in his March 1936 UK patent 471,368 &#8220;Improvements relating to the propulsion of aircraft&#8221;, in which he describes the principles behind the turbofan,<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-8\" target=\"_blank\" rel=\"noreferrer noopener\">[8]<\/a> although not called as such at that time. While the turbojet uses the gas from its thermodynamic cycle as its propelling jet, for aircraft speeds below 500 mph there are two penalties to this design which are addressed by the turbofan.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5f17\u5170\u514b\u00b7\u60e0\u7279\u5c14\u5728\u4ed61936\u5e743\u6708\u7684\u82f1\u56fd\u4e13\u5229471,368\u300a\u6539\u8fdb\u6709\u5173\u98de\u673a\u63a8\u8fdb\u7684\u65b9\u6cd5\u300b\u4e2d\u8bbe\u60f3\u4e86500\u82f1\u91cc\u6bcf\u5c0f\u65f6\u7684\u98de\u884c\u901f\u5ea6\uff0c\u5e76\u5728\u5176\u4e2d\u63cf\u8ff0\u4e86\u6da1\u6247\u53d1\u52a8\u673a\u80cc\u540e\u7684\u539f\u7406[8]\uff0c\u5c3d\u7ba1\u5f53\u65f6\u8fd8\u6ca1\u6709\u4ee5\u8fd9\u6837\u7684\u540d\u79f0\u3002\u5c3d\u7ba1\u6da1\u55b7\u53d1\u52a8\u673a\u4f7f\u7528\u5176\u70ed\u529b\u5faa\u73af\u4e2d\u7684\u6c14\u4f53\u4f5c\u4e3a\u63a8\u8fdb\u55b7\u6d41\uff0c\u4f46\u5728\u98de\u884c\u901f\u5ea6\u4f4e\u4e8e500\u82f1\u91cc\u6bcf\u5c0f\u65f6\u65f6\uff0c\u8fd9\u79cd\u8bbe\u8ba1\u5b58\u5728\u4e24\u4e2a\u95ee\u9898\uff0c\u800c\u6da1\u6247\u53d1\u52a8\u673a\u89e3\u51b3\u4e86\u8fd9\u4e9b\u95ee\u9898\u3002<\/p>\n\n\n\n<p>Firstly, energy is wasted as the propelling jet is going much faster rearwards than the aircraft is going forwards, leaving a very fast wake. This wake contains kinetic energy that reflects the fuel used to produce it, rather than the fuel used to move the aircraft forwards. A turbofan harvests that wasted velocity and uses it to power a ducted fan that blows air in bypass channels around the rest of the turbine. This reduces the speed of the propelling jet while pushing more air, and thus more mass.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u9996\u5148\uff0c\u7531\u4e8e\u63a8\u8fdb\u55b7\u6d41\u5411\u540e\u7684\u901f\u5ea6\u8fdc\u8fdc\u5feb\u4e8e\u98de\u673a\u5411\u524d\u7684\u901f\u5ea6\uff0c\u80fd\u91cf\u88ab\u6d6a\u8d39\u6389\u4e86\uff0c\u5f62\u6210\u4e86\u4e00\u4e2a\u975e\u5e38\u5feb\u901f\u7684\u5c3e\u6d41\u3002\u8fd9\u4e2a\u5c3e\u6d41\u5305\u542b\u4e86\u7528\u4e8e\u4ea7\u751f\u5b83\u7684\u71c3\u6599\u6240\u53cd\u6620\u7684\u52a8\u80fd\uff0c\u800c\u4e0d\u662f\u7528\u4e8e\u63a8\u52a8\u98de\u673a\u5411\u524d\u7684\u71c3\u6599\u3002\u6da1\u6247\u53d1\u52a8\u673a\u5229\u7528\u8fd9\u79cd\u88ab\u6d6a\u8d39\u7684\u901f\u5ea6\uff0c\u7528\u6765\u9a71\u52a8\u4e00\u4e2a\u5e26\u5bfc\u6d41\u98ce\u6247\u7684\u65c1\u901a\u901a\u9053\uff0c\u5c06\u7a7a\u6c14\u7ed5\u8fc7\u6da1\u8f6e\u7684\u5176\u4f59\u90e8\u5206\u5439\u51fa\u3002\u8fd9\u964d\u4f4e\u4e86\u63a8\u8fdb\u55b7\u6d41\u7684\u901f\u5ea6\u540c\u65f6\u4e5f\u63a8\u52a8\u66f4\u591a\u7684\u7a7a\u6c14\uff0c\u4ece\u800c\u589e\u52a0\u4e86\u8d28\u91cf\u3002<\/p>\n\n\n\n<p>The other penalty is that combustion is less efficient at lower speeds. Any action to reduce the fuel consumption of the engine by increasing its pressure ratio or turbine temperature to achieve better combustion causes a corresponding increase in pressure and temperature in the exhaust duct which in turn cause a higher gas speed from the propelling nozzle (and higher KE and wasted fuel). Although the engine would use less fuel to produce a pound of thrust, more fuel is wasted in the faster propelling jet. In other words, the independence of thermal and propulsive efficiencies, as exists with the piston engine\/propeller combination which preceded the turbojet, is lost.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-9\" target=\"_blank\" rel=\"noreferrer noopener\">[9]<\/a> In contrast, Roth<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-10\" target=\"_blank\" rel=\"noreferrer noopener\">[10]<\/a> considers regaining this independence the single most important feature of the turbofan which allows specific thrust to be chosen independently of the gas generator cycle.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u53e6\u4e00\u4e2a\u95ee\u9898\u662f\uff0c\u5728\u8f83\u4f4e\u7684\u901f\u5ea6\u4e0b\uff0c\u71c3\u70e7\u6548\u7387\u8f83\u4f4e\u3002\u4e3a\u4e86\u901a\u8fc7\u589e\u52a0\u6da1\u6247\u53d1\u52a8\u673a\u7684\u538b\u529b\u6bd4\u6216\u6da1\u8f6e\u6e29\u5ea6\u4ee5\u5b9e\u73b0\u66f4\u597d\u7684\u71c3\u70e7\u6765\u51cf\u5c11\u71c3\u6599\u6d88\u8017\uff0c\u5bfc\u81f4\u6392\u6c14\u7ba1\u4e2d\u7684\u538b\u529b\u548c\u6e29\u5ea6\u76f8\u5e94\u589e\u52a0\uff0c\u4ece\u800c\u5bfc\u81f4\u63a8\u8fdb\u55b7\u5634\u4e2d\u7684\u6c14\u4f53\u901f\u5ea6\u589e\u52a0\uff08\u4ee5\u53ca\u52a8\u80fd\u548c\u71c3\u6599\u6d6a\u8d39\u589e\u52a0\uff09\u3002\u5c3d\u7ba1\u53d1\u52a8\u673a\u6bcf\u4ea7\u751f\u4e00\u78c5\u7684\u63a8\u529b\u6240\u9700\u7684\u71c3\u6599\u66f4\u5c11\uff0c\u4f46\u5728\u901f\u5ea6\u66f4\u5feb\u7684\u63a8\u8fdb\u55b7\u6d41\u4e2d\u6d6a\u8d39\u66f4\u591a\u7684\u71c3\u6599\u3002\u6362\u53e5\u8bdd\u8bf4\uff0c\u4e0e\u4e4b\u524d\u7684\u6d3b\u585e\u53d1\u52a8\u673a\/\u87ba\u65cb\u6868\u7ec4\u5408\u76f8\u6bd4\uff08\u8fd9\u79cd\u7ec4\u5408\u5728\u6da1\u55b7\u53d1\u52a8\u673a\u4e4b\u524d\u5b58\u5728\uff09\uff0c\u70ed\u6548\u7387\u548c\u63a8\u529b\u6548\u7387\u662f\u72ec\u7acb\u7684\uff0c\u8fd9\u79cd\u72ec\u7acb\u6027\u5df2\u7ecf\u4e27\u5931[9]\u3002\u76f8\u6bd4\u4e4b\u4e0b\uff0cRoth\u8ba4\u4e3a\uff0c\u6062\u590d\u8fd9\u79cd\u72ec\u7acb\u6027\u662f\u6da1\u6247\u53d1\u52a8\u673a\u6700\u91cd\u8981\u7684\u7279\u70b9\uff0c\u5b83\u5141\u8bb8\u7279\u5b9a\u7684\u63a8\u529b\u72ec\u7acb\u4e8e\u6c14\u4f53\u53d1\u751f\u5668\u5faa\u73af\u7684\u9009\u62e9[10]\u3002<\/p>\n\n\n\n<p>The working substance of the thermodynamic cycle is the only mass accelerated to produce thrust in a turbojet which is a serious limitation (high fuel consumption) for aircraft speeds below supersonic. For subsonic flight speeds the speed of the propelling jet has to be reduced because there is a price to be paid in producing the thrust. The energy required to accelerate the gas inside the engine (increase in kinetic energy) is expended in two ways, by producing a change in momentum ( ie a force), and a wake which is an unavoidable consequence of producing thrust by an airbreathing engine<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-11\" target=\"_blank\" rel=\"noreferrer noopener\">[11]<\/a> (or propeller). The wake velocity, and fuel burned to produce it, can be reduced and the required thrust still maintained by increasing the mass accelerated. A turbofan does this by transferring energy available inside the engine, from the gas generator, to a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Ducted_fan\" target=\"_blank\" rel=\"noreferrer noopener\">ducted fan<\/a> which produces a second, additional mass of accelerated air.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6da1\u55b7\u53d1\u52a8\u673a\u7684\u70ed\u529b\u5faa\u73af\u4e2d\u7684\u5de5\u4f5c\u7269\u8d28\u662f\u552f\u4e00\u7528\u4e8e\u4ea7\u751f\u63a8\u529b\u7684\u52a0\u901f\u8d28\u91cf\uff0c\u8fd9\u5bf9\u4e8e\u4e9a\u97f3\u901f\u7684\u98de\u884c\u901f\u5ea6\u6765\u8bf4\u662f\u4e00\u4e2a\u4e25\u91cd\u7684\u9650\u5236\uff08\u71c3\u6599\u6d88\u8017\u9ad8\uff09\u3002\u5bf9\u4e8e\u4e9a\u97f3\u901f\u98de\u884c\u901f\u5ea6\uff0c\u63a8\u8fdb\u55b7\u6d41\u7684\u901f\u5ea6\u5fc5\u987b\u964d\u4f4e\uff0c\u56e0\u4e3a\u4ea7\u751f\u63a8\u529b\u662f\u9700\u8981\u4ed8\u51fa\u4ee3\u4ef7\u7684\u3002\u52a0\u901f\u53d1\u52a8\u673a\u5185\u90e8\u6c14\u4f53\uff08\u52a8\u80fd\u589e\u52a0\uff09\u6240\u9700\u7684\u80fd\u91cf\u4ee5\u4e24\u79cd\u65b9\u5f0f\u6d88\u8017\uff0c\u4e00\u79cd\u662f\u4ea7\u751f\u52a8\u91cf\u53d8\u5316\uff08\u5373\u529b\uff09\uff0c\u53e6\u4e00\u79cd\u662f\u4ea7\u751f\u5c3e\u6d41\uff0c\u8fd9\u662f\u901a\u8fc7\u7a7a\u6c14\u547c\u5438\u53d1\u52a8\u673a\uff08\u6216\u87ba\u65cb\u6868\uff09\u4ea7\u751f\u63a8\u529b\u7684\u4e0d\u53ef\u907f\u514d\u7684\u540e\u679c[11]\u3002\u5c3e\u6d41\u7684\u901f\u5ea6\u548c\u4ea7\u751f\u5c3e\u6d41\u6240\u71c3\u70e7\u7684\u71c3\u6599\u53ef\u4ee5\u901a\u8fc7\u589e\u52a0\u52a0\u901f\u8d28\u91cf\u6765\u51cf\u5c11\uff0c\u5e76\u4ecd\u7136\u4fdd\u6301\u6240\u9700\u7684\u63a8\u529b\u3002\u6da1\u6247\u53d1\u52a8\u673a\u901a\u8fc7\u5c06\u53d1\u52a8\u673a\u5185\u7684\u80fd\u91cf\u4ece\u6c14\u4f53\u53d1\u751f\u5668\u8f6c\u79fb\u5230\u5e26\u5bfc\u6d41\u98ce\u6247\u4e0a\uff0c\u4ea7\u751f\u4e86\u7b2c\u4e8c\u4e2a\u989d\u5916\u7684\u52a0\u901f\u7a7a\u6c14\u8d28\u91cf\uff0c\u5b9e\u73b0\u4e86\u8fd9\u4e00\u70b9\u3002<\/p>\n\n\n\n<p>The transfer of energy from the core to bypass air results in lower pressure and temperature gas entering the core nozzle (lower exhaust velocity) and fan-produced temperature and pressure entering the fan nozzle. The amount of energy transferred depends on how much pressure rise the fan is designed to produce (fan pressure ratio). The best energy exchange (lowest fuel consumption) between the two flows, and how the jet velocities compare, depends on how efficiently the transfer takes place which depends on the losses in the fan-turbine and fan.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-12\" target=\"_blank\" rel=\"noreferrer noopener\">[12]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u5c06\u80fd\u91cf\u4ece\u6838\u5fc3\u4f20\u8f93\u5230\u65c1\u901a\u7a7a\u6c14\u4e2d\u5bfc\u81f4\u8fdb\u5165\u6838\u5fc3\u55b7\u5634\u7684\u6c14\u4f53\u7684\u538b\u529b\u548c\u6e29\u5ea6\u964d\u4f4e\uff08\u6392\u6c14\u901f\u5ea6\u964d\u4f4e\uff09\uff0c\u800c\u8fdb\u5165\u98ce\u6247\u55b7\u5634\u7684\u6c14\u4f53\u7684\u6e29\u5ea6\u548c\u538b\u529b\u7531\u98ce\u6247\u4ea7\u751f\u3002\u4f20\u8f93\u7684\u80fd\u91cf\u91cf\u53d6\u51b3\u4e8e\u98ce\u6247\u8bbe\u8ba1\u8981\u4ea7\u751f\u591a\u5c11\u538b\u529b\u589e\u5347\uff08\u98ce\u6247\u538b\u529b\u6bd4\uff09\u3002\u4e24\u4e2a\u6d41\u4e4b\u95f4\u7684\u80fd\u91cf\u4ea4\u6362\uff08\u71c3\u6599\u6d88\u8017\u6700\u4f4e\uff09\u4ee5\u53ca\u55b7\u6c14\u901f\u5ea6\u7684\u6bd4\u8f83\u53d6\u51b3\u4e8e\u4f20\u8f93\u7684\u6548\u7387\uff0c\u8fd9\u53c8\u53d6\u51b3\u4e8e\u98ce\u6247-\u6da1\u8f6e\u548c\u98ce\u6247\u4e2d\u7684\u635f\u5931[12]\u3002<\/p>\n\n\n\n<p>The fan flow has lower exhaust velocity, giving much more thrust per unit energy (lower <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Specific_thrust\" target=\"_blank\" rel=\"noreferrer noopener\">specific thrust<\/a>). Both airstreams contribute to the gross thrust of the engine. The additional air for the bypass stream increases the ram drag in the air intake stream-tube, but there is still a significant increase in net thrust. The overall effective exhaust velocity of the two exhaust jets can be made closer to a normal subsonic aircraft&#8217;s flight speed and gets closer to the ideal <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Aquatic_locomotion%23Efficiency\" target=\"_blank\" rel=\"noreferrer noopener\">Froude efficiency<\/a>. A turbofan accelerates a larger mass of air more slowly, compared to a turbojet which accelerates a smaller amount more quickly, which is a less efficient way to generate the same thrust (see the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23Efficiency\" target=\"_blank\" rel=\"noreferrer noopener\">efficiency<\/a> section below).<br>\u53c2\u8003\u8bd1\u6587\uff1a\u98ce\u6247\u6d41\u5177\u6709\u8f83\u4f4e\u7684\u6392\u6c14\u901f\u5ea6\uff0c\u6bcf\u5355\u4f4d\u80fd\u91cf\u4ea7\u751f\u66f4\u591a\u7684\u63a8\u529b\uff08\u6bd4\u51b2\u8f83\u4f4e\uff09\u3002\u4e24\u4e2a\u6c14\u6d41\u90fd\u5bf9\u53d1\u52a8\u673a\u7684\u603b\u63a8\u529b\u505a\u51fa\u8d21\u732e\u3002\u65c1\u901a\u6d41\u7684\u989d\u5916\u7a7a\u6c14\u589e\u52a0\u4e86\u8fdb\u6c14\u6d41\u7ba1\u4e2d\u7684\u51b2\u538b\u963b\u529b\uff0c\u4f46\u51c0\u63a8\u529b\u4ecd\u7136\u663e\u8457\u589e\u52a0\u3002\u4e24\u4e2a\u6392\u6c14\u55b7\u6d41\u7684\u6574\u4f53\u6709\u6548\u6392\u6c14\u901f\u5ea6\u53ef\u4ee5\u63a5\u8fd1\u6b63\u5e38\u4e9a\u97f3\u901f\u98de\u673a\u7684\u98de\u884c\u901f\u5ea6\uff0c\u5e76\u63a5\u8fd1\u7406\u60f3\u7684\u5f17\u52b3\u5fb7\u6548\u7387\u3002\u6da1\u55b7\u53d1\u52a8\u673a\u4ee5\u8f83\u6162\u7684\u901f\u5ea6\u52a0\u901f\u66f4\u5927\u8d28\u91cf\u7684\u7a7a\u6c14\uff0c\u800c\u6da1\u55b7\u53d1\u52a8\u673a\u4ee5\u8f83\u5feb\u7684\u901f\u5ea6\u52a0\u901f\u8f83\u5c0f\u8d28\u91cf\u7684\u7a7a\u6c14\uff0c\u8fd9\u662f\u4e00\u79cd\u4ea7\u751f\u76f8\u540c\u63a8\u529b\u7684\u6548\u7387\u8f83\u4f4e\u7684\u65b9\u5f0f\uff08\u8bf7\u53c2\u9605\u4e0b\u9762\u7684\u6548\u7387\u90e8\u5206\uff09\u3002<\/p>\n\n\n\n<p>The ratio of the mass-flow of air bypassing the engine core compared to the mass-flow of air passing through the core is referred to as the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Bypass_ratio\" target=\"_blank\" rel=\"noreferrer noopener\">bypass ratio<\/a>. Engines with more <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Propelling_nozzle\" target=\"_blank\" rel=\"noreferrer noopener\">jet thrust<\/a> relative to fan thrust are known as <em>low-bypass turbofans<\/em>, those that have considerably more fan thrust than jet thrust are known as <em>high-bypass<\/em>. Most commercial aviation jet engines in use today are high-bypass,<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-Hall-2\" target=\"_blank\" rel=\"noreferrer noopener\">[2]<\/a><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-HackerBurghardt2009-3\" target=\"_blank\" rel=\"noreferrer noopener\">[3]<\/a> and most modern fighter engines are low-bypass.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-Verma2013-4\" target=\"_blank\" rel=\"noreferrer noopener\">[4]<\/a><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-Magill-5\" target=\"_blank\" rel=\"noreferrer noopener\">[5]<\/a> <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Afterburner\" target=\"_blank\" rel=\"noreferrer noopener\">Afterburners<\/a> are used on low-bypass turbofans on combat aircraft.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u65c1\u901a\u6bd4\u662f\u65c1\u901a\u53d1\u52a8\u673a\u6838\u5fc3\u901a\u8fc7\u7684\u7a7a\u6c14\u8d28\u91cf\u6d41\u91cf\u4e0e\u65c1\u901a\u53d1\u52a8\u673a\u6838\u5fc3\u901a\u8fc7\u7684\u7a7a\u6c14\u8d28\u91cf\u6d41\u91cf\u6bd4\u3002\u76f8\u5bf9\u4e8e\u98ce\u6247\u63a8\u529b\uff0c\u55b7\u6c14\u63a8\u529b\u66f4\u5927\u7684\u53d1\u52a8\u673a\u79f0\u4e3a\u4f4e\u65c1\u901a\u6da1\u55b7\u53d1\u52a8\u673a\uff0c\u800c\u76f8\u5bf9\u4e8e\u55b7\u6c14\u63a8\u529b\uff0c\u98ce\u6247\u63a8\u529b\u66f4\u5927\u7684\u53d1\u52a8\u673a\u5219\u79f0\u4e3a\u9ad8\u65c1\u901a\u55b7\u53d1\u52a8\u673a\u3002\u76ee\u524d\u4f7f\u7528\u7684\u5927\u591a\u6570\u5546\u7528\u822a\u7a7a\u55b7\u6c14\u53d1\u52a8\u673a\u90fd\u662f\u9ad8\u65c1\u901a\u6da1\u55b7\u53d1\u52a8\u673a\uff0c\u800c\u5927\u591a\u6570\u73b0\u4ee3\u6218\u6597\u673a\u53d1\u52a8\u673a\u5219\u662f\u4f4e\u65c1\u901a\u6da1\u55b7\u53d1\u52a8\u673a\u3002\u4f4e\u65c1\u901a\u6da1\u55b7\u53d1\u52a8\u673a\u4e0a\u7684\u52a0\u529b\u71c3\u70e7\u5668\u7528\u4e8e\u6218\u6597\u673a\u4e0a\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_2\">1.1 \u6db5\u9053\u6bd4\/\u65c1\u901a\u6bd4 | Bypass ratio<\/h3>\n\n\n\n<p><em>Main article: <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Bypass_ratio\" target=\"_blank\" rel=\"noreferrer noopener\">Bypass ratio<\/a><\/em><br><em>\u4e3b\u6761\u76ee\uff1a\u6db5\u9053\u6bd4\/\u65c1\u901a\u6bd4<\/em><\/p>\n\n\n\n<p>The <em>bypass ratio (BPR)<\/em> of a turbofan engine is the ratio between the mass flow rate of the bypass stream to the mass flow rate entering the core.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-13\" target=\"_blank\" rel=\"noreferrer noopener\">[13]<\/a> A bypass ratio of 6, for example, means that 6 times more air passes through the bypass duct than the amount that passes through the combustion chamber.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u65c1\u901a\u6bd4\uff08BPR\uff09\u662f\u6da1\u55b7\u53d1\u52a8\u673a\u4e2d\u65c1\u901a\u6d41\u7684\u8d28\u91cf\u6d41\u91cf\u4e0e\u8fdb\u5165\u6838\u5fc3\u7684\u8d28\u91cf\u6d41\u91cf\u4e4b\u95f4\u7684\u6bd4\u503c[13]\u3002\u4f8b\u5982\uff0c\u65c1\u901a\u6bd4\u4e3a6\u610f\u5473\u7740\u65c1\u901a\u7ba1\u4e2d\u901a\u8fc7\u7684\u7a7a\u6c14\u91cf\u662f\u901a\u8fc7\u71c3\u70e7\u5ba4\u901a\u8fc7\u7684\u7a7a\u6c14\u91cf\u76846\u500d\u3002<\/p>\n\n\n\n<p>Turbofan engines are usually described in terms of BPR, which together with overall pressure ratio, turbine inlet temperature and fan pressure ratio are important design parameters. In addition BPR is quoted for turboprop and unducted fan installations because their high propulsive efficiency gives them the overall efficiency characteristics of very high bypass turbofans. This allows them to be shown together with turbofans on plots which show trends of reducing <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Thrust-specific_fuel_consumption\" target=\"_blank\" rel=\"noreferrer noopener\">specific fuel consumption<\/a> (SFC) with increasing BPR.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-14\" target=\"_blank\" rel=\"noreferrer noopener\">[14]<\/a> BPR can also be quoted for lift fan installations where the fan airflow is remote from the engine and doesn&#8217;t flow past the engine core.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6da1\u6247\u53d1\u52a8\u673a\u901a\u5e38\u4ee5\u65c1\u901a\u6bd4\u3001\u603b\u538b\u6bd4\u3001\u6da1\u8f6e\u8fdb\u53e3\u6e29\u5ea6\u548c\u98ce\u6247\u538b\u6bd4\u7b49\u91cd\u8981\u8bbe\u8ba1\u53c2\u6570\u6765\u63cf\u8ff0\u3002\u6b64\u5916\uff0c\u65c1\u901a\u6bd4\u4e5f\u9002\u7528\u4e8e\u6da1\u6868\u548c\u975e\u5bfc\u6d41\u98ce\u6247\u88c5\u7f6e\uff0c\u56e0\u4e3a\u5b83\u4eec\u5177\u6709\u975e\u5e38\u9ad8\u7684\u63a8\u529b\u6548\u7387\uff0c\u53ef\u4ee5\u5177\u5907\u975e\u5e38\u9ad8\u7684\u65c1\u901a\u6da1\u55b7\u53d1\u52a8\u673a\u7684\u6574\u4f53\u6548\u7387\u7279\u6027\u3002\u8fd9\u4f7f\u5f97\u5b83\u4eec\u53ef\u4ee5\u4e0e\u6da1\u55b7\u53d1\u52a8\u673a\u4e00\u8d77\u663e\u793a\u5728\u663e\u793a\u968f\u7740\u65c1\u901a\u6bd4\u589e\u52a0\u800c\u964d\u4f4e\u6bd4\u6cb9\u8017\u7684\u8d8b\u52bf\u7684\u56fe\u8868\u4e0a[14]\u3002\u5bf9\u4e8e\u5347\u529b\u98ce\u6247\u88c5\u7f6e\uff0c\u65c1\u901a\u6bd4\u4e5f\u53ef\u4ee5\u4f5c\u4e3a\u5f15\u7528\uff0c\u5176\u4e2d\u98ce\u6247\u6c14\u6d41\u4e0e\u53d1\u52a8\u673a\u76f8\u9694\u4e00\u6bb5\u8ddd\u79bb\uff0c\u5e76\u4e0d\u7ecf\u8fc7\u53d1\u52a8\u673a\u6838\u5fc3\u3002<\/p>\n\n\n\n<p>Considering a constant core (ie fixed pressure ratio and turbine inlet temperature), core and bypass jet velocities equal and a particular flight condition (ie Mach number and altitude) the fuel consumption per lb of thrust (sfc) decreases with increase in BPR. At the same time gross and net thrusts increase, but by different amounts.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-15\" target=\"_blank\" rel=\"noreferrer noopener\">[15]<\/a> There is considerable potential for reducing fuel consumption for the same core cycle by increasing BPR.This is achieved because of the reduction in pounds of thrust per lb\/sec of airflow (specific thrust) and the resultant reduction in lost kinetic energy in the jets (increase in propulsive efficiency).<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-16\" target=\"_blank\" rel=\"noreferrer noopener\">[16]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u5728\u6838\u5fc3\u6052\u5b9a\uff08\u5373\u538b\u529b\u6bd4\u548c\u6da1\u8f6e\u8fdb\u53e3\u6e29\u5ea6\u56fa\u5b9a\uff09\u3001\u6838\u5fc3\u548c\u65c1\u901a\u55b7\u6d41\u901f\u5ea6\u76f8\u7b49\u4ee5\u53ca\u7279\u5b9a\u7684\u98de\u884c\u6761\u4ef6\uff08\u5373\u9a6c\u8d6b\u6570\u548c\u9ad8\u5ea6\uff09\u4e0b\uff0c\u6bcf\u78c5\u63a8\u529b\u7684\u71c3\u6cb9\u6d88\u8017\uff08\u6bd4\u6cb9\u8017\uff09\u968f\u7740\u65c1\u901a\u6bd4\u7684\u589e\u52a0\u800c\u51cf\u5c11\u3002\u540c\u65f6\uff0c\u603b\u63a8\u529b\u548c\u51c0\u63a8\u529b\u90fd\u4f1a\u589e\u52a0\uff0c\u4f46\u589e\u52a0\u7684\u5e45\u5ea6\u4e0d\u540c[15]\u3002\u901a\u8fc7\u589e\u52a0\u65c1\u901a\u6bd4\uff0c\u53ef\u4ee5\u5927\u5e45\u964d\u4f4e\u76f8\u540c\u6838\u5fc3\u5faa\u73af\u7684\u71c3\u6cb9\u6d88\u8017\u3002\u8fd9\u662f\u56e0\u4e3a\u6bcf\u79d2\u7a7a\u6c14\u6d41\u91cf\u7684\u78c5\u63a8\u529b\uff08\u6bd4\u63a8\u529b\uff09\u51cf\u5c11\uff0c\u55b7\u6d41\u4e2d\u5931\u53bb\u7684\u52a8\u80fd\u51cf\u5c11\uff08\u63a8\u529b\u6548\u7387\u589e\u52a0\uff09[16]\u3002<\/p>\n\n\n\n<p>If all the gas power from a gas turbine is converted to kinetic energy in a propelling nozzle, the aircraft is best suited to high supersonic speeds. If it is all transferred to a separate big mass of air with low kinetic energy, the aircraft is best suited to zero speed (hovering). For speeds in between, the gas power is shared between a separate airstream and the gas turbine&#8217;s own nozzle flow in a proportion which gives the aircraft performance required. The trade off between mass flow and velocity is also seen with propellers and helicopter rotors by comparing disc loading and power loading.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-17\" target=\"_blank\" rel=\"noreferrer noopener\">[17]<\/a> For example, the same helicopter weight can be supported by a high power engine and small diameter rotor or, for less fuel, a lower power engine and bigger rotor with lower velocity through the rotor.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5982\u679c\u5c06\u71c3\u6c14\u6da1\u8f6e\u4e2d\u7684\u6240\u6709\u6c14\u4f53\u529f\u7387\u8f6c\u5316\u4e3a\u63a8\u8fdb\u55b7\u7ba1\u4e2d\u7684\u52a8\u80fd\uff0c\u98de\u673a\u6700\u9002\u5408\u9ad8\u8d85\u97f3\u901f\u98de\u884c\u3002\u5982\u679c\u5c06\u6240\u6709\u6c14\u4f53\u529f\u7387\u8f6c\u79fb\u5230\u5177\u6709\u4f4e\u52a8\u80fd\u7684\u72ec\u7acb\u5927\u6c14\u56e2\u4e2d\uff0c\u98de\u673a\u6700\u9002\u5408\u96f6\u901f\uff08\u60ac\u505c\uff09\u3002\u5bf9\u4e8e\u4e2d\u95f4\u901f\u5ea6\uff0c\u6c14\u4f53\u529f\u7387\u5728\u72ec\u7acb\u7684\u6c14\u6d41\u548c\u71c3\u6c14\u6da1\u8f6e\u7684\u55b7\u7ba1\u6d41\u4e4b\u95f4\u6309\u6bd4\u4f8b\u5171\u4eab\uff0c\u4ee5\u83b7\u5f97\u6240\u9700\u7684\u98de\u673a\u6027\u80fd\u3002\u901a\u8fc7\u6bd4\u8f83\u76d8\u9762\u8d1f\u8f7d\u548c\u529f\u7387\u8d1f\u8f7d\uff0c\u53ef\u4ee5\u770b\u5230\u63a8\u8fdb\u5668\u548c\u76f4\u5347\u673a\u65cb\u7ffc\u7684\u8d28\u91cf\u6d41\u91cf\u548c\u901f\u5ea6\u4e4b\u95f4\u7684\u6743\u8861[17]\u3002\u4f8b\u5982\uff0c\u76f8\u540c\u7684\u76f4\u5347\u673a\u91cd\u91cf\u53ef\u4ee5\u901a\u8fc7\u9ad8\u529f\u7387\u53d1\u52a8\u673a\u548c\u5c0f\u76f4\u5f84\u65cb\u7ffc\u652f\u6491\uff0c\u4e5f\u53ef\u4ee5\u901a\u8fc7\u529f\u7387\u8f83\u4f4e\u7684\u53d1\u52a8\u673a\u548c\u66f4\u5927\u76f4\u5f84\u3001\u65cb\u7ffc\u901f\u5ea6\u8f83\u4f4e\u7684\u65cb\u7ffc\u6765\u652f\u6491\uff0c\u4ee5\u51cf\u5c11\u71c3\u6599\u6d88\u8017\u3002<\/p>\n\n\n\n<p>Bypass usually refers to transferring gas power from a gas turbine to a bypass stream of air to reduce fuel consumption and jet noise. Alternatively, there may be a requirement for an afterburning engine where the sole requirement for bypass is to provide cooling air. This sets the lower limit for BPR and these engines have been called &#8220;leaky&#8221; or continuous bleed turbojets<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-18\" target=\"_blank\" rel=\"noreferrer noopener\">[18]<\/a> (General Electric YJ-101 BPR 0.25) and low BPR turbojets<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-19\" target=\"_blank\" rel=\"noreferrer noopener\">[19]<\/a> (Pratt &amp; Whitney PW1120). Low BPR (0.2) has also been used to provide surge margin as well as afterburner cooling for the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_J58\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney J58<\/a>.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-20\" target=\"_blank\" rel=\"noreferrer noopener\">[20]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u65c1\u901a\u901a\u5e38\u6307\u5c06\u71c3\u6c14\u6da1\u8f6e\u4e2d\u7684\u6c14\u4f53\u529f\u7387\u8f6c\u79fb\u5230\u65c1\u901a\u6c14\u6d41\u4e2d\uff0c\u4ee5\u51cf\u5c11\u71c3\u6599\u6d88\u8017\u548c\u55b7\u6c14\u566a\u97f3\u3002\u53e6\u5916\uff0c\u53ef\u80fd\u8fd8\u6709\u5bf9\u52a0\u529b\u53d1\u52a8\u673a\u7684\u9700\u6c42\uff0c\u5176\u65c1\u901a\u7684\u552f\u4e00\u8981\u6c42\u662f\u63d0\u4f9b\u51b7\u5374\u7a7a\u6c14\u3002\u8fd9\u4e3a\u65c1\u901a\u6bd4\u8bbe\u5b9a\u4e86\u4e0b\u9650\uff0c\u8fd9\u4e9b\u53d1\u52a8\u673a\u88ab\u79f0\u4e3a\u201c\u6cc4\u6f0f\u201d\u6216\u8fde\u7eed\u6cc4\u6f0f\u6da1\u6c14\u55b7\u6c14\u53d1\u52a8\u673a[18]\uff08\u901a\u7528\u7535\u6c14YJ-101\uff0c\u65c1\u901a\u6bd4\u4e3a0.25\uff09\u548c\u4f4e\u65c1\u901a\u6bd4\u55b7\u6c14\u53d1\u52a8\u673a[19]\uff08\u666e\u60e0PW1120\uff09\u3002\u4f4e\u65c1\u901a\u6bd4\uff080.2\uff09\u4e5f\u7528\u4e8e\u4e3a\u666e\u60e0J58\u63d0\u4f9b\u6da1\u524d\u88d5\u5ea6\u4ee5\u53ca\u52a0\u529b\u71c3\u70e7\u5ba4\u51b7\u5374[20]\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_3\">1.2 \u80fd\u6548 | Efficiency<\/h3>\n\n\n\n<div class=\"wp-block-buttons is-layout-flex wp-block-buttons-is-layout-flex\">\n<div class=\"wp-block-button\"><a class=\"wp-block-button__link wp-element-button\" href=\"https:\/\/www.zhihu.com\/pin\/1849397327292407810\">\u56fe1-2\uff08\u53d1\u5e03\u4e8e\u77e5\u4e4e\u60f3\u6cd5\uff09<\/a><\/div>\n<\/div>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Propeller_%28aeronautics%29\" target=\"_blank\" rel=\"noreferrer noopener\">Propeller<\/a> engines are most efficient for low speeds, <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbojet\" target=\"_blank\" rel=\"noreferrer noopener\">turbojet<\/a> engines for high speeds, and turbofan engines between the two. Turbofans are the most efficient engines in the range of speeds from about 500 to 1,000 km\/h (270 to 540 kn; 310 to 620 mph), the speed at which most commercial aircraft operate.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-grc_nasa-21\" target=\"_blank\" rel=\"noreferrer noopener\">[21]<\/a><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-Neumann_2004_1984_pp228-230-22\" target=\"_blank\" rel=\"noreferrer noopener\">[22]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u87ba\u65cb\u6868\u53d1\u52a8\u673a\u5728\u4f4e\u901f\u4e0b\u6548\u7387\u6700\u9ad8\uff0c\u6da1\u55b7\u53d1\u52a8\u673a\u5728\u9ad8\u901f\u4e0b\u6548\u7387\u6700\u9ad8\uff0c\u800c\u6da1\u6247\u53d1\u52a8\u673a\u5219\u4ecb\u4e8e\u4e24\u8005\u4e4b\u95f4\u3002\u6da1\u6247\u53d1\u52a8\u673a\u5728\u5927\u7ea6500\u52301,000\u516c\u91cc\/\u5c0f\u65f6\uff08270\u5230540\u8282\uff1b310\u5230620\u82f1\u91cc\/\u5c0f\u65f6\uff09\u7684\u901f\u5ea6\u8303\u56f4\u5185\u662f\u6700\u9ad8\u6548\u7684\u53d1\u52a8\u673a\uff0c\u8fd9\u4e5f\u662f\u5927\u591a\u6570\u5546\u7528\u98de\u673a\u8fd0\u884c\u7684\u901f\u5ea6[21][22]\u3002<\/p>\n\n\n\n<p>In a turbojet (zero-bypass) engine, the high temperature and high pressure exhaust gas is accelerated when it undergoes expansion through a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Propelling_nozzle\" target=\"_blank\" rel=\"noreferrer noopener\">propelling nozzle<\/a> and produces all the thrust. The compressor absorbs the mechanical power produced by the turbine. In a bypass design, extra turbines drive a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Ducted_fan\" target=\"_blank\" rel=\"noreferrer noopener\">ducted fan<\/a> that accelerates air rearward from the front of the engine. In a high-bypass design, the ducted fan and nozzle produce most of the thrust. Turbofans are closely related to <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turboprop\" target=\"_blank\" rel=\"noreferrer noopener\">turboprops<\/a> in principle because both transfer some of the gas turbine&#8217;s gas power, using extra machinery, to a bypass stream leaving less for the hot nozzle to convert to kinetic energy. Turbofans represent an intermediate stage between <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbojet\" target=\"_blank\" rel=\"noreferrer noopener\">turbojets<\/a>, which derive all their thrust from exhaust gases, and turbo-props which derive minimal thrust from exhaust gases (typically 10% or less).<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-srm-23\" target=\"_blank\" rel=\"noreferrer noopener\">[23]<\/a> Extracting shaft power and transferring it to a bypass stream introduces extra losses which are more than made up by the improved propulsive efficiency. The turboprop at its best flight speed gives significant fuel savings over a turbojet even though an extra turbine, a gearbox and a propeller are added to the turbojet&#8217;s low-loss propelling nozzle.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-24\" target=\"_blank\" rel=\"noreferrer noopener\">[24]<\/a> The turbofan has additional losses from its greater number of compressor stages\/blades, fan and bypass duct.[<em><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Wikipedia%3APlease_clarify\" target=\"_blank\" rel=\"noreferrer noopener\">clarification needed<\/a><\/em>]<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5728\u6da1\u55b7\uff08\u96f6\u65c1\u901a\u6bd4\uff09\u53d1\u52a8\u673a\u4e2d\uff0c\u9ad8\u6e29\u9ad8\u538b\u7684\u6392\u6c14\u7ecf\u8fc7\u55b7\u5c04\u55b7\u5634\u81a8\u80c0\u65f6\u52a0\u901f\uff0c\u5e76\u4ea7\u751f\u6240\u6709\u7684\u63a8\u529b\u3002\u538b\u6c14\u673a\u5438\u6536\u6da1\u8f6e\u4ea7\u751f\u7684\u673a\u68b0\u529f\u7387\u3002\u5728\u65c1\u901a\u8bbe\u8ba1\u4e2d\uff0c\u989d\u5916\u7684\u6da1\u8f6e\u9a71\u52a8\u4e00\u4e2a\u5bfc\u6d41\u98ce\u6247\uff0c\u4ece\u53d1\u52a8\u673a\u524d\u90e8\u5411\u540e\u52a0\u901f\u7a7a\u6c14\u3002\u5728\u9ad8\u65c1\u901a\u6bd4\u8bbe\u8ba1\u4e2d\uff0c\u5bfc\u6d41\u98ce\u6247\u548c\u55b7\u5634\u4ea7\u751f\u5927\u90e8\u5206\u7684\u63a8\u529b\u3002\u6da1\u6247\u53d1\u52a8\u673a\u4e0e\u6da1\u8f74\u87ba\u65cb\u6868\u53d1\u52a8\u673a\u5728\u539f\u7406\u4e0a\u5bc6\u5207\u76f8\u5173\uff0c\u56e0\u4e3a\u4e24\u8005\u90fd\u4f7f\u7528\u989d\u5916\u7684\u673a\u68b0\u88c5\u7f6e\u5c06\u90e8\u5206\u71c3\u6c14\u6da1\u8f6e\u7684\u529f\u7387\u8f6c\u79fb\u5230\u65c1\u901a\u6c14\u6d41\u4e2d\uff0c\u4ece\u800c\u51cf\u5c11\u4e86\u70ed\u55b7\u5634\u5c06\u5176\u8f6c\u5316\u4e3a\u52a8\u80fd\u7684\u80fd\u91cf\u3002\u6da1\u6247\u53d1\u52a8\u673a\u5904\u4e8e\u6da1\u55b7\u53d1\u52a8\u673a\u5b8c\u5168\u4f9d\u9760\u6392\u6c14\u6c14\u4f53\u4ea7\u751f\u63a8\u529b\u548c\u6da1\u8f74\u87ba\u65cb\u6868\u53d1\u52a8\u673a\u4ec5\u5728\u5c11\u91cf\u7a0b\u5ea6\u4e0a\u4f9d\u9760\u6392\u6c14\u6c14\u4f53\u4ea7\u751f\u63a8\u529b\u4e4b\u95f4\u7684\u4e2d\u95f4\u9636\u6bb5[23]\u3002\u63d0\u53d6\u8f74\u529f\u5e76\u5c06\u5176\u8f6c\u79fb\u5230\u65c1\u901a\u6c14\u6d41\u4e2d\u4f1a\u5f15\u5165\u989d\u5916\u7684\u635f\u5931\uff0c\u4f46\u8fd9\u4e9b\u635f\u5931\u88ab\u63d0\u9ad8\u7684\u63a8\u8fdb\u6548\u7387\u6240\u5f25\u8865\u3002\u5728\u6700\u4f73\u98de\u884c\u901f\u5ea6\u4e0b\uff0c\u6da1\u8f74\u87ba\u65cb\u6868\u53d1\u52a8\u673a\u7684\u71c3\u6599\u8282\u7ea6\u660e\u663e\u4f18\u4e8e\u6da1\u55b7\u53d1\u52a8\u673a\uff0c\u5373\u4f7f\u6da1\u55b7\u53d1\u52a8\u673a\u7684\u4f4e\u635f\u5931\u55b7\u5c04\u55b7\u5634\u9700\u8981\u589e\u52a0\u989d\u5916\u7684\u6da1\u8f6e\u3001\u9f7f\u8f6e\u7bb1\u548c\u87ba\u65cb\u6868[24]\u3002\u6da1\u6247\u53d1\u52a8\u673a\u7531\u4e8e\u5176\u8f83\u591a\u7684\u538b\u6c14\u673a\u7ea7\u6570\/\u53f6\u7247\u3001\u98ce\u6247\u548c\u65c1\u901a\u5bfc\u6d41\u7ba1\u800c\u4ea7\u751f\u989d\u5916\u7684\u635f\u5931[\u9700\u8981\u6f84\u6e05]\u3002<\/p>\n\n\n\n<p>Froude, or propulsive, efficiency can be defined as:<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5f17\u52b3\u5fb7\u6548\u7387\uff08Froude efficiency\uff09\uff0c\u53c8\u79f0\u63a8\u8fdb\u6548\u7387\uff0c\u53ef\u4ee5\u5b9a\u4e49\u4e3a\uff1a<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/pic2.zhimg.com\/80\/v2-4b000ce30fbe5192b6253f9396c5a23d_720w.webp\" alt=\"\"\/><\/figure>\n\n\n\n<p>where:<br>\u5728\u8fd9\u91cc\uff1a<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>Vj = thrust equivalent jet velocity<br>Vj\u4ee3\u8868\u63a8\u529b\u7b49\u6548\u55b7\u6d41\u901f\u5ea6\u3002<\/li>\n\n\n\n<li>Va = aircraft velocity<br>Va\u4ee3\u8868\u98de\u673a\u901f\u5ea6\u3002<\/li>\n<\/ul>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_4\">1.3 \u63a8\u529b | Thrust<\/h3>\n\n\n\n<p>While a turbojet engine uses all of the engine&#8217;s output to produce thrust in the form of a hot high-velocity exhaust gas jet, a turbofan&#8217;s cool low-velocity bypass air yields between 30% and 70% of the total thrust produced by a turbofan system.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-25\" target=\"_blank\" rel=\"noreferrer noopener\">[25]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u5f53\u6da1\u55b7\u53d1\u52a8\u673a\u5c06\u5176\u6240\u6709\u8f93\u51fa\u7528\u4e8e\u4ea7\u751f\u9ad8\u901f\u70ed\u6392\u6c14\u55b7\u6d41\u5f62\u5f0f\u7684\u63a8\u529b\u65f6\uff0c\u6da1\u6247\u53d1\u52a8\u673a\u7684\u51b7\u4f4e\u901f\u526f\u6d41\u6c14\u4f53\u4ea7\u751f\u4e86\u6da1\u6247\u7cfb\u7edf\u603b\u63a8\u529b\u768430%\u81f370%\u3002<\/p>\n\n\n\n<p>The thrust (<em><strong>FN<\/strong><\/em>) generated by a turbofan depends on the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Effective_exhaust_velocity\" target=\"_blank\" rel=\"noreferrer noopener\">effective exhaust velocity<\/a> of the total exhaust, as with any jet engine, but because two exhaust jets are present the thrust equation can be expanded as:<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-26\" target=\"_blank\" rel=\"noreferrer noopener\">[26]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u6da1\u6247\u53d1\u52a8\u673a\u4ea7\u751f\u7684\u63a8\u529b\uff08FN\uff09\u53d6\u51b3\u4e8e\u603b\u6392\u6c14\u7684\u6709\u6548\u6392\u6c14\u901f\u5ea6\uff0c\u5c31\u50cf\u4efb\u4f55\u55b7\u6c14\u53d1\u52a8\u673a\u4e00\u6837\uff0c\u4f46\u7531\u4e8e\u5b58\u5728\u4e24\u4e2a\u6392\u6c14\u55b7\u6d41\uff0c\u63a8\u529b\u65b9\u7a0b\u53ef\u4ee5\u6269\u5c55\u4e3a\uff1a<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/pic3.zhimg.com\/80\/v2-3623639a4c5734511482e988e55278a6_720w.webp\" alt=\"\"\/><\/figure>\n\n\n\n<p>where:<br>\u5728\u8fd9\u91cc\uff1a<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>me = the mass rate of hot combustion exhaust flow from the core engine<br>me\u4ee3\u8868\u4ece\u6838\u5fc3\u53d1\u52a8\u673a\u6392\u51fa\u7684\u71c3\u70e7\u70ed\u6392\u6c14\u6d41\u7684\u8d28\u91cf\u6d41\u7387\u3002<\/li>\n\n\n\n<li>mo = the mass rate of total air flow entering the turbofan = \u2022mc + \u2022mf<br>mo\u4ee3\u8868\u8fdb\u5165\u6da1\u6247\u53d1\u52a8\u673a\u7684\u603b\u7a7a\u6c14\u6d41\u91cf\u7684\u8d28\u91cf\u6d41\u7387\uff0c\u5373mo = mc + mf\uff0c\u5176\u4e2dmc\u8868\u793a\u4ece\u6838\u5fc3\u53d1\u52a8\u673a\u8fdb\u5165\u7684\u7a7a\u6c14\u8d28\u91cf\u6d41\u7387\uff0cmf\u8868\u793a\u4ece\u98ce\u6247\u8fdb\u5165\u7684\u7a7a\u6c14\u8d28\u91cf\u6d41\u7387\u3002<\/li>\n\n\n\n<li>mc = the mass rate of intake air that flows to the core engine<br>mc\u8868\u6d41\u5411\u6838\u5fc3\u53d1\u52a8\u673a\u7684\u8fdb\u6c14\u7a7a\u6c14\u7684\u8d28\u91cf\u6d41\u91cf\u3002<\/li>\n\n\n\n<li>mf = the mass rate of intake air that bypasses the core engine<br>mf\u4ee3\u8868\u7ed5\u8fc7\u6838\u5fc3\u53d1\u52a8\u673a\u7684\u8fdb\u6c14\u7a7a\u6c14\u7684\u8d28\u91cf\u6d41\u91cf\u3002<\/li>\n\n\n\n<li>vf = the velocity of the air flow bypassed around the core engine<br>vf\u8868\u793a\u7ed5\u8fc7\u6838\u5fc3\u53d1\u52a8\u673a\u7684\u7a7a\u6c14\u6d41\u52a8\u7684\u901f\u5ea6\u3002<\/li>\n\n\n\n<li>vhe = the velocity of the hot exhaust gas from the core engine<br>vhe\u4ee3\u8868\u6838\u5fc3\u53d1\u52a8\u673a\u6392\u51fa\u7684\u70ed\u6392\u6c14\u6c14\u4f53\u7684\u901f\u5ea6\u3002<\/li>\n\n\n\n<li>vo = the velocity of the total air intake = the true airspeed of the aircraft<br>vo\u4ee3\u8868\u603b\u8fdb\u6c14\u901f\u5ea6\uff0c\u4e5f\u53ef\u4ee5\u7406\u89e3\u4e3a\u98de\u673a\u7684\u771f\u7a7a\u901f\u3002<\/li>\n\n\n\n<li><em>BPR<\/em> = bypass ratio<br>\u65c1\u901a\u6bd4\uff08\u6db5\u9053\u6bd4\uff09<\/li>\n<\/ul>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_5\">1.4 Nozzles | \u55b7\u5634<\/h3>\n\n\n\n<p>The cold duct and core duct&#8217;s nozzle systems are relatively complex due to the use of two separate exhaust flows. In high bypass engines, the fan is situated in a short duct near the front of the engine and typically has a convergent cold nozzle, with the tail of the duct forming a low pressure ratio nozzle that under normal conditions will choke creating supersonic flow patterns around the core[<em><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Wikipedia%3ACitation_needed\" target=\"_blank\" rel=\"noreferrer noopener\">citation needed<\/a><\/em>]. The core nozzle is more conventional, but generates less of the thrust, and depending on design choices, such as noise considerations, may conceivably not choke.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-27\" target=\"_blank\" rel=\"noreferrer noopener\">[27]<\/a> In low bypass engines the two flows may combine within the ducts, and share a common nozzle, which can be fitted with afterburner.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u7531\u4e8e\u4f7f\u7528\u4e86\u4e24\u4e2a\u5355\u72ec\u7684\u6392\u6c14\u6d41\uff0c\u51b7\u6c14\u9053\u548c\u6838\u5fc3\u6c14\u9053\u7684\u55b7\u7ba1\u7cfb\u7edf\u76f8\u5bf9\u590d\u6742\u3002\u5728\u9ad8\u526f\u63a8\u53d1\u52a8\u673a\u4e2d\uff0c\u98ce\u6247\u4f4d\u4e8e\u53d1\u52a8\u673a\u524d\u90e8\u9644\u8fd1\u7684\u4e00\u4e2a\u77ed\u6c14\u9053\u5185\uff0c\u901a\u5e38\u5177\u6709\u6536\u655b\u7684\u51b7\u55b7\u7ba1\uff0c\u800c\u6c14\u9053\u5c3e\u90e8\u5f62\u6210\u4e00\u4e2a\u4f4e\u538b\u6bd4\u55b7\u7ba1\uff0c\u5728\u6b63\u5e38\u60c5\u51b5\u4e0b\u4f1a\u7a92\u606f\uff0c\u5f62\u6210\u7ed5\u8fc7\u6838\u5fc3\u7684\u8d85\u97f3\u901f\u6d41\u52a8\u6a21\u5f0f[\u9700\u8981\u5f15\u8bc1]\u3002\u6838\u5fc3\u55b7\u7ba1\u6bd4\u8f83\u4f20\u7edf\uff0c\u4f46\u4ea7\u751f\u7684\u63a8\u529b\u8f83\u5c0f\uff0c\u6839\u636e\u8bbe\u8ba1\u9009\u62e9\uff0c\u5982\u566a\u97f3\u8003\u8651\uff0c\u53ef\u80fd\u4e0d\u4f1a\u7a92\u606f[27]\u3002\u5728\u4f4e\u526f\u63a8\u53d1\u52a8\u673a\u4e2d\uff0c\u4e24\u4e2a\u6d41\u52a8\u53ef\u4ee5\u5728\u6c14\u9053\u5185\u5408\u5e76\uff0c\u5e76\u5171\u7528\u4e00\u4e2a\u55b7\u7ba1\uff0c\u8be5\u55b7\u7ba1\u53ef\u4ee5\u5b89\u88c5\u52a0\u529b\u71c3\u70e7\u5668\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_6\">1.5 Noise | \u566a\u97f3<\/h3>\n\n\n\n<div class=\"wp-block-buttons is-layout-flex wp-block-buttons-is-layout-flex\">\n<div class=\"wp-block-button\"><a class=\"wp-block-button__link wp-element-button\" href=\"https:\/\/www.zhihu.com\/pin\/1849397052548714497\">\u56fe1-3\uff08\u53d1\u5e03\u4e8e\u77e5\u4e4e\u60f3\u6cd5\uff09<\/a><\/div>\n<\/div>\n\n\n\n<p>Most of the air flow through a high-bypass turbofan is lower-velocity bypass flow: even when combined with the much-higher-velocity engine exhaust, the average exhaust velocity is considerably lower than in a pure turbojet. Turbojet engine noise is predominately <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Jet_noise\" target=\"_blank\" rel=\"noreferrer noopener\">jet noise<\/a> from the high exhaust velocity. Therefore, turbofan engines are significantly quieter than a pure-jet of the same thrust, and jet noise is no longer the predominant source.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-Kempton2011-28\" target=\"_blank\" rel=\"noreferrer noopener\">[28]<\/a> Turbofan engine noise propagates both upstream via the inlet and downstream via the primary nozzle and the by-pass duct. Other noise sources are the fan, compressor and turbine.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-29\" target=\"_blank\" rel=\"noreferrer noopener\">[29]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u9ad8\u526f\u63a8\u6da1\u6247\u53d1\u52a8\u673a\u4e2d\u7684\u5927\u90e8\u5206\u7a7a\u6c14\u6d41\u52a8\u662f\u4f4e\u901f\u7ed5\u6d41\uff1a\u5373\u4f7f\u4e0e\u9ad8\u901f\u53d1\u52a8\u673a\u6392\u6c14\u76f8\u7ed3\u5408\uff0c\u5e73\u5747\u6392\u6c14\u901f\u5ea6\u8fdc\u4f4e\u4e8e\u7eaf\u6da1\u55b7\u53d1\u52a8\u673a\u3002\u6da1\u55b7\u53d1\u52a8\u673a\u7684\u566a\u97f3\u4e3b\u8981\u6765\u81ea\u9ad8\u901f\u6392\u6c14\u7684\u55b7\u6c14\u566a\u97f3\u3002\u56e0\u6b64\uff0c\u4e0e\u76f8\u540c\u63a8\u529b\u7684\u7eaf\u55b7\u6c14\u53d1\u52a8\u673a\u76f8\u6bd4\uff0c\u6da1\u6247\u53d1\u52a8\u673a\u7684\u566a\u97f3\u660e\u663e\u8f83\u4f4e\uff0c\u55b7\u6c14\u566a\u97f3\u4e0d\u518d\u662f\u4e3b\u8981\u7684\u566a\u97f3\u6e90[28]\u3002\u6da1\u6247\u53d1\u52a8\u673a\u7684\u566a\u97f3\u901a\u8fc7\u8fdb\u6c14\u53e3\u5411\u4e0a\u6e38\u4f20\u64ad\uff0c\u5e76\u901a\u8fc7\u4e3b\u55b7\u7ba1\u548c\u65c1\u901a\u7ba1\u5411\u4e0b\u6e38\u4f20\u64ad\u3002\u5176\u4ed6\u566a\u97f3\u6e90\u5305\u62ec\u98ce\u6247\u3001\u538b\u6c14\u673a\u548c\u6da1\u8f6e[29]\u3002<\/p>\n\n\n\n<p>Modern commercial aircraft employ high-bypass-ratio (HBPR) engines with separate flow, non-mixing, short-duct exhaust systems. Their noise is due to the speed, temperature, and pressure of the exhaust jet, especially during high-thrust conditions, such as those required for takeoff. The primary source of jet noise is the turbulent mixing of shear layers in the engine&#8217;s exhaust. These shear layers contain instabilities that lead to highly turbulent vortices that generate the pressure fluctuations responsible for sound. To reduce the noise associated with jet flow, the aerospace industry has sought to disrupt shear layer turbulence and reduce the overall noise produced.[<em><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Wikipedia%3ACitation_needed\" target=\"_blank\" rel=\"noreferrer noopener\">citation needed<\/a><\/em>]<br>\u53c2\u8003\u8bd1\u6587\uff1a\u73b0\u4ee3\u5546\u7528\u98de\u673a\u91c7\u7528\u9ad8\u526f\u63a8\u6bd4\uff08HBPR\uff09\u53d1\u52a8\u673a\uff0c\u5177\u6709\u5355\u72ec\u6d41\u52a8\u3001\u975e\u6df7\u5408\u3001\u77ed\u6c14\u9053\u6392\u6c14\u7cfb\u7edf\u3002\u5b83\u4eec\u7684\u566a\u97f3\u662f\u7531\u6392\u6c14\u55b7\u6d41\u7684\u901f\u5ea6\u3001\u6e29\u5ea6\u548c\u538b\u529b\u5f15\u8d77\u7684\uff0c\u7279\u522b\u662f\u5728\u9700\u8981\u9ad8\u63a8\u529b\u7684\u60c5\u51b5\u4e0b\uff0c\u6bd4\u5982\u8d77\u98de\u65f6\u3002\u55b7\u6c14\u566a\u97f3\u7684\u4e3b\u8981\u6765\u6e90\u662f\u53d1\u52a8\u673a\u6392\u6c14\u4e2d\u7684\u526a\u5207\u5c42\u7684\u6e4d\u6d41\u6df7\u5408\u3002\u8fd9\u4e9b\u526a\u5207\u5c42\u5305\u542b\u4e0d\u7a33\u5b9a\u6027\uff0c\u5bfc\u81f4\u9ad8\u5ea6\u6e4d\u6d41\u7684\u6da1\u65cb\u4ea7\u751f\u538b\u529b\u6ce2\u52a8\uff0c\u4ece\u800c\u4ea7\u751f\u58f0\u97f3\u3002\u4e3a\u4e86\u51cf\u5c11\u4e0e\u55b7\u6d41\u76f8\u5173\u7684\u566a\u97f3\uff0c\u822a\u7a7a\u822a\u5929\u5de5\u4e1a\u4e00\u76f4\u5728\u5bfb\u6c42\u7834\u574f\u526a\u5207\u5c42\u6e4d\u6d41\u5e76\u51cf\u5c11\u603b\u4f53\u566a\u97f3\u7684\u65b9\u6cd5[\u9700\u8981\u5f15\u8bc1]\u3002<\/p>\n\n\n\n<p>Fan noise may come from the interaction of the fan-blade wakes with the pressure field of the downstream fan-exit stator vanes. It may be minimized by adequate axial spacing between blade trailing edge and stator entrance.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-30\" target=\"_blank\" rel=\"noreferrer noopener\">[30]<\/a> At high engine speeds, as at takeoff, shock waves from the supersonic fan tips, because of their unequal nature, produce noise of a discordant nature known as &#8220;buzz saw&#8221; noise.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-31\" target=\"_blank\" rel=\"noreferrer noopener\">[31]<\/a><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-buzz_saw-32\" target=\"_blank\" rel=\"noreferrer noopener\">[32]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u98ce\u6247\u566a\u97f3\u53ef\u80fd\u6765\u81ea\u98ce\u6247\u53f6\u7247\u5c3e\u8ff9\u4e0e\u4e0b\u6e38\u98ce\u6247\u51fa\u53e3\u5b9a\u5411\u53f6\u7247\u7684\u538b\u529b\u573a\u7684\u76f8\u4e92\u4f5c\u7528\u3002\u901a\u8fc7\u5728\u53f6\u7247\u5c3e\u7f18\u548c\u5b9a\u5411\u53f6\u7247\u8fdb\u53e3\u4e4b\u95f4\u4fdd\u6301\u8db3\u591f\u7684\u8f74\u5411\u95f4\u8ddd\uff0c\u53ef\u4ee5\u5c06\u5176\u6700\u5c0f\u5316[30]\u3002\u5728\u9ad8\u8f6c\u901f\u4e0b\uff0c\u6bd4\u5982\u8d77\u98de\u65f6\uff0c\u7531\u4e8e\u8d85\u97f3\u901f\u98ce\u6247\u53f6\u5c16\u7684\u4e0d\u5747\u5300\u6027\uff0c\u4f1a\u4ea7\u751f\u4e0d\u548c\u8c10\u7684\u566a\u97f3\uff0c\u88ab\u79f0\u4e3a\u201c\u952f\u9f7f\u566a\u97f3\u201d[31][32]\u3002<\/p>\n\n\n\n<p>All modern turbofan engines have <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Acoustic_liner\" target=\"_blank\" rel=\"noreferrer noopener\">acoustic liners<\/a> in the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Nacelle\" target=\"_blank\" rel=\"noreferrer noopener\">nacelle<\/a> to damp their noise. They extend as much as possible to cover the largest surface area. The acoustic performance of the engine can be experimentally evaluated by means of ground tests<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-Schuster2010-33\" target=\"_blank\" rel=\"noreferrer noopener\">[33]<\/a> or in dedicated experimental test rigs.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-Ferrante2011-34\" target=\"_blank\" rel=\"noreferrer noopener\">[34]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u6240\u6709\u73b0\u4ee3\u6da1\u6247\u53d1\u52a8\u673a\u90fd\u5728\u53d1\u52a8\u673a\u8231\u58f3\u4e2d\u88c5\u6709\u58f0\u5b66\u886c\u677f\uff0c\u7528\u4e8e\u51cf\u632f\u566a\u97f3\u3002\u5b83\u4eec\u5c3d\u53ef\u80fd\u5730\u5ef6\u4f38\u4ee5\u8986\u76d6\u6700\u5927\u7684\u8868\u9762\u79ef\u3002\u53d1\u52a8\u673a\u7684\u58f0\u5b66\u6027\u80fd\u53ef\u4ee5\u901a\u8fc7\u5730\u9762\u8bd5\u9a8c[33]\u6216\u4e13\u95e8\u7684\u5b9e\u9a8c\u6d4b\u8bd5\u88c5\u7f6e\u8fdb\u884c\u5b9e\u9a8c\u8bc4\u4f30[34]\u3002<\/p>\n\n\n\n<p>In the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Aerospace\" target=\"_blank\" rel=\"noreferrer noopener\">aerospace<\/a> industry, <strong>chevrons<\/strong> are the &#8220;saw-tooth&#8221; patterns on the trailing edges of some <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Jet_engine\" target=\"_blank\" rel=\"noreferrer noopener\">jet engine<\/a> nozzles<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-NASA-35\" target=\"_blank\" rel=\"noreferrer noopener\">[35]<\/a> that are used for <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Noise_control\" target=\"_blank\" rel=\"noreferrer noopener\">noise reduction<\/a>. The shaped edges smooth the mixing of hot air from the engine core and cooler air flowing through the engine fan, which reduces noise-creating turbulence.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-NASA-35\" target=\"_blank\" rel=\"noreferrer noopener\">[35]<\/a> Chevrons were developed by GE under a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/NASA\" target=\"_blank\" rel=\"noreferrer noopener\">NASA<\/a> contract.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-NASA-35\" target=\"_blank\" rel=\"noreferrer noopener\">[35]<\/a><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-chevron_technology-36\" target=\"_blank\" rel=\"noreferrer noopener\">[36]<\/a> Some notable examples of such designs are <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Boeing_787\" target=\"_blank\" rel=\"noreferrer noopener\">Boeing 787<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Boeing_747-8\" target=\"_blank\" rel=\"noreferrer noopener\">Boeing 747-8<\/a> \u2013 on the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_Trent_1000\" target=\"_blank\" rel=\"noreferrer noopener\">Rolls-Royce Trent 1000<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_GEnx\" target=\"_blank\" rel=\"noreferrer noopener\">General Electric GEnx<\/a> engines.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-37\" target=\"_blank\" rel=\"noreferrer noopener\">[37]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u5728\u822a\u7a7a\u822a\u5929\u5de5\u4e1a\u4e2d\uff0c\u5207\u5f17\u6717\u662f\u4e00\u4e9b\u55b7\u6c14\u53d1\u52a8\u673a\u55b7\u53e3\u5c3e\u8ff9\u7684\u201c\u952f\u9f7f\u201d\u56fe\u6848[35]\uff0c\u7528\u4e8e\u964d\u566a\u3002\u8fd9\u4e9b\u5f62\u72b6\u7684\u8fb9\u7f18\u5e73\u6ed1\u4e86\u6765\u81ea\u53d1\u52a8\u673a\u6838\u5fc3\u7684\u70ed\u7a7a\u6c14\u548c\u901a\u8fc7\u53d1\u52a8\u673a\u98ce\u6247\u6d41\u52a8\u7684\u51b7\u6c14\u6d41\u7684\u6df7\u5408\uff0c\u4ece\u800c\u51cf\u5c11\u4e86\u4ea7\u751f\u566a\u97f3\u7684\u6e4d\u6d41[35]\u3002\u5207\u5f17\u6717\u662f\u7531\u901a\u7528\u7535\u6c14\u516c\u53f8\u5728NASA\u7684\u5408\u540c\u4e0b\u5f00\u53d1\u7684[35][36]\u3002\u4e00\u4e9b\u8457\u540d\u7684\u8bbe\u8ba1\u793a\u4f8b\u5305\u62ec\u6ce2\u97f3787\u548c\u6ce2\u97f3747-8\u4e0a\u7684\u52b3\u65af\u83b1\u65af\u7279\u4f261000\u548c\u901a\u7528\u7535\u6c14GEnx\u53d1\u52a8\u673a[37]\u3002<\/p>\n\n\n\n<h2 class=\"wp-block-heading\" id=\"h_659034614_7\">2. \u5386\u53f2 | History<\/h2>\n\n\n\n<div class=\"wp-block-buttons is-layout-flex wp-block-buttons-is-layout-flex\">\n<div class=\"wp-block-button\"><a class=\"wp-block-button__link wp-element-button\" href=\"https:\/\/www.zhihu.com\/pin\/1849396728438059008\">\u56fe2-1\u548c2-2\uff08\u53d1\u5e03\u4e8e\u77e5\u4e4e\u60f3\u6cd5\uff09<\/a><\/div>\n<\/div>\n\n\n\n<p>Early turbojet engines were not very fuel-efficient because their overall pressure ratio and turbine inlet temperature were severely limited by the technology and materials available at the time.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u65e9\u671f\u7684\u6da1\u8f6e\u55b7\u6c14\u53d1\u52a8\u673a\u71c3\u6cb9\u6548\u7387\u4e0d\u9ad8\uff0c\u56e0\u4e3a\u5b83\u4eec\u7684\u603b\u538b\u529b\u6bd4\u548c\u6da1\u8f6e\u5165\u53e3\u6e29\u5ea6\u53d7\u5230\u5f53\u65f6\u53ef\u7528\u7684\u6280\u672f\u548c\u6750\u6599\u7684\u4e25\u91cd\u9650\u5236\u3002<\/p>\n\n\n\n<p>The first turbofan engine, which was only run on a test bed, was the German <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Daimler-Benz_DB_007\" target=\"_blank\" rel=\"noreferrer noopener\">Daimler-Benz DB 670<\/a>, designated the 109-007 by the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Ministry_of_Aviation_%28Nazi_Germany%29\" target=\"_blank\" rel=\"noreferrer noopener\">Nazi Ministry of Aviation<\/a>, with a first run date of 27 May 1943, after the testing of the turbomachinery using an electric motor, which had been undertaken on 1 April 1943.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-38\" target=\"_blank\" rel=\"noreferrer noopener\">[38]<\/a> Development of the engine was abandoned with its problems unsolved, as the war situation worsened for Germany.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u7b2c\u4e00\u4e2a\u6da1\u6247\u53d1\u52a8\u673a\u662f\u5fb7\u56fd\u6234\u59c6\u52d2-\u5954\u9a70DB 670\uff0c\u5728\u7eb3\u7cb9\u822a\u7a7a\u90e8\u95e8\u88ab\u79f0\u4e3a109-007\uff0c\u4e8e1943\u5e745\u670827\u65e5\u9996\u6b21\u8fd0\u884c\uff0c\u5728\u6b64\u4e4b\u524d\uff0c\u8be5\u53d1\u52a8\u673a\u7684\u6da1\u8f6e\u673a\u68b0\u88c5\u7f6e\u5df2\u4e8e1943\u5e744\u67081\u65e5\u4f7f\u7528\u7535\u52a8\u673a\u8fdb\u884c\u4e86\u6d4b\u8bd5[38]\u3002\u7531\u4e8e\u6218\u4e89\u5bf9\u5fb7\u56fd\u7684\u60c5\u51b5\u65e5\u76ca\u6076\u5316\uff0c\u8be5\u53d1\u52a8\u673a\u7684\u5f00\u53d1\u88ab\u4e2d\u6b62\uff0c\u5e76\u4e14\u5176\u95ee\u9898\u672a\u80fd\u89e3\u51b3\u3002<\/p>\n\n\n\n<p>Later in 1943, the British ground tested the Metrovick F.3<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-39\" target=\"_blank\" rel=\"noreferrer noopener\">[39]<\/a> turbofan, which used the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Metropolitan-Vickers_F.2\" target=\"_blank\" rel=\"noreferrer noopener\">Metrovick F.2<\/a> turbojet as a gas generator with the exhaust discharging into a close-coupled aft-fan module comprising a contra-rotating LP turbine system driving two co-axial contra-rotating fans.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-40\" target=\"_blank\" rel=\"noreferrer noopener\">[40]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u57281943\u5e74\u665a\u4e9b\u65f6\u5019\uff0c\u82f1\u56fd\u5bf9Metrovick F.3\u8fdb\u884c\u4e86\u5730\u9762\u6d4b\u8bd5[39]\uff0c\u8be5\u53d1\u52a8\u673a\u4f7f\u7528Metrovick F.2\u6da1\u55b7\u4f5c\u4e3a\u6c14\u4f53\u53d1\u751f\u5668\uff0c\u6392\u6c14\u53e3\u6392\u653e\u5230\u4e00\u4e2a\u7d27\u5bc6\u8026\u5408\u7684\u540e\u98ce\u6247\u6a21\u5757\u4e2d\uff0c\u8be5\u6a21\u5757\u7531\u4e00\u4e2a\u9006\u8f6c\u7684\u4f4e\u538b\u6da1\u8f6e\u7cfb\u7edf\u9a71\u52a8\u4e24\u4e2a\u540c\u8f74\u9006\u8f6c\u7684\u98ce\u6247[40]\u3002<\/p>\n\n\n\n<p>Improved materials, and the introduction of twin compressors, such as in the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_Olympus\" target=\"_blank\" rel=\"noreferrer noopener\">Bristol Olympus<\/a>,<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-41\" target=\"_blank\" rel=\"noreferrer noopener\">[41]<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_JT3C\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney JT3C<\/a> engines, increased the overall pressure ratio and thus the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Thermodynamics\" target=\"_blank\" rel=\"noreferrer noopener\">thermodynamic<\/a> efficiency of engines. They also had poor propulsive efficiency, because pure turbojets have a high specific thrust\/high velocity exhaust, which is better suited to supersonic flight.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6539\u8fdb\u7684\u6750\u6599\u4ee5\u53ca\u5f15\u5165\u4e86\u53cc\u538b\u7f29\u673a\uff0c\u4f8b\u5982\u5e03\u91cc\u65af\u6258\u5c14\u5965\u6797\u5339\u65af[41]\u548c\u666e\u62c9\u7279\u548c\u60e0\u7279\u5c3cJT3C\u53d1\u52a8\u673a\uff0c\u63d0\u9ad8\u4e86\u53d1\u52a8\u673a\u7684\u603b\u538b\u6bd4\uff0c\u4ece\u800c\u63d0\u9ad8\u4e86\u70ed\u529b\u5b66\u6548\u7387\u3002\u7136\u800c\uff0c\u5b83\u4eec\u7684\u63a8\u529b\u6548\u7387\u8f83\u4f4e\uff0c\u56e0\u4e3a\u7eaf\u6da1\u55b7\u53d1\u52a8\u673a\u5177\u6709\u9ad8\u6bd4\u51b2\/\u9ad8\u901f\u6392\u6c14\uff0c\u66f4\u9002\u5408\u4e8e\u8d85\u97f3\u901f\u98de\u884c\u3002<\/p>\n\n\n\n<p>The original low-bypass turbofan engines were designed to improve propulsive efficiency by reducing the exhaust velocity to a value closer to that of the aircraft. The <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_Conway\" target=\"_blank\" rel=\"noreferrer noopener\">Rolls-Royce Conway<\/a>, the world&#8217;s first production turbofan, had a bypass ratio of 0.3, similar to the modern <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_F404\" target=\"_blank\" rel=\"noreferrer noopener\">General Electric F404<\/a> fighter engine. Civilian turbofan engines of the 1960s, such as the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_JT8D\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney JT8D<\/a> and the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_Spey\" target=\"_blank\" rel=\"noreferrer noopener\">Rolls-Royce Spey<\/a>, had bypass ratios closer to 1 and were similar to their military equivalents.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6700\u521d\u7684\u4f4e\u6db5\u9053\u6bd4\u6da1\u6247\u53d1\u52a8\u673a\u65e8\u5728\u901a\u8fc7\u5c06\u6392\u6c14\u901f\u5ea6\u964d\u4f4e\u5230\u63a5\u8fd1\u98de\u673a\u901f\u5ea6\u7684\u503c\u6765\u63d0\u9ad8\u63a8\u529b\u6548\u7387\u7f57\u5c14\u65af-\u7f57\u4f0a\u65af\u5eb7\u5a01\u662f\u4e16\u754c\u4e0a\u7b2c\u4e00\u6b3e\u91cf\u4ea7\u6da1\u6247\u53d1\u52a8\u673a\uff0c\u5176\u6db5\u9053\u6bd4\u4e3a0.3\uff0c\u7c7b\u4f3c\u4e8e\u73b0\u4ee3\u7684\u901a\u7528\u7535\u6c14F404\u6218\u6597\u673a\u53d1\u52a8\u673a\u300220\u4e16\u7eaa60\u5e74\u4ee3\u7684\u6c11\u7528\u6da1\u6247\u53d1\u52a8\u673a\uff0c\u5982\u666e\u60e0JT8D\u548c\u7f57\u5c14\u65af-\u7f57\u4f0a\u65afSpey\uff0c\u6db5\u9053\u6bd4\u66f4\u63a5\u8fd11\uff0c\u4e0e\u5176\u519b\u7528\u5bf9\u5e94\u578b\u53f7\u76f8\u4f3c\u3002<\/p>\n\n\n\n<p>The first Soviet airliner powered by turbofan engines was the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Tupolev_Tu-124\" target=\"_blank\" rel=\"noreferrer noopener\">Tupolev Tu-124<\/a> introduced in 1962. It used the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Soloviev_D-20\" target=\"_blank\" rel=\"noreferrer noopener\">Soloviev D-20<\/a>.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-42\" target=\"_blank\" rel=\"noreferrer noopener\">[42]<\/a> 164 aircraft were produced between 1960 and 1965 for <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Aeroflot\" target=\"_blank\" rel=\"noreferrer noopener\">Aeroflot<\/a> and other <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Eastern_Bloc\" target=\"_blank\" rel=\"noreferrer noopener\">Eastern Bloc<\/a> airlines, with some operating until the early 1990s.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u9996\u6b3e\u7531\u6da1\u6247\u53d1\u52a8\u673a\u9a71\u52a8\u7684\u82cf\u8054\u5ba2\u673a\u662f1962\u5e74\u5f15\u5165\u7684\u56fe\u6ce2\u5217\u592bTu-124\u3002\u5b83\u4f7f\u7528\u7684\u662fSoloviev D-20\u53d1\u52a8\u673a[42]\u3002\u57281960\u5e74\u81f31965\u5e74\u671f\u95f4\uff0c\u5171\u751f\u4ea7\u4e86164\u67b6\u98de\u673a\u4f9b\u4fc4\u7f57\u65af\u822a\u7a7a\u548c\u5176\u4ed6\u4e1c\u65b9\u96c6\u56e2\u56fd\u5bb6\u7684\u822a\u7a7a\u516c\u53f8\u4f7f\u7528\uff0c\u5176\u4e2d\u4e00\u4e9b\u98de\u673a\u4e00\u76f4\u8fd0\u8425\u523090\u5e74\u4ee3\u521d\u3002<\/p>\n\n\n\n<p>The first General Electric turbofan was the aft-fan <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_CJ805\" target=\"_blank\" rel=\"noreferrer noopener\">CJ805-23<\/a>, based on the CJ805-3 turbojet. It was followed by the aft-fan <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_CF700\" target=\"_blank\" rel=\"noreferrer noopener\">General Electric CF700<\/a> engine, with a 2.0 bypass ratio. This was derived from the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_J85\" target=\"_blank\" rel=\"noreferrer noopener\">General Electric J85\/CJ610<\/a> turbojet 2,850 lbf (12,700 N) to power the larger <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/North_American_Sabreliner\" target=\"_blank\" rel=\"noreferrer noopener\">Rockwell Sabreliner<\/a> 75\/80 model aircraft, as well as the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Dassault_Falcon_20\" target=\"_blank\" rel=\"noreferrer noopener\">Dassault Falcon 20<\/a>, with about a 50% increase in thrust to 4,200 lbf (19,000 N). The CF700 was the first small turbofan to be certified by the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Federal_Aviation_Administration\" target=\"_blank\" rel=\"noreferrer noopener\">Federal Aviation Administration<\/a> (FAA). There were at one time over 400 CF700 aircraft in operation around the world, with an experience base of over 10 million service hours. The CF700 turbofan engine was also used to train Moon-bound astronauts in <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Project_Apollo\" target=\"_blank\" rel=\"noreferrer noopener\">Project Apollo<\/a> as the powerplant for the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/LLRV\" target=\"_blank\" rel=\"noreferrer noopener\">Lunar Landing Research Vehicle<\/a>.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u7b2c\u4e00\u6b3e\u901a\u7528\u7535\u6c14\u6da1\u6247\u53d1\u52a8\u673a\u662f\u57fa\u4e8eCJ805-3\u6da1\u55b7\u53d1\u52a8\u673a\u7684\u540e\u7f6e\u98ce\u6247CJ805-23\u3002\u968f\u540e\u63a8\u51fa\u4e86\u540e\u7f6e\u98ce\u6247\u901a\u7528\u7535\u6c14CF700\u53d1\u52a8\u673a\uff0c\u6db5\u9053\u6bd4\u4e3a2.0\u3002\u8be5\u53d1\u52a8\u673a\u662f\u7531\u901a\u7528\u7535\u6c14J85\/CJ610\u6da1\u55b7\u53d1\u52a8\u673a\u53d1\u5c55\u800c\u6765\uff0c\u5177\u67092,850\u78c5\u529b\uff0812,700\u725b\u987f\uff09\u7684\u63a8\u529b\uff0c\u7528\u4e8e\u4e3a\u66f4\u5927\u7684\u6d1b\u514b\u97e6\u5c14Sabreliner 75\/80\u578b\u98de\u673a\u548c\u8fbe\u7d22\u730e\u9e7020\u578b\u98de\u673a\u63d0\u4f9b\u52a8\u529b\uff0c\u5e76\u5c06\u63a8\u529b\u589e\u52a0\u4e86\u7ea650%\u81f34,200\u78c5\u529b\uff0819,000\u725b\u987f\uff09\u3002CF700\u662f\u7b2c\u4e00\u6b3e\u83b7\u5f97\u7f8e\u56fd\u8054\u90a6\u822a\u7a7a\u5c40\uff08FAA\uff09\u8ba4\u8bc1\u7684\u5c0f\u578b\u6da1\u6247\u53d1\u52a8\u673a\u3002\u66fe\u7ecf\u5728\u5168\u7403\u8303\u56f4\u5185\u8fd0\u8425\u7740400\u591a\u67b6CF700\u98de\u673a\uff0c\u7d2f\u8ba1\u4f7f\u7528\u65f6\u95f4\u8d85\u8fc71000\u4e07\u5c0f\u65f6\u3002CF700\u6da1\u6247\u53d1\u52a8\u673a\u8fd8\u88ab\u7528\u4f5c\u963f\u6ce2\u7f57\u8ba1\u5212\u4e2d\u524d\u5f80\u6708\u7403\u7684\u5b87\u822a\u5458\u5728\u767b\u6708\u7814\u7a76\u8f66\u4e0a\u7684\u52a8\u529b\u88c5\u7f6e\u3002<\/p>\n\n\n\n<h2 class=\"wp-block-heading\" id=\"h_659034614_8\">3. \u5e38\u89c1\u7c7b\u578b | Common types<\/h2>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_9\">3.1 \u5c0f\u6db5\u9053\u6bd4\u6da1\u6247 | Low-bypass turbofan<\/h3>\n\n\n\n<div class=\"wp-block-buttons is-layout-flex wp-block-buttons-is-layout-flex\">\n<div class=\"wp-block-button\"><a class=\"wp-block-button__link wp-element-button\" href=\"https:\/\/www.zhihu.com\/pin\/1849396244570566656\">\u56fe3-1\uff08\u53d1\u5e03\u4e8e\u77e5\u4e4e\u60f3\u6cd5\uff09<\/a><\/div>\n<\/div>\n\n\n\n<p>A high-specific-thrust\/low-bypass-ratio turbofan normally has a multi-stage fan behind inlet guide vanes, developing a relatively high pressure ratio and, thus, yielding a high (mixed or cold) exhaust velocity. The core airflow needs to be large enough to ensure there is sufficient <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/w\/index.php%3Ftitle%3DCore_power%26action%3Dedit%26redlink%3D1\" target=\"_blank\" rel=\"noreferrer noopener\">core power<\/a> to drive the fan. A smaller core flow\/higher bypass ratio cycle can be achieved by raising the inlet temperature of the high-pressure (HP) turbine rotor.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u9ad8\u6bd4\u63a8\u529b\/\u4f4e\u6db5\u9053\u6bd4\u6da1\u6247\u901a\u5e38\u5728\u8fdb\u6c14\u5bfc\u53f6\u540e\u9762\u6709\u591a\u7ea7\u98ce\u6247\uff0c\u5f62\u6210\u76f8\u5bf9\u8f83\u9ad8\u7684\u538b\u529b\u6bd4\uff0c\u4ece\u800c\u4ea7\u751f\u8f83\u9ad8\u7684\uff08\u6df7\u5408\u6216\u51b7\uff09\u6392\u6c14\u901f\u5ea6\u3002\u6838\u5fc3\u6c14\u6d41\u9700\u8981\u8db3\u591f\u5927\uff0c\u4ee5\u786e\u4fdd\u6709\u8db3\u591f\u7684\u6838\u5fc3\u52a8\u529b\u6765\u9a71\u52a8\u98ce\u6247\u3002\u901a\u8fc7\u63d0\u9ad8\u9ad8\u538b\uff08HP\uff09\u6da1\u8f6e\u8f6c\u5b50\u7684\u8fdb\u6c14\u6e29\u5ea6\uff0c\u53ef\u4ee5\u5b9e\u73b0\u8f83\u5c0f\u7684\u6838\u5fc3\u6d41\u91cf\/\u8f83\u9ad8\u7684\u6db5\u9053\u6bd4\u5faa\u73af\u3002<\/p>\n\n\n\n<p>To illustrate one aspect of how a turbofan differs from a turbojet, comparisons can be made at the same airflow (to keep a common intake for example) and the same net thrust (i.e. same specific thrust). A bypass flow can be added only if the turbine inlet temperature is not too high to compensate for the smaller core flow. Future improvements in turbine cooling\/material technology can allow higher turbine inlet temperature, which is necessary because of increased cooling air temperature, resulting from an <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Overall_pressure_ratio\" target=\"_blank\" rel=\"noreferrer noopener\">overall pressure ratio<\/a> increase.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u4e3a\u4e86\u8bf4\u660e\u6da1\u6247\u4e0e\u6da1\u55b7\u53d1\u52a8\u673a\u7684\u4e00\u65b9\u9762\u533a\u522b\uff0c\u53ef\u4ee5\u5728\u76f8\u540c\u7684\u6c14\u6d41\u6761\u4ef6\u4e0b\u8fdb\u884c\u6bd4\u8f83\uff08\u4f8b\u5982\u4fdd\u6301\u76f8\u540c\u7684\u8fdb\u6c14\u53e3\uff09\uff0c\u5e76\u4e14\u5177\u6709\u76f8\u540c\u7684\u51c0\u63a8\u529b\uff08\u5373\u76f8\u540c\u7684\u6bd4\u63a8\u529b\uff09\u3002\u53ea\u6709\u5728\u6da1\u8f6e\u8fdb\u53e3\u6e29\u5ea6\u4e0d\u592a\u9ad8\u4ee5\u8865\u507f\u8f83\u5c0f\u7684\u6838\u5fc3\u6d41\u91cf\u65f6\uff0c\u624d\u80fd\u589e\u52a0\u6db5\u9053\u6d41\u91cf\u3002\u672a\u6765\u6da1\u8f6e\u51b7\u5374\/\u6750\u6599\u6280\u672f\u7684\u6539\u8fdb\u53ef\u4ee5\u5b9e\u73b0\u66f4\u9ad8\u7684\u6da1\u8f6e\u8fdb\u53e3\u6e29\u5ea6\uff0c\u8fd9\u662f\u5fc5\u8981\u7684\uff0c\u56e0\u4e3a\u6574\u4f53\u538b\u6bd4\u589e\u52a0\u5bfc\u81f4\u51b7\u5374\u6c14\u6e29\u589e\u52a0\u3002<\/p>\n\n\n\n<p>The resulting turbofan, with reasonable efficiencies and duct loss for the added components, would probably operate at a higher nozzle pressure ratio than the turbojet, but with a lower exhaust temperature to retain net thrust. Since the temperature rise across the whole engine (intake to nozzle) would be lower, the (dry power) fuel flow would also be reduced, resulting in a better <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Thrust_specific_fuel_consumption\" target=\"_blank\" rel=\"noreferrer noopener\">specific fuel consumption<\/a> (SFC).<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6700\u7ec8\u5f97\u5230\u7684\u6da1\u6247\u53d1\u52a8\u673a\uff0c\u901a\u8fc7\u5408\u7406\u7684\u6548\u7387\u548c\u7ba1\u9053\u635f\u5931\u6765\u8003\u8651\u65b0\u589e\u7ec4\u4ef6\uff0c\u53ef\u80fd\u4f1a\u4ee5\u6bd4\u6da1\u55b7\u53d1\u52a8\u673a\u66f4\u9ad8\u7684\u55b7\u5634\u538b\u529b\u6bd4\u8fd0\u884c\uff0c\u4f46\u51fa\u53e3\u6e29\u5ea6\u8f83\u4f4e\u4ee5\u4fdd\u6301\u51c0\u63a8\u529b\u3002\u7531\u4e8e\u6574\u4e2a\u53d1\u52a8\u673a\uff08\u8fdb\u6c14\u53e3\u5230\u55b7\u5634\uff09\u7684\u6e29\u5ea6\u5347\u9ad8\u8f83\u4f4e\uff0c\uff08\u5e72\u529f\uff09\u71c3\u6cb9\u6d41\u91cf\u4e5f\u4f1a\u51cf\u5c11\uff0c\u4ece\u800c\u5b9e\u73b0\u66f4\u597d\u7684\u6bd4\u71c3\u6cb9\u6d88\u8017\u7387\uff08SFC\uff09\u3002<\/p>\n\n\n\n<p>Some low-bypass ratio military turbofans (e.g. <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_F404\" target=\"_blank\" rel=\"noreferrer noopener\">F404<\/a>, <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_JT8D\" target=\"_blank\" rel=\"noreferrer noopener\">JT8D<\/a>) have variable inlet guide vanes to direct air onto the first fan rotor stage. This improves the fan <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Compressor_stall\" target=\"_blank\" rel=\"noreferrer noopener\">surge<\/a> margin (see <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Compressor_map\" target=\"_blank\" rel=\"noreferrer noopener\">compressor map<\/a>).<br>\u53c2\u8003\u8bd1\u6587\uff1a\u4e00\u4e9b\u4f4e\u6db5\u9053\u6bd4\u7684\u519b\u7528\u6da1\u6247\u53d1\u52a8\u673a\uff08\u4f8b\u5982F404\u3001JT8D\uff09\u914d\u5907\u4e86\u53ef\u53d8\u8fdb\u6c14\u5bfc\u53f6\uff0c\u7528\u4e8e\u5c06\u7a7a\u6c14\u5f15\u5bfc\u5230\u7b2c\u4e00\u7ea7\u98ce\u6247\u53f6\u7247\u4e0a\u3002\u8fd9\u53ef\u4ee5\u6539\u5584\u98ce\u6247\u7684\u6da1\u6d41\u8fb9\u7f18\uff08\u53c2\u89c1\u538b\u6c14\u673a\u7279\u6027\u66f2\u7ebf\uff09\u3002<\/p>\n\n\n\n<p><a target=\"_blank\" href=\"https:\/\/www.zhihu.com\/pin\/1691976014949990400\" rel=\"noreferrer noopener\">\u56fe\u96c6\uff1a\u4ee3\u8868\u6027\u7684\u5c0f\u6db5\u9053\u6bd4\u6da1\u6247\u53d1\u52a8\u673a \u8bf7\u70b9\u51fb\u8fd9\u91cc\u8bbf\u95ee\u200b<\/a><\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_10\">3.2 \u52a0\u529b\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a | Afterburning turbofan<\/h3>\n\n\n\n<p><em>Further information: <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Afterburner\" target=\"_blank\" rel=\"noreferrer noopener\">Afterburner<\/a><\/em><br><em>\u66f4\u591a\u4fe1\u606f\uff1a\u540e\u71c3\u70e7\u5ba4<\/em><\/p>\n\n\n\n<div class=\"wp-block-buttons is-layout-flex wp-block-buttons-is-layout-flex\">\n<div class=\"wp-block-button\"><a class=\"wp-block-button__link wp-element-button\" href=\"https:\/\/www.zhihu.com\/pin\/1849395962142920704\">\u56fe3-2\uff08\u53d1\u5e03\u4e8e\u77e5\u4e4e\u60f3\u6cd5\uff09<\/a><\/div>\n<\/div>\n\n\n\n<p>Since the 1970s, most <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Jet_fighter\" target=\"_blank\" rel=\"noreferrer noopener\">jet fighter<\/a> engines have been low\/medium bypass turbofans with a mixed exhaust, <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Afterburner\" target=\"_blank\" rel=\"noreferrer noopener\">afterburner<\/a> and variable area exit nozzle. An afterburner is a combustor located downstream of the turbine blades and directly upstream of the nozzle, which burns fuel from afterburner-specific fuel injectors. When lit, large volumes of fuel are burnt in the afterburner, raising the temperature of exhaust gases by a significant degree, resulting in a higher exhaust velocity\/engine specific thrust. The variable geometry nozzle must open to a larger throat area to accommodate the extra volume and increased flow rate when the afterburner is lit. Afterburning is often designed to give a significant thrust boost for take off, transonic acceleration and combat maneuvers, but is very fuel intensive. Consequently, afterburning can be used only for short portions of a mission.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u81ea20\u4e16\u7eaa70\u5e74\u4ee3\u4ee5\u6765\uff0c\u5927\u591a\u6570\u55b7\u6c14\u5f0f\u6218\u6597\u673a\u53d1\u52a8\u673a\u90fd\u91c7\u7528\u4f4e\/\u4e2d\u6db5\u9053\u6bd4\u7684\u6da1\u6247\u53d1\u52a8\u673a\uff0c\u914d\u5907\u4e86\u6df7\u5408\u6392\u6c14\u3001\u52a0\u529b\u71c3\u70e7\u5ba4\u548c\u53ef\u53d8\u9762\u79ef\u55b7\u5634\u3002\u52a0\u529b\u71c3\u70e7\u5ba4\u4f4d\u4e8e\u6da1\u8f6e\u53f6\u7247\u7684\u4e0b\u6e38\uff0c\u76f4\u63a5\u4f4d\u4e8e\u55b7\u5634\u7684\u4e0a\u6e38\uff0c\u4ece\u52a0\u529b\u71c3\u70e7\u5ba4\u4e13\u7528\u7684\u71c3\u6cb9\u55b7\u5c04\u5668\u4e2d\u71c3\u70e7\u71c3\u6599\u3002\u5f53\u70b9\u706b\u65f6\uff0c\u5927\u91cf\u71c3\u6599\u5728\u52a0\u529b\u71c3\u70e7\u5ba4\u4e2d\u71c3\u70e7\uff0c\u663e\u8457\u63d0\u9ad8\u6392\u6c14\u6c14\u4f53\u7684\u6e29\u5ea6\uff0c\u4ece\u800c\u4f7f\u55b7\u6c14\u901f\u5ea6\/\u53d1\u52a8\u673a\u6bd4\u63a8\u529b\u589e\u52a0\u3002\u53ef\u53d8\u51e0\u4f55\u55b7\u5634\u5fc5\u987b\u5f00\u5230\u66f4\u5927\u7684\u5589\u90e8\u9762\u79ef\uff0c\u4ee5\u9002\u5e94\u70b9\u706b\u65f6\u7684\u989d\u5916\u5bb9\u79ef\u548c\u589e\u52a0\u7684\u6d41\u91cf\u3002\u52a0\u529b\u71c3\u70e7\u901a\u5e38\u8bbe\u8ba1\u7528\u4e8e\u8d77\u98de\u3001\u8d85\u97f3\u901f\u52a0\u901f\u548c\u6218\u6597\u673a\u52a8\u7b49\u9636\u6bb5\uff0c\u80fd\u591f\u663e\u8457\u63d0\u4f9b\u63a8\u529b\u589e\u76ca\uff0c\u4f46\u71c3\u6cb9\u6d88\u8017\u91cf\u5f88\u5927\u3002\u56e0\u6b64\uff0c\u52a0\u529b\u71c3\u70e7\u53ea\u80fd\u5728\u4efb\u52a1\u7684\u77ed\u65f6\u95f4\u5185\u4f7f\u7528\u3002<\/p>\n\n\n\n<p>Unlike in the main engine, where <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Stoichiometric\" target=\"_blank\" rel=\"noreferrer noopener\">stoichiometric<\/a> temperatures in the combustor have to be reduced before they reach the turbine, an afterburner at maximum fuelling is designed to produce stoichiometric temperatures at entry to the nozzle, about 2,100 K (3,800 \u00b0R; 3,300 \u00b0F; 1,800 \u00b0C). At a fixed total applied fuel:air ratio, the total fuel flow for a given fan airflow will be the same, regardless of the dry specific thrust of the engine. However, a high specific thrust turbofan will, by definition, have a higher nozzle pressure ratio, resulting in a higher afterburning net thrust and, therefore, a lower afterburning specific fuel consumption (SFC). However, high specific thrust engines have a high dry SFC. The situation is reversed for a medium specific thrust afterburning turbofan: i.e., poor afterburning SFC\/good dry SFC. The former engine is suitable for a combat aircraft which must remain in afterburning combat for a fairly long period, but has to fight only fairly close to the airfield (e.g. cross border skirmishes). The latter engine is better for an aircraft that has to fly some distance, or loiter for a long time, before going into combat. However, the pilot can afford to stay in afterburning only for a short period, before aircraft fuel reserves become dangerously low.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u4e0e\u4e3b\u53d1\u52a8\u673a\u4e0d\u540c\uff0c\u71c3\u70e7\u5ba4\u4e2d\u7684\u5316\u5b66\u5f53\u91cf\u6e29\u5ea6\u5fc5\u987b\u5728\u8fdb\u5165\u6da1\u8f6e\u4e4b\u524d\u964d\u4f4e\uff0c\u800c\u6700\u5927\u71c3\u6cb9\u55b7\u5c04\u91cf\u4e0b\u7684\u52a0\u529b\u71c3\u70e7\u5ba4\u88ab\u8bbe\u8ba1\u6210\u5728\u8fdb\u5165\u55b7\u5634\u65f6\u4ea7\u751f\u5316\u5b66\u5f53\u91cf\u6e29\u5ea6\uff0c\u7ea6\u4e3a2100K\uff083800\u00b0R\uff1b3300\u00b0F\uff1b1800\u00b0C\uff09\u3002\u5728\u56fa\u5b9a\u7684\u71c3\u6cb9:\u7a7a\u6c14\u6bd4\u4e0b\uff0c\u5bf9\u4e8e\u7ed9\u5b9a\u7684\u98ce\u6247\u7a7a\u6c14\u6d41\u91cf\uff0c\u603b\u71c3\u6cb9\u6d41\u91cf\u5c06\u662f\u76f8\u540c\u7684\uff0c\u800c\u4e0d\u8003\u8651\u53d1\u52a8\u673a\u7684\u5e72\u529f\u6bd4\u63a8\u529b\u3002\u7136\u800c\uff0c\u9ad8\u6bd4\u63a8\u529b\u7684\u6da1\u6247\u53d1\u52a8\u673a\u5c06\u5177\u6709\u66f4\u9ad8\u7684\u55b7\u5634\u538b\u529b\u6bd4\uff0c\u4ece\u800c\u5bfc\u81f4\u66f4\u9ad8\u7684\u52a0\u529b\u71c3\u70e7\u51c0\u63a8\u529b\uff0c\u56e0\u6b64\u52a0\u529b\u71c3\u70e7\u7684\u6bd4\u71c3\u6cb9\u6d88\u8017\u7387\uff08SFC\uff09\u8f83\u4f4e\u3002\u7136\u800c\uff0c\u9ad8\u6bd4\u63a8\u529b\u53d1\u52a8\u673a\u7684\u5e72\u529f\u6bd4\u71c3\u6cb9\u6d88\u8017\u7387\u8f83\u9ad8\u3002\u5bf9\u4e8e\u4e2d\u7b49\u6bd4\u63a8\u529b\u7684\u52a0\u529b\u6da1\u6247\u53d1\u52a8\u673a\u6765\u8bf4\u60c5\u51b5\u5c31\u76f8\u53cd\uff0c\u5373\u52a0\u529b\u71c3\u70e7\u7684\u6bd4\u71c3\u6cb9\u6d88\u8017\u7387\u8f83\u9ad8\uff0c\u4f46\u5e72\u529f\u6bd4\u71c3\u6cb9\u6d88\u8017\u7387\u8f83\u597d\u3002\u524d\u4e00\u79cd\u53d1\u52a8\u673a\u9002\u7528\u4e8e\u9700\u8981\u5728\u52a0\u529b\u71c3\u70e7\u72b6\u6001\u4e0b\u8fdb\u884c\u76f8\u5f53\u957f\u65f6\u95f4\u7684\u6218\u6597\u673a\uff0c\u4f46\u53ea\u9700\u5728\u79bb\u673a\u573a\u76f8\u5f53\u8fd1\u7684\u5730\u65b9\u6218\u6597\uff08\u4f8b\u5982\uff0c\u8de8\u5883\u51b2\u7a81\uff09\u3002\u540e\u4e00\u79cd\u53d1\u52a8\u673a\u66f4\u9002\u7528\u4e8e\u5728\u8fdb\u5165\u6218\u6597\u4e4b\u524d\u9700\u8981\u98de\u884c\u4e00\u6bb5\u8ddd\u79bb\u6216\u957f\u65f6\u95f4\u76d8\u65cb\u7684\u98de\u673a\u3002\u7136\u800c\uff0c\u98de\u884c\u5458\u53ea\u80fd\u5728\u71c3\u6cb9\u50a8\u5907\u53d8\u5f97\u5371\u9669\u4f4e\u4e4b\u524d\u77ed\u65f6\u95f4\u5185\u4f7f\u7528\u52a0\u529b\u71c3\u70e7\u3002<\/p>\n\n\n\n<p>The first production afterburning turbofan engine was the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_TF30\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney TF30<\/a>, which initially powered the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Dynamics_F-111_Aardvark\" target=\"_blank\" rel=\"noreferrer noopener\">F-111 Aardvark<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Grumman_F-14_Tomcat\" target=\"_blank\" rel=\"noreferrer noopener\">F-14 Tomcat<\/a>. Current low-bypass military turbofans include the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_F119\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney F119<\/a>, the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Eurojet_EJ200\" target=\"_blank\" rel=\"noreferrer noopener\">Eurojet EJ200<\/a>, the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_F110\" target=\"_blank\" rel=\"noreferrer noopener\">General Electric F110<\/a>, the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Klimov_RD-33\" target=\"_blank\" rel=\"noreferrer noopener\">Klimov RD-33<\/a>, and the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Saturn_AL-31\" target=\"_blank\" rel=\"noreferrer noopener\">Saturn AL-31<\/a>, all of which feature a mixed exhaust, afterburner and variable area propelling nozzle.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u9996\u6b3e\u751f\u4ea7\u578b\u52a0\u529b\u6da1\u6247\u53d1\u52a8\u673a\u662f\u666e\u60e0TF30\uff0c\u6700\u521d\u7528\u4e8eF-111 Aardvark\u548cF-14 Tomcat\u6218\u6597\u673a\u3002\u76ee\u524d\u7684\u4f4e\u6db5\u9053\u6bd4\u519b\u7528\u6da1\u6247\u53d1\u52a8\u673a\u5305\u62ec\u666e\u60e0F119\u3001\u6b27\u6d32\u5408\u4f5cEJ200\u3001\u901a\u7528\u7535\u6c14F110\u3001\u514b\u6797\u59c6\u592bRD-33\u548c\u8428\u56fe\u5c14AL-31\uff0c\u5b83\u4eec\u90fd\u91c7\u7528\u6df7\u5408\u6392\u6c14\u3001\u52a0\u529b\u71c3\u70e7\u5ba4\u548c\u53ef\u53d8\u9762\u79ef\u55b7\u5634\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_11\">3.3 \u5927\u6db5\u9053\u6bd4\u6da1\u6247\u53d1\u52a8\u673a | High-bypass turbofan<\/h3>\n\n\n\n<p><em>Further information: <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Bypass_ratio\" target=\"_blank\" rel=\"noreferrer noopener\">Bypass ratio<\/a><\/em><br><em>\u66f4\u591a\u4fe1\u606f\uff1a\u6db5\u9053\u6bd4<\/em><\/p>\n\n\n\n<div class=\"wp-block-buttons is-layout-flex wp-block-buttons-is-layout-flex\">\n<div class=\"wp-block-button\"><a class=\"wp-block-button__link wp-element-button\" href=\"https:\/\/www.zhihu.com\/pin\/1849395658848616448\">\u56fe3-3\uff08\u53d1\u5e03\u4e8e\u77e5\u4e4e\u60f3\u6cd5\uff09<\/a><\/div>\n<\/div>\n\n\n\n<p>To further improve fuel economy and reduce noise, almost all of today&#8217;s jet airliners and most military transport aircraft (e.g., the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/C-17_Globemaster_III\" target=\"_blank\" rel=\"noreferrer noopener\">C-17<\/a>) are powered by low-specific-thrust\/high-bypass-ratio turbofans. These engines evolved from the high-specific-thrust\/low-bypass-ratio turbofans used in such aircraft in the 1960s. Modern combat aircraft tend to use low-bypass ratio turbofans, and some military transport aircraft use <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turboprop\" target=\"_blank\" rel=\"noreferrer noopener\">turboprops<\/a>.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u4e3a\u4e86\u8fdb\u4e00\u6b65\u63d0\u9ad8\u71c3\u6cb9\u7ecf\u6d4e\u6027\u548c\u51cf\u5c11\u566a\u97f3\uff0c\u51e0\u4e4e\u6240\u6709\u73b0\u4ee3\u55b7\u6c14\u5f0f\u5ba2\u673a\u548c\u5927\u591a\u6570\u519b\u7528\u8fd0\u8f93\u673a\uff08\u4f8b\u5982C-17\uff09\u90fd\u91c7\u7528\u4e86\u4f4e\u6bd4\u63a8\u529b\/\u9ad8\u6db5\u9053\u6bd4\u6da1\u6247\u53d1\u52a8\u673a\u3002\u8fd9\u4e9b\u53d1\u52a8\u673a\u662f\u4ece20\u4e16\u7eaa60\u5e74\u4ee3\u4f7f\u7528\u5728\u8fd9\u4e9b\u98de\u673a\u4e0a\u7684\u9ad8\u6bd4\u63a8\u529b\/\u4f4e\u6db5\u9053\u6bd4\u6da1\u6247\u53d1\u52a8\u673a\u53d1\u5c55\u800c\u6765\u7684\u3002\u73b0\u4ee3\u6218\u6597\u673a\u503e\u5411\u4e8e\u4f7f\u7528\u4f4e\u6db5\u9053\u6bd4\u6da1\u6247\u53d1\u52a8\u673a\uff0c\u4e00\u4e9b\u519b\u7528\u8fd0\u8f93\u673a\u5219\u91c7\u7528\u6da1\u6868\u53d1\u52a8\u673a\u3002<\/p>\n\n\n\n<p>Low specific thrust is achieved by replacing the multi-stage fan with a single-stage unit. Unlike some military engines, modern civil turbofans lack stationary inlet guide vanes in front of the fan rotor. The fan is scaled to achieve the desired net thrust.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u901a\u8fc7\u4f7f\u7528\u5355\u7ea7\u98ce\u6247\u53d6\u4ee3\u591a\u7ea7\u98ce\u6247\uff0c\u53ef\u4ee5\u5b9e\u73b0\u4f4e\u6bd4\u63a8\u529b\u3002\u4e0e\u67d0\u4e9b\u519b\u7528\u53d1\u52a8\u673a\u4e0d\u540c\uff0c\u73b0\u4ee3\u6c11\u7528\u6da1\u6247\u53d1\u52a8\u673a\u5728\u98ce\u6247\u8f6c\u5b50\u524d\u65b9\u7f3a\u4e4f\u9759\u6b62\u8fdb\u53e3\u5bfc\u5411\u53f6\u7247\u3002\u98ce\u6247\u7684\u5c3a\u5bf8\u8c03\u6574\u4ee5\u5b9e\u73b0\u6240\u9700\u7684\u51c0\u63a8\u529b\u3002<\/p>\n\n\n\n<p>The core (or gas generator) of the engine must generate enough power to drive the fan at its rated mass flow and pressure ratio. Improvements in turbine cooling\/material technology allow for a higher (HP) turbine rotor inlet temperature, which allows a smaller (and lighter) core, potentially improving the core thermal efficiency. Reducing the core mass flow tends to increase the load on the LP turbine, so this unit may require additional stages to reduce the average <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Stage_loading\" target=\"_blank\" rel=\"noreferrer noopener\">stage loading<\/a> and to maintain LP turbine efficiency. Reducing core flow also increases bypass ratio. Bypass ratios greater than 5:1 are increasingly common; the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_PW1000G\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney PW1000G<\/a>, which entered commercial service in 2016, attains 12.5:1.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u53d1\u52a8\u673a\u7684\u6838\u5fc3\u90e8\u5206\uff08\u6216\u6c14\u4f53\u53d1\u751f\u5668\uff09\u5fc5\u987b\u4ea7\u751f\u8db3\u591f\u7684\u529f\u7387\u4ee5\u9a71\u52a8\u98ce\u6247\u8fbe\u5230\u989d\u5b9a\u8d28\u91cf\u6d41\u91cf\u548c\u538b\u529b\u6bd4\u3002\u6da1\u8f6e\u51b7\u5374\/\u6750\u6599\u6280\u672f\u7684\u6539\u8fdb\u4f7f\u5f97\u9ad8\u538b\uff08HP\uff09\u6da1\u8f6e\u8f6c\u5b50\u8fdb\u53e3\u6e29\u5ea6\u53ef\u4ee5\u66f4\u9ad8\uff0c\u4ece\u800c\u5b9e\u73b0\u66f4\u5c0f\uff08\u548c\u66f4\u8f7b\uff09\u7684\u6838\u5fc3\uff0c\u6f5c\u5728\u63d0\u9ad8\u6838\u5fc3\u70ed\u6548\u7387\u3002\u51cf\u5c11\u6838\u5fc3\u8d28\u91cf\u6d41\u91cf\u5f80\u5f80\u4f1a\u589e\u52a0\u4f4e\u538b\uff08LP\uff09\u6da1\u8f6e\u7684\u8d1f\u8377\uff0c\u56e0\u6b64\u53ef\u80fd\u9700\u8981\u989d\u5916\u7684\u7ea7\u6570\u6765\u51cf\u5c0f\u5e73\u5747\u7ea7\u8d1f\u8377\u5e76\u4fdd\u6301\u4f4e\u538b\u6da1\u8f6e\u7684\u6548\u7387\u3002\u51cf\u5c11\u6838\u5fc3\u6d41\u91cf\u8fd8\u4f1a\u589e\u52a0\u6db5\u9053\u6bd4\u3002\u8d85\u8fc75:1\u7684\u6db5\u9053\u6bd4\u8d8a\u6765\u8d8a\u5e38\u89c1\uff1b\u666e\u60e0PW1000G\u53d1\u52a8\u673a\u4e8e2016\u5e74\u6295\u5165\u5546\u4e1a\u670d\u52a1\uff0c\u5176\u6db5\u9053\u6bd4\u8fbe\u523012.5:1\u3002<\/p>\n\n\n\n<p>Further improvements in core thermal efficiency can be achieved by raising the overall pressure ratio of the core. Improvements in blade aerodynamics can reduce the number of extra compressor stages required, and variable geometry (i.e., <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Axial_compressor%23Bleed_air%2C_variable_stators\" target=\"_blank\" rel=\"noreferrer noopener\">stators<\/a>) enable high-pressure-ratio compressors to work surge-free at all throttle settings.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u901a\u8fc7\u63d0\u9ad8\u6838\u5fc3\u7684\u603b\u538b\u6bd4\uff0c\u53ef\u4ee5\u8fdb\u4e00\u6b65\u63d0\u9ad8\u6838\u5fc3\u7684\u70ed\u6548\u7387\u3002\u53f6\u7247\u7a7a\u6c14\u52a8\u529b\u5b66\u7684\u6539\u8fdb\u53ef\u4ee5\u51cf\u5c11\u6240\u9700\u7684\u989d\u5916\u538b\u7f29\u673a\u7ea7\u6570\uff0c\u800c\u53ef\u53d8\u51e0\u4f55\uff08\u5373\u9759\u5b50\uff09\u4f7f\u9ad8\u538b\u6bd4\u538b\u7f29\u673a\u80fd\u591f\u5728\u6240\u6709\u8282\u6d41\u9600\u8bbe\u7f6e\u4e0b\u65e0\u5598\u632f\u5730\u5de5\u4f5c\u3002<\/p>\n\n\n\n<div class=\"wp-block-buttons is-layout-flex wp-block-buttons-is-layout-flex\">\n<div class=\"wp-block-button\"><a class=\"wp-block-button__link wp-element-button\" href=\"https:\/\/www.zhihu.com\/pin\/1849395260205178880\">\u56fe3-4\uff08\u53d1\u5e03\u4e8e\u77e5\u4e4e\u60f3\u6cd5\uff09<\/a><\/div>\n<\/div>\n\n\n\n<p>The first (experimental) high-bypass turbofan engine was the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Lycoming_Engines\" target=\"_blank\" rel=\"noreferrer noopener\">AVCO-Lycoming<\/a> PLF1A-2, a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Honeywell_T55\" target=\"_blank\" rel=\"noreferrer noopener\">Honeywell T55<\/a> turboshaft-derived engine that was first run in February 1962. The PLF1A-2 had a 40 in diameter (100 cm) geared fan stage, produced a static thrust of 4,320 lb (1,960 kg),<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-Boyne2002-43\" target=\"_blank\" rel=\"noreferrer noopener\">[43]<\/a> and had a bypass ratio of 6:1.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-NASM-PLF1A-2-44\" target=\"_blank\" rel=\"noreferrer noopener\">[44]<\/a> The <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_TF39\" target=\"_blank\" rel=\"noreferrer noopener\">General Electric TF39<\/a> became the first production model, designed to power the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Lockheed_Corporation\" target=\"_blank\" rel=\"noreferrer noopener\">Lockheed<\/a> <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/C-5_Galaxy\" target=\"_blank\" rel=\"noreferrer noopener\">C-5 Galaxy<\/a> military transport aircraft.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-Neumann_2004_1984_pp228-230-22\" target=\"_blank\" rel=\"noreferrer noopener\">[22]<\/a> The civil <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_CF6\" target=\"_blank\" rel=\"noreferrer noopener\">General Electric CF6<\/a> engine used a derived design. Other high-bypass turbofans are the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_JT9D\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney JT9D<\/a>, the three-shaft <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_RB211\" target=\"_blank\" rel=\"noreferrer noopener\">Rolls-Royce RB211<\/a> and the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/CFM_International_CFM56\" target=\"_blank\" rel=\"noreferrer noopener\">CFM International CFM56<\/a>; also the smaller <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/TF34\" target=\"_blank\" rel=\"noreferrer noopener\">TF34<\/a>. More recent large high-bypass turbofans include the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_PW4000\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney PW4000<\/a>, the three-shaft <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_Trent\" target=\"_blank\" rel=\"noreferrer noopener\">Rolls-Royce Trent<\/a>, the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_GE90\" target=\"_blank\" rel=\"noreferrer noopener\">General Electric GE90<\/a>\/<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/GEnx\" target=\"_blank\" rel=\"noreferrer noopener\">GEnx<\/a> and the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/GP7000\" target=\"_blank\" rel=\"noreferrer noopener\">GP7000<\/a>, produced jointly by GE and P&amp;W.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u7b2c\u4e00\u53f0\uff08\u5b9e\u9a8c\u6027\uff09\u9ad8\u6db5\u9053\u6bd4\u6da1\u6247\u53d1\u52a8\u673a\u662fAVCO-Lycoming PLF1A-2\uff0c\u5b83\u662fHoneywell T55\u6da1\u8f74\u53d1\u52a8\u673a\u6539\u8fdb\u800c\u6765\uff0c\u4e8e1962\u5e742\u6708\u9996\u6b21\u8fd0\u884c\u3002PLF1A-2\u91c7\u7528\u76f4\u5f8440\u82f1\u5bf8\uff08100\u5398\u7c73\uff09\u7684\u9f7f\u8f6e\u98ce\u6247\u7ea7\uff0c\u9759\u6001\u63a8\u529b\u4e3a4,320\u78c5\uff081,960\u516c\u65a4\uff09\uff0c\u6db5\u9053\u6bd4\u4e3a6:1\u3002\u901a\u7528\u7535\u6c14TF39\u6210\u4e3a\u7b2c\u4e00\u6b3e\u91cf\u4ea7\u578b\u53f7\uff0c\u4e13\u4e3a\u63a8\u52a8\u6d1b\u514b\u5e0c\u5fb7C-5\u94f6\u6cb3\u519b\u7528\u8fd0\u8f93\u673a\u800c\u8bbe\u8ba1\u3002\u6c11\u7528\u7684\u901a\u7528\u7535\u6c14CF6\u53d1\u52a8\u673a\u91c7\u7528\u4e86\u884d\u751f\u8bbe\u8ba1\u3002\u5176\u4ed6\u9ad8\u6db5\u9053\u6bd4\u6da1\u6247\u53d1\u52a8\u673a\u5305\u62ec\u666e\u60e0JT9D\uff0c\u4e09\u8f74\u5f0f\u52b3\u65af\u83b1\u65afRB211\u548cCFM\u56fd\u9645CFM56\uff0c\u4ee5\u53ca\u66f4\u5c0f\u7684TF34\u3002\u66f4\u8fd1\u671f\u7684\u5927\u578b\u9ad8\u6db5\u9053\u6bd4\u6da1\u6247\u53d1\u52a8\u673a\u5305\u62ec\u666e\u60e0PW4000\uff0c\u4e09\u8f74\u5f0f\u52b3\u65af\u83b1\u65af\u7279\u4f26\u7279\uff0c\u901a\u7528\u7535\u6c14GE90\/GEnx\u548cGE\u4e0eP&amp;W\u8054\u5408\u751f\u4ea7\u7684GP7000\u3002<\/p>\n\n\n\n<p>The lower the specific thrust of a turbofan, the lower the mean jet outlet velocity, which in turn translates into a high <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Thrust_lapse\" target=\"_blank\" rel=\"noreferrer noopener\">thrust lapse rate<\/a> (i.e. decreasing thrust with increasing flight speed). See technical discussion below, item 2. Consequently, an engine sized to propel an aircraft at high subsonic flight speed (e.g., Mach 0.83) generates a relatively high thrust at low flight speed, thus enhancing runway performance. Low specific thrust engines tend to have a high bypass ratio, but this is also a function of the temperature of the turbine system.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6da1\u6247\u53d1\u52a8\u673a\u7684\u6bd4\u63a8\u529b\u8d8a\u4f4e\uff0c\u55b7\u6d41\u51fa\u53e3\u901f\u5ea6\u8d8a\u4f4e\uff0c\u8fd9\u53cd\u8fc7\u6765\u5bfc\u81f4\u63a8\u529b\u9012\u51cf\u7387\u9ad8\uff08\u5373\u968f\u7740\u98de\u884c\u901f\u5ea6\u589e\u52a0\u63a8\u529b\u51cf\u5c0f\uff09\u3002\u8bf7\u53c2\u89c1\u4e0b\u9762\u6280\u672f\u8ba8\u8bba\uff0c2\u9879\u3002\u56e0\u6b64\uff0c\u4e3a\u4e86\u4f7f\u98de\u673a\u4ee5\u9ad8\u4e9a\u97f3\u901f\u98de\u884c\uff08\u4f8b\u5982Mach 0.83\uff09\uff0c\u53d1\u52a8\u673a\u9700\u8981\u4ea7\u751f\u76f8\u5bf9\u8f83\u9ad8\u7684\u63a8\u529b\u4ee5\u5728\u4f4e\u901f\u98de\u884c\u65f6\u63d0\u5347\u8d77\u98de\u8ddd\u79bb\u6027\u80fd\u3002\u4f4e\u6bd4\u63a8\u529b\u53d1\u52a8\u673a\u5f80\u5f80\u5177\u6709\u9ad8\u6db5\u9053\u6bd4\uff0c\u4f46\u8fd9\u4e5f\u4e0e\u6da1\u8f6e\u7cfb\u7edf\u7684\u6e29\u5ea6\u6709\u5173\u3002<\/p>\n\n\n\n<p>The turbofans on twin-engined transport aircraft produce enough take-off thrust to continue a take-off on one engine if the other engine shuts down after a critical point in the take-off run. From that point on the aircraft has less than half the thrust compared to two operating engines because the non-functioning engine is a source of drag. Modern twin engined airliners normally climb very steeply immediately after take-off. If one engine shuts down, the climb-out is much shallower, but sufficient to clear obstacles in the flightpath.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u53cc\u53d1\u8fd0\u8f93\u673a\u4e0a\u7684\u6da1\u6247\u53d1\u52a8\u673a\u4ea7\u751f\u8db3\u591f\u7684\u8d77\u98de\u63a8\u529b\uff0c\u5982\u679c\u53e6\u4e00\u4e2a\u53d1\u52a8\u673a\u5728\u8d77\u98de\u8fc7\u7a0b\u4e2d\u7684\u4e00\u4e2a\u4e34\u754c\u70b9\u540e\u5173\u95ed\uff0c\u5b83\u53ef\u4ee5\u7ee7\u7eed\u5728\u4e00\u4e2a\u53d1\u52a8\u673a\u4e0a\u8d77\u98de\u3002\u4ece\u90a3\u65f6\u8d77\uff0c\u98de\u673a\u7684\u63a8\u529b\u8fd8\u4e0d\u5230\u4e24\u4e2a\u8fd0\u884c\u4e2d\u7684\u53d1\u52a8\u673a\u7684\u4e00\u534a\uff0c\u56e0\u4e3a\u4e0d\u5de5\u4f5c\u7684\u53d1\u52a8\u673a\u662f\u963b\u529b\u7684\u6765\u6e90\u3002\u73b0\u4ee3\u53cc\u5f15\u64ce\u5ba2\u673a\u901a\u5e38\u5728\u8d77\u98de\u540e\u7acb\u5373\u6025\u5267\u722c\u5347\u3002\u5982\u679c\u4e00\u4e2a\u5f15\u64ce\u5173\u95ed\uff0c\u722c\u5347\u7684\u5e45\u5ea6\u4f1a\u5c0f\u5f97\u591a\uff0c\u4f46\u8db3\u4ee5\u6e05\u9664\u98de\u884c\u8def\u7ebf\u4e0a\u7684\u969c\u788d\u7269\u3002<\/p>\n\n\n\n<p>The Soviet Union&#8217;s engine technology was less advanced than the West&#8217;s, and its first wide-body aircraft, the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Ilyushin_Il-86\" target=\"_blank\" rel=\"noreferrer noopener\">Ilyushin Il-86<\/a>, was powered by low-bypass engines. The <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Yakovlev_Yak-42\" target=\"_blank\" rel=\"noreferrer noopener\">Yakovlev Yak-42<\/a>, a medium-range, rear-engined aircraft seating up to 120 passengers, introduced in 1980, was the first Soviet aircraft to use high-bypass engines.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u82cf\u8054\u7684\u53d1\u52a8\u673a\u6280\u672f\u4e0d\u5982\u897f\u65b9\u5148\u8fdb\uff0c\u5b83\u7684\u7b2c\u4e00\u67b6\u5bbd\u4f53\u98de\u673a\u4f0a\u5c1486 (Ilyushin Il-86)\u4f7f\u7528\u7684\u662f\u4f4e\u6db5\u9053\u6bd4\u53d1\u52a8\u673a\u3002\u96c5\u79d1\u592b\u5217\u592b\u96c5\u514b-42\u662f\u4e00\u79cd\u53ef\u5bb9\u7eb3120\u540d\u4e58\u5ba2\u7684\u4e2d\u7a0b\u540e\u7f6e\u53d1\u52a8\u673a\u98de\u673a\uff0c\u4e8e1980\u5e74\u63a8\u51fa\uff0c\u662f\u7b2c\u4e00\u79cd\u4f7f\u7528\u9ad8\u6db5\u9053\u6bd4\u53d1\u52a8\u673a\u7684\u82cf\u8054\u98de\u673a\u3002<\/p>\n\n\n\n<p>\u3010<strong>\u4ee3\u8868\u6027\u7684\u5927\u63a8\u529b\u6da1\u6247\u53d1\u52a8\u673a \u56fe\u96c6<\/strong>\u3011<\/p>\n\n\n\n<p><a target=\"_blank\" href=\"https:\/\/www.zhihu.com\/pin\/1692329290111238145\" rel=\"noreferrer noopener\">\u7b2c\u4e00\u90e8\u5206\u8bf7\u70b9\u51fb\u8fd9\u91cc\u8bbf\u95ee\u200b<\/a><\/p>\n\n\n\n<p><a target=\"_blank\" href=\"https:\/\/www.zhihu.com\/pin\/1692692590712029184\" rel=\"noreferrer noopener\">\u7b2c\u4e8c\u90e8\u5206\u8bf7\u70b9\u51fb\u8fd9\u91cc\u8bbf\u95ee\u200b<\/a><\/p>\n\n\n\n<h2 class=\"wp-block-heading\" id=\"h_659034614_12\">4. \u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\u914d\u7f6e | Turbofan configurations<\/h2>\n\n\n\n<p>Turbofan engines come in a variety of engine configurations. For a given engine cycle (i.e., same airflow, bypass ratio, fan pressure ratio, overall pressure ratio and HP turbine rotor inlet temperature), the choice of turbofan configuration has little impact upon the design point performance (e.g., net thrust, SFC), as long as overall component performance is maintained. Off-design performance and stability is, however, affected by engine configuration.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6da1\u6247\u53d1\u52a8\u673a\u6709\u591a\u79cd\u53d1\u52a8\u673a\u914d\u7f6e\u3002\u5bf9\u4e8e\u7ed9\u5b9a\u7684\u53d1\u52a8\u673a\u5faa\u73af(\u5373\u76f8\u540c\u7684\u6c14\u6d41\u3001\u6db5\u9053\u6bd4\u3001\u98ce\u6247\u538b\u529b\u6bd4\u3001\u603b\u538b\u6bd4\u548c\u9ad8\u538b\u6da1\u8f6e\u8f6c\u5b50\u5165\u53e3\u6e29\u5ea6)\uff0c\u53ea\u8981\u4fdd\u6301\u6574\u4f53\u90e8\u4ef6\u6027\u80fd\uff0c\u6da1\u6247\u914d\u7f6e\u7684\u9009\u62e9\u5bf9\u8bbe\u8ba1\u70b9\u6027\u80fd(\u5982\u51c0\u63a8\u529b\u3001SFC)\u7684\u5f71\u54cd\u5f88\u5c0f\u3002\u7136\u800c\uff0c\u975e\u8bbe\u8ba1\u6027\u80fd\u548c\u7a33\u5b9a\u6027\u53d7\u5230\u53d1\u52a8\u673a\u914d\u7f6e\u7684\u5f71\u54cd\u3002<\/p>\n\n\n\n<p>The basic element of a turbofan is a <strong>spool<\/strong>, a single combination of fan\/compressor, turbine and shaft rotating at a single speed. For a given pressure ratio, the surge margin can be increased by two different design paths:<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6da1\u8f6e\u98ce\u6247\u7684\u57fa\u672c\u90e8\u4ef6\u662f\u4e00\u4e2a\u9600\u82af\uff0c\u5b83\u662f\u98ce\u6247\/\u538b\u7f29\u673a\u3001\u6da1\u8f6e\u548c\u4ee5\u5355\u4e00\u901f\u5ea6\u65cb\u8f6c\u7684\u8f74\u7684\u5355\u4e00\u7ec4\u5408\u3002\u5bf9\u4e8e\u7ed9\u5b9a\u7684\u538b\u529b\u6bd4\uff0c\u53ef\u4ee5\u901a\u8fc7\u4e24\u79cd\u4e0d\u540c\u7684\u8bbe\u8ba1\u8def\u5f84\u6765\u589e\u52a0\u5598\u632f\u88d5\u5ea6:<\/p>\n\n\n\n<ol class=\"wp-block-list\">\n<li>Splitting the compressor into two smaller spools rotating at different speeds, as with the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_J57\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney J57<\/a>; or<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5c06\u538b\u7f29\u673a\u5206\u6210\u4e24\u4e2a\u8f83\u5c0f\u7684\u4ee5\u4e0d\u540c\u901f\u5ea6\u65cb\u8f6c\u7684\u7ebf\u8f74\uff0c\u5982\u666e\u60e0J57;\u6216<\/li>\n\n\n\n<li>Making the stator vane pitch adjustable, typically in the front stages, as with the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/J79\" target=\"_blank\" rel=\"noreferrer noopener\">J79<\/a>.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u4f7f\u5b9a\u5b50\u53f6\u7247\u87ba\u8ddd\u53ef\u8c03\uff0c\u901a\u5e38\u5728\u524d\u7ea7\uff0c\u5982J79\u3002<\/li>\n<\/ol>\n\n\n\n<p>Most modern western civil turbofans employ a relatively high-pressure-ratio high-pressure (HP) compressor, with many rows of variable stators to control surge margin at low rpm. In the three-spool <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_RB211\" target=\"_blank\" rel=\"noreferrer noopener\">RB211<\/a>\/<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_Trent\" target=\"_blank\" rel=\"noreferrer noopener\">Trent<\/a> the core compression system is split into two, with the IP compressor, which supercharges the HP compressor, being on a different coaxial shaft and driven by a separate (IP) turbine. As the HP compressor has a modest pressure ratio its speed can be reduced surge-free, without employing variable geometry. However, because a shallow IP compressor working line is inevitable, the IPC has one stage of variable geometry on all variants except the \u2212535, which has none.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-45\" target=\"_blank\" rel=\"noreferrer noopener\">[45]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u5927\u591a\u6570\u73b0\u4ee3\u897f\u65b9\u6c11\u7528\u6da1\u8f6e\u98ce\u6247\u91c7\u7528\u76f8\u5bf9\u9ad8\u538b\u529b\u6bd4\u7684\u9ad8\u538b(HP)\u538b\u7f29\u673a\uff0c\u914d\u6709\u591a\u6392\u53ef\u53d8\u5b9a\u5b50\u6765\u63a7\u5236\u4f4e\u8f6c\u901f\u65f6\u7684\u5598\u632f\u88d5\u5ea6\u3002\u5728\u4e09\u8f74RB211\/Trent\u4e2d\uff0c\u6838\u5fc3\u538b\u7f29\u7cfb\u7edf\u5206\u4e3a\u4e24\u4e2a\uff0c\u5176\u4e2dIP\u538b\u7f29\u673a\u589e\u538bHP\u538b\u7f29\u673a\uff0c\u4f4d\u4e8e\u4e0d\u540c\u7684\u540c\u8f74\u8f74\u4e0a\uff0c\u7531\u5355\u72ec\u7684(IP)\u6da1\u8f6e\u9a71\u52a8\u3002\u7531\u4e8eHP\u538b\u7f29\u673a\u5177\u6709\u9002\u5ea6\u7684\u538b\u529b\u6bd4\uff0c\u5b83\u7684\u901f\u5ea6\u53ef\u4ee5\u5728\u65e0\u6d6a\u6d8c\u7684\u60c5\u51b5\u4e0b\u964d\u4f4e\uff0c\u800c\u65e0\u9700\u91c7\u7528\u53ef\u53d8\u51e0\u4f55\u5f62\u72b6\u3002\u7136\u800c\uff0c\u7531\u4e8e\u6d45IP\u538b\u7f29\u673a\u5de5\u4f5c\u7ebf\u662f\u4e0d\u53ef\u907f\u514d\u7684\uff0cIPC\u5728\u6240\u6709\u53d8\u4f53\u4e0a\u90fd\u6709\u4e00\u4e2a\u53ef\u53d8\u51e0\u4f55\u9636\u6bb5\uff0c\u9664\u4e86\u2212535\uff0c\u5b83\u6ca1\u6709\u3002[45]<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_13\">4.1 \u5355\u8f74\u6da1\u6247 | Single-shaft turbofan<\/h3>\n\n\n\n<p>Although far from common, the single-shaft turbofan is probably the simplest configuration, comprising a fan and high-pressure compressor driven by a single turbine unit, all on the same spool. The <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Snecma_M53\" target=\"_blank\" rel=\"noreferrer noopener\">Snecma M53<\/a>, which powers <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Dassault_Mirage_2000\" target=\"_blank\" rel=\"noreferrer noopener\">Dassault Mirage 2000<\/a> fighter aircraft, is an example of a single-shaft turbofan. Despite the simplicity of the turbomachinery configuration, the M53 requires a variable area mixer to facilitate part-throttle operation.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u867d\u7136\u8fdc\u4e0d\u5e38\u89c1\uff0c\u4f46\u5355\u8f74\u6da1\u6247\u53ef\u80fd\u662f\u6700\u7b80\u5355\u7684\u914d\u7f6e\uff0c\u5305\u62ec\u4e00\u4e2a\u98ce\u6247\u548c\u9ad8\u538b\u538b\u6c14\u673a\uff0c\u7531\u4e00\u4e2a\u5355\u4e00\u7684\u6da1\u8f6e\u5355\u5143\u9a71\u52a8\uff0c\u90fd\u5728\u540c\u4e00\u4e2a\u8f74\u4e0a\u3002\u4e3a\u8fbe\u7d22\u5e7b\u5f712000\u6218\u6597\u673a\u63d0\u4f9b\u52a8\u529b\u7684\u65af\u5948\u514b\u739bM53\u662f\u5355\u8f74\u6da1\u6247\u53d1\u52a8\u673a\u7684\u4e00\u4e2a\u4f8b\u5b50\u3002\u5c3d\u7ba1\u6da1\u8f6e\u673a\u68b0\u914d\u7f6e\u7b80\u5355\uff0cM53\u9700\u8981\u4e00\u4e2a\u53ef\u53d8\u533a\u57df\u6df7\u5408\u5668\uff0c\u4ee5\u65b9\u4fbf\u90e8\u5206\u8282\u6d41\u64cd\u4f5c\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_14\">4.2 \u98ce\u6247\u5728\u540e\u7684\u6da1\u6247\u53d1\u52a8\u673a | Aft-fan turbofan<\/h3>\n\n\n\n<p>One of the earliest turbofans was a derivative of the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_J79\" target=\"_blank\" rel=\"noreferrer noopener\">General Electric J79<\/a> turbojet, known as the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_CJ805\" target=\"_blank\" rel=\"noreferrer noopener\">CJ805-23<\/a>, which featured an integrated aft fan\/low-pressure (LP) turbine unit located in the turbojet exhaust jetpipe. Hot gas from the turbojet turbine exhaust expanded through the LP turbine, the fan blades being a radial extension of the turbine blades. This arrangement introduces an additional gas leakage path compared to a front-fan configuration and was a problem with this engine with higher-pressure turbine gas leaking into the fan airflow.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-46\" target=\"_blank\" rel=\"noreferrer noopener\">[46]<\/a> An aft-fan configuration was later used for the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_GE36\" target=\"_blank\" rel=\"noreferrer noopener\">General Electric GE36<\/a> UDF (propfan) demonstrator of the early 1980s.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6700\u65e9\u7684\u6da1\u6247\u53d1\u52a8\u673a\u4e4b\u4e00\u662f\u901a\u7528\u7535\u6c14J79\u6da1\u55b7\u53d1\u52a8\u673a\u7684\u884d\u751f\u578b\uff0c\u88ab\u79f0\u4e3aCJ805-23\uff0c\u5176\u7279\u70b9\u662f\u5728\u6da1\u55b7\u53d1\u52a8\u673a\u6392\u6c14\u55b7\u5c04\u7ba1\u4e2d\u5b89\u88c5\u4e86\u4e00\u4e2a\u96c6\u6210\u7684\u5c3e\u90e8\u98ce\u6247\/\u4f4e\u538b(LP)\u6da1\u8f6e\u5355\u5143\u3002\u70ed\u6c14\u4f53\u4ece\u6da1\u8f6e\u55b7\u5c04\u6da1\u8f6e\u6392\u6c14\u81a8\u80c0\u901a\u8fc7\u4f4e\u538b\u6da1\u8f6e\uff0c\u98ce\u6247\u53f6\u7247\u662f\u6da1\u8f6e\u53f6\u7247\u7684\u5f84\u5411\u5ef6\u4f38\u3002\u4e0e\u524d\u98ce\u6247\u914d\u7f6e\u76f8\u6bd4\uff0c\u8fd9\u79cd\u5e03\u7f6e\u5f15\u5165\u4e86\u4e00\u4e2a\u989d\u5916\u7684\u6c14\u4f53\u6cc4\u6f0f\u8def\u5f84\uff0c\u8fd9\u662f\u9ad8\u538b\u6da1\u8f6e\u6c14\u4f53\u6cc4\u6f0f\u5230\u98ce\u6247\u6c14\u6d41\u4e2d\u7684\u53d1\u52a8\u673a\u7684\u4e00\u4e2a\u95ee\u9898\u3002[46]\u540e\u98ce\u6247\u914d\u7f6e\u540e\u6765\u7528\u4e8e1980\u5e74\u4ee3\u65e9\u671f\u901a\u7528\u7535\u6c14GE36 UDF (profan)\u6f14\u793a\u673a\u3002<\/p>\n\n\n\n<p>In 1971 a concept was put forward by the NASA Lewis Research Center for a supersonic transport engine which operated as an aft-fan turbofan at take-off and subsonic speeds and a turbojet at higher speeds. This would give the low noise and high thrust characteristics of a turbofan at take-off, together with turbofan high propulsive efficiency at subsonic flight speeds. It would have the high propulsive efficiency of a turbojet at supersonic cruise speeds.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-47\" target=\"_blank\" rel=\"noreferrer noopener\">[47]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a1971\u5e74\uff0c\u7f8e\u56fd\u56fd\u5bb6\u822a\u7a7a\u822a\u5929\u5c40\u5218\u6613\u65af\u7814\u7a76\u4e2d\u5fc3\u63d0\u51fa\u4e86\u4e00\u79cd\u8d85\u97f3\u901f\u8fd0\u8f93\u53d1\u52a8\u673a\u7684\u6982\u5ff5\uff0c\u8fd9\u79cd\u53d1\u52a8\u673a\u5728\u8d77\u98de\u548c\u4e9a\u97f3\u901f\u65f6\u4f5c\u4e3a\u540e\u6247\u6da1\u6247\u53d1\u52a8\u673a\uff0c\u5728\u66f4\u9ad8\u7684\u901f\u5ea6\u4e0b\u4f5c\u4e3a\u6da1\u8f6e\u55b7\u6c14\u53d1\u52a8\u673a\u3002\u8fd9\u5c06\u4f7f\u6da1\u6247\u53d1\u52a8\u673a\u5728\u8d77\u98de\u65f6\u5177\u6709\u4f4e\u566a\u97f3\u548c\u9ad8\u63a8\u529b\u7279\u6027\uff0c\u540c\u65f6\u5728\u4e9a\u97f3\u901f\u98de\u884c\u901f\u5ea6\u4e0b\u5177\u6709\u9ad8\u63a8\u8fdb\u6548\u7387\u3002\u5b83\u5c06\u5728\u8d85\u97f3\u901f\u5de1\u822a\u901f\u5ea6\u4e0b\u5177\u6709\u6da1\u8f6e\u55b7\u6c14\u53d1\u52a8\u673a\u7684\u9ad8\u63a8\u8fdb\u6548\u7387\u3002[47]<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_15\">4.3 \u57fa\u672c\u7684\u53cc\u8f6c\u5b50 | Basic two-spool<\/h3>\n\n\n\n<div class=\"wp-block-buttons is-layout-flex wp-block-buttons-is-layout-flex\">\n<div class=\"wp-block-button\"><a class=\"wp-block-button__link wp-element-button\" href=\"https:\/\/www.zhihu.com\/pin\/1849394761980575746\">\u56fe4-1\uff08\u53d1\u5e03\u4e8e\u77e5\u4e4e\u60f3\u6cd5\uff09<\/a><\/div>\n<\/div>\n\n\n\n<p>Many turbofans have at least basic two-spool configuration where the fan is on a separate low pressure (LP) spool, running concentrically with the compressor or high pressure (HP) spool; the LP spool runs at a lower <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Angular_velocity\" target=\"_blank\" rel=\"noreferrer noopener\">angular velocity<\/a>, while the HP spool turns faster and its compressor further compresses part of the air for combustion.[<em><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Wikipedia%3ACitation_needed\" target=\"_blank\" rel=\"noreferrer noopener\">citation needed<\/a><\/em>] The <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_BR700\" target=\"_blank\" rel=\"noreferrer noopener\">BR710<\/a> is typical of this configuration. At the smaller thrust sizes, instead of all-axial blading, the HP compressor configuration may be axial-centrifugal (e.g., <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/CFE_CFE738\" target=\"_blank\" rel=\"noreferrer noopener\">CFE CFE738<\/a>), double-centrifugal or even <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Mixed_flow_compressor\" target=\"_blank\" rel=\"noreferrer noopener\">diagonal\/centrifugal<\/a> (e.g. <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_Canada_PW600\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney Canada PW600<\/a>).<br>\u53c2\u8003\u8bd1\u6587\uff1a\u8bb8\u591a\u6da1\u8f6e\u98ce\u6247\u81f3\u5c11\u6709\u57fa\u672c\u7684\u53cc\u8f74\u914d\u7f6e\uff0c\u98ce\u6247\u5728\u4e00\u4e2a\u5355\u72ec\u7684\u4f4e\u538b(LP)\u8f74\u4e0a\uff0c\u4e0e\u538b\u7f29\u673a\u6216\u9ad8\u538b(HP)\u8f74\u540c\u5fc3\u8fd0\u884c;\u4f4e\u538b\u9600\u82af\u4ee5\u8f83\u4f4e\u7684\u89d2\u901f\u5ea6\u8fd0\u884c\uff0c\u800c\u9ad8\u538b\u9600\u82af\u65cb\u8f6c\u5f97\u66f4\u5feb\uff0c\u5176\u538b\u7f29\u673a\u8fdb\u4e00\u6b65\u538b\u7f29\u90e8\u5206\u7a7a\u6c14\u4ee5\u4f9b\u71c3\u70e7\u3002BR710\u662f\u5178\u578b\u7684\u8fd9\u79cd\u914d\u7f6e\u3002\u5728\u63a8\u529b\u8f83\u5c0f\u7684\u60c5\u51b5\u4e0b\uff0c\u9ad8\u538b\u538b\u7f29\u673a\u7684\u914d\u7f6e\u53ef\u4ee5\u662f\u8f74\u5411\u79bb\u5fc3(\u4f8b\u5982CFE CFE738)\u3001\u53cc\u79bb\u5fc3\u751a\u81f3\u662f\u5bf9\u89d2\/\u79bb\u5fc3(\u4f8b\u5982\u666e\u60e0\u52a0\u62ff\u5927PW600)\uff0c\u800c\u4e0d\u662f\u5168\u8f74\u5411\u53f6\u7247\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_16\">4.4 \u63d0\u9ad8\u7684\u53cc\u8f6c\u5b50 | Boosted two-spool<\/h3>\n\n\n\n<p>Higher overall pressure ratios can be achieved by either raising the HP compressor pressure ratio or adding compressor (non-bypass) stages to the LP spool, between the fan and the HP compressor, to boost the latter. All of the large American turbofans (e.g. <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_CF6\" target=\"_blank\" rel=\"noreferrer noopener\">General Electric CF6<\/a>, <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/GE90\" target=\"_blank\" rel=\"noreferrer noopener\">GE90<\/a>, <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_GE9X\" target=\"_blank\" rel=\"noreferrer noopener\">GE9X<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/GEnx\" target=\"_blank\" rel=\"noreferrer noopener\">GEnx<\/a> plus <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_JT9D\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney JT9D<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_PW4000\" target=\"_blank\" rel=\"noreferrer noopener\">PW4000<\/a>) use booster stages. The Rolls-Royce BR715 is another example. The high bypass ratios used in modern civil turbofans tend to reduce the relative diameter of the booster stages, reducing their mean tip speed. Consequently, more booster stages are required to develop the necessary pressure rise.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u66f4\u9ad8\u7684\u603b\u538b\u529b\u6bd4\u53ef\u4ee5\u901a\u8fc7\u63d0\u9ad8\u9ad8\u538b\u538b\u7f29\u673a\u538b\u529b\u6bd4\u6216\u5728\u98ce\u673a\u548c\u9ad8\u538b\u538b\u7f29\u673a\u4e4b\u95f4\u7684\u4f4e\u538b\u9600\u82af\u4e0a\u589e\u52a0\u538b\u7f29\u673a(\u975e\u65c1\u8def)\u7ea7\u6765\u5b9e\u73b0\uff0c\u4ee5\u63d0\u9ad8\u540e\u8005\u3002\u6240\u6709\u7684\u5927\u578b\u7f8e\u56fd\u6da1\u8f6e\u98ce\u6247(\u4f8b\u5982\u901a\u7528\u7535\u6c14\u7684CF6, GE90, GE9X\u548cGEnx\u52a0\u4e0a\u666e\u60e0\u516c\u53f8\u7684JT9D\u548cPW4000)\u90fd\u4f7f\u7528\u52a9\u63a8\u5668\u7ea7\u3002\u52b3\u65af\u83b1\u65afBR715\u662f\u53e6\u4e00\u4e2a\u4f8b\u5b50\u3002\u73b0\u4ee3\u6c11\u7528\u6da1\u6247\u91c7\u7528\u7684\u9ad8\u6db5\u9053\u6bd4\u5f80\u5f80\u4f1a\u51cf\u5c0f\u52a9\u63a8\u5668\u7ea7\u7684\u76f8\u5bf9\u76f4\u5f84\uff0c\u4ece\u800c\u964d\u4f4e\u5176\u5e73\u5747\u53f6\u5c16\u901f\u5ea6\u3002\u56e0\u6b64\uff0c\u9700\u8981\u66f4\u591a\u7684\u52a9\u63a8\u5668\u7ea7\u6765\u4ea7\u751f\u5fc5\u8981\u7684\u538b\u529b\u4e0a\u5347\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_17\">4.5 \u4e09\u8f6c\u5b50 | Three-spool<\/h3>\n\n\n\n<p>Rolls-Royce chose a three-spool configuration for their large civil turbofans (i.e. the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_RB211\" target=\"_blank\" rel=\"noreferrer noopener\">RB211<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_Trent\" target=\"_blank\" rel=\"noreferrer noopener\">Trent<\/a> families), where the booster stages of a boosted two-spool configuration are separated into an intermediate pressure (IP) spool, driven by its own turbine. The first three-spool engine was the earlier <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_RB.203_Trent\" target=\"_blank\" rel=\"noreferrer noopener\">Rolls-Royce RB.203 Trent<\/a> of 1967.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u7f57\u5c14\u65af\u00b7\u7f57\u4f0a\u65af\u4e3a\u4ed6\u4eec\u7684\u5927\u578b\u6c11\u7528\u6da1\u8f6e\u98ce\u6247(\u5373RB211\u548cTrent\u7cfb\u5217)\u9009\u62e9\u4e86\u4e09\u8f74\u914d\u7f6e\uff0c\u5176\u4e2d\u589e\u538b\u7684\u4e24\u8f74\u914d\u7f6e\u7684\u589e\u538b\u7ea7\u88ab\u5206\u79bb\u6210\u4e00\u4e2a\u4e2d\u538b(IP)\u8f74\uff0c\u7531\u81ea\u5df1\u7684\u6da1\u8f6e\u673a\u9a71\u52a8\u3002\u7b2c\u4e00\u4e2a\u4e09\u8f74\u53d1\u52a8\u673a\u662f1967\u5e74\u65e9\u671f\u7684\u52b3\u65af\u83b1\u65afRB.203 Trent\u3002<\/p>\n\n\n\n<p>The <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Garrett_ATF3\" target=\"_blank\" rel=\"noreferrer noopener\">Garrett ATF3<\/a>, powering the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Dassault_Falcon_20\" target=\"_blank\" rel=\"noreferrer noopener\">Dassault Falcon 20<\/a> business jet, has an unusual three spool layout with an aft spool not concentric with the two others.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u4e3a\u8fbe\u7d22\u730e\u9e7020\u516c\u52a1\u673a\u63d0\u4f9b\u52a8\u529b\u7684\u52a0\u52d2\u7279ATF3\u53d1\u52a8\u673a\u91c7\u7528\u4e86\u4e0d\u540c\u5bfb\u5e38\u7684\u4e09\u8f74\u5e03\u5c40\uff0c\u5176\u4e2d\u4e00\u4e2a\u540e\u8f74\u4e0e\u53e6\u5916\u4e24\u4e2a\u8f74\u4e0d\u540c\u8f74\u3002<\/p>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Ivchenko-Progress\" target=\"_blank\" rel=\"noreferrer noopener\">Ivchenko Design Bureau<\/a> chose the same configuration as Rolls-Royce for their <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Lotarev_D-36\" target=\"_blank\" rel=\"noreferrer noopener\">Lotarev D-36<\/a> engine, followed by <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Progress_D-18T\" target=\"_blank\" rel=\"noreferrer noopener\">Lotarev\/Progress D-18T<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Progress_D-436\" target=\"_blank\" rel=\"noreferrer noopener\">Progress D-436<\/a>.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u4f0a\u592b\u7434\u79d1\u8bbe\u8ba1\u5c40\u4e3a\u4ed6\u4eec\u7684Lotarev D-36\u53d1\u52a8\u673a\u9009\u62e9\u4e86\u4e0e\u52b3\u65af\u83b1\u65af\u76f8\u540c\u7684\u914d\u7f6e\uff0c\u968f\u540e\u662fLotarev\/Progress D-18T\u548cProgress D-436\u3002<\/p>\n\n\n\n<p>The <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbo-Union_RB199\" target=\"_blank\" rel=\"noreferrer noopener\">Turbo-Union RB199<\/a> military turbofan also has a three-spool configuration, as do the military <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Kuznetsov_NK-25\" target=\"_blank\" rel=\"noreferrer noopener\">Kuznetsov NK-25<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Kuznetsov_NK-32\" target=\"_blank\" rel=\"noreferrer noopener\">NK-321<\/a>.<br>\u53c2\u8003\u8bd1\u6587\uff1aTurbo-Union RB199\u519b\u7528\u6da1\u6247\u53d1\u52a8\u673a\u4e5f\u91c7\u7528\u4e09\u8f74\u914d\u7f6e\uff0c\u4e0e\u519b\u7528\u5e93\u5179\u6d85\u4f50\u592bNK-25\u548cNK-321\u4e00\u6837\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_18\">4.6 \u9f7f\u8f6e\u98ce\u6247 | Geared fan<\/h3>\n\n\n\n<p><em>Main article: <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Geared_turbofan\" target=\"_blank\" rel=\"noreferrer noopener\">Geared turbofan<\/a><\/em><br><em>\u4e3b\u6761\u76ee\uff1a\u9f7f\u8f6e\u4f20\u52a8\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a<\/em><\/p>\n\n\n\n<div class=\"wp-block-buttons is-layout-flex wp-block-buttons-is-layout-flex\">\n<div class=\"wp-block-button\"><a class=\"wp-block-button__link wp-element-button\" href=\"https:\/\/www.zhihu.com\/pin\/1849394168608202753\">\u56fe4-2\uff08\u53d1\u5e03\u4e8e\u77e5\u4e4e\u60f3\u6cd5\uff09<\/a><\/div>\n<\/div>\n\n\n\n<p>As bypass ratio increases, the fan blade tip speed increases relative to the LPT blade speed. This will reduce the LPT blade speed, requiring more turbine stages to extract enough energy to drive the fan. Introducing a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Epicyclic_gearing\" target=\"_blank\" rel=\"noreferrer noopener\">(planetary) reduction gearbox<\/a>, with a suitable gear ratio, between the LP shaft and the fan enables both the fan and LP turbine to operate at their optimum speeds. Examples of this configuration are the long-established <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Garrett_TFE731\" target=\"_blank\" rel=\"noreferrer noopener\">Garrett TFE731<\/a>, the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Honeywell_ALF_502\" target=\"_blank\" rel=\"noreferrer noopener\">Honeywell ALF 502<\/a>\/507, and the recent <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney_PW1000G\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney PW1000G<\/a>.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5f53\u65c1\u901a\u6bd4\u589e\u52a0\u65f6\uff0c\u98ce\u6247\u53f6\u5c16\u901f\u5ea6\u76f8\u5bf9\u4e8e\u4f4e\u538b\u6da1\u8f6e\u53f6\u901f\u5ea6\u589e\u52a0\u3002\u8fd9\u5c06\u51cf\u4f4e\u538b\u6da1\u8f6e\u53f6\u901f\u5ea6\uff0c\u9700\u8981\u66f4\u591a\u7684\u6da1\u8f6e\u7ea7\u6765\u63d0\u53d6\u8db3\u591f\u7684\u80fd\u91cf\u6765\u9a71\u52a8\u98ce\u6247\u3002\u901a\u8fc7\u5728\u4f4e\u538b\u8f74\u548c\u98ce\u6247\u4e4b\u95f4\u5f15\u5165\uff08\u884c\u661f\u5f0f\uff09\u51cf\u901f\u5668\uff0c\u5177\u6709\u5408\u9002\u7684\u9f7f\u8f6e\u6bd4\uff0c\u53ef\u4ee5\u4f7f\u98ce\u6247\u548c\u4f4e\u538b\u6da1\u8f6e\u4ee5\u6700\u4f73\u901f\u5ea6\u8fd0\u884c\u3002\u8fd9\u79cd\u914d\u7f6e\u7684\u4f8b\u5b50\u6709\u5386\u53f2\u60a0\u4e45\u7684Garrett TFE731\u3001Honeywell ALF 502\/507\uff0c\u4ee5\u53ca\u6700\u8fd1\u7684Pratt &amp; Whitney PW1000G\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_19\">4.7 \u519b\u7528\u6da1\u6247\u53d1\u52a8\u673a | Military turbofans<\/h3>\n\n\n\n<p>Most of the configurations discussed above are used in civilian turbofans, while modern military turbofans (e.g., <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Snecma_M88\" target=\"_blank\" rel=\"noreferrer noopener\">Snecma M88<\/a>) are usually basic two-spool.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u4e0a\u9762\u8ba8\u8bba\u7684\u5927\u591a\u6570\u914d\u7f6e\u90fd\u7528\u4e8e\u6c11\u7528\u6da1\u8f6e\u98ce\u6247\uff0c\u800c\u73b0\u4ee3\u519b\u7528\u6da1\u8f6e\u98ce\u6247(\u4f8b\u5982\uff0c\u65af\u5948\u514b\u739bM88)\u901a\u5e38\u662f\u57fa\u672c\u7684\u4e24\u8f74\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_20\">4.8 \u9ad8\u538b\u6da1\u8f6e | High-pressure turbine<\/h3>\n\n\n\n<p>Most civil turbofans use a high-efficiency, 2-stage HP turbine to drive the HP compressor. The <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/CFM_International_CFM56\" target=\"_blank\" rel=\"noreferrer noopener\">CFM International CFM56<\/a> uses an alternative approach: a single-stage, high-work unit. While this approach is probably less efficient, there are savings on cooling air, weight and cost.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5927\u591a\u6570\u6c11\u7528\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\u91c7\u7528\u9ad8\u6548\u7387\u7684\u4e24\u7ea7\u9ad8\u538b\u6da1\u8f6e\u6765\u9a71\u52a8\u9ad8\u538b\u538b\u6c14\u673a\u3002CFM\u56fd\u9645CFM56\u91c7\u7528\u4e86\u53e6\u4e00\u79cd\u65b9\u6cd5\uff1a\u5355\u7ea7\u9ad8\u529f\u7387\u5355\u5143\u3002\u867d\u7136\u8fd9\u79cd\u65b9\u6cd5\u53ef\u80fd\u6548\u7387\u8f83\u4f4e\uff0c\u4f46\u5728\u51b7\u5374\u7a7a\u6c14\u3001\u91cd\u91cf\u548c\u6210\u672c\u65b9\u9762\u8282\u7701\u4e86\u4e00\u4e9b\u5f00\u9500\u3002<\/p>\n\n\n\n<p>In the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_RB211\" target=\"_blank\" rel=\"noreferrer noopener\">RB211<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_Trent\" target=\"_blank\" rel=\"noreferrer noopener\">Trent<\/a> 3-spool engine series, the HP compressor pressure ratio is modest so only a single HP turbine stage is required. Modern military turbofans also tend to use a single HP turbine stage and a modest HP compressor.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5728RB211\u548cTrent\u4e09\u8f74\u53d1\u52a8\u673a\u7cfb\u5217\u4e2d\uff0c\u9ad8\u538b\u538b\u6c14\u673a\u538b\u6bd4\u8f83\u4f4e\uff0c\u56e0\u6b64\u53ea\u9700\u8981\u4e00\u4e2a\u9ad8\u538b\u6da1\u8f6e\u7ea7\u3002\u73b0\u4ee3\u519b\u7528\u6da1\u6247\u53d1\u52a8\u673a\u4e5f\u503e\u5411\u4e8e\u4f7f\u7528\u5355\u7ea7\u9ad8\u538b\u6da1\u8f6e\u7ea7\u548c\u8f83\u4f4e\u538b\u6bd4\u7684\u9ad8\u538b\u538b\u6c14\u673a\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_21\">4.9 \u4f4e\u538b\u6da1\u8f6e | Low-pressure turbine<\/h3>\n\n\n\n<p>Modern civil turbofans have multi-stage LP turbines (anywhere from 3 to 7). The number of stages required depends on the engine cycle bypass ratio and the boost (on boosted two-spools). A geared fan may reduce the number of required LPT stages in some applications.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-%3A0-48\" target=\"_blank\" rel=\"noreferrer noopener\">[48]<\/a> Because of the much lower bypass ratios employed, military turbofans require only one or two LP turbine stages.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u73b0\u4ee3\u6c11\u7528\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\u901a\u5e38\u5177\u6709\u591a\u7ea7\u4f4e\u538b\u6da1\u8f6e\uff08\u4ece3\u7ea7\u52307\u7ea7\u4e0d\u7b49\uff09\u3002\u6240\u9700\u7ea7\u6570\u53d6\u51b3\u4e8e\u53d1\u52a8\u673a\u5faa\u73af\u7684\u526f\u63a8\u529b\u6bd4\u548c\u589e\u538b\uff08\u5bf9\u4e8e\u589e\u538b\u7684\u53cc\u8f74\u53d1\u52a8\u673a\uff09\u3002\u5728\u67d0\u4e9b\u5e94\u7528\u4e2d\uff0c\u4f7f\u7528\u9f7f\u8f6e\u98ce\u6247\u53ef\u80fd\u4f1a\u51cf\u5c11\u6240\u9700\u7684\u4f4e\u538b\u6da1\u8f6e\u7ea7\u6570\u3002\u7531\u4e8e\u91c7\u7528\u7684\u526f\u63a8\u529b\u6bd4\u8f83\u4f4e\uff0c\u519b\u7528\u6da1\u6247\u53d1\u52a8\u673a\u53ea\u9700\u89811~2\u7ea7\u4f4e\u538b\u6da1\u8f6e\u3002<\/p>\n\n\n\n<h2 class=\"wp-block-heading\" id=\"h_659034614_22\">5. \u6574\u4f53\u6027\u80fd Overall performance<\/h2>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_23\">5.1 \u5faa\u73af\u6539\u8fdb | Cycle improvements<\/h3>\n\n\n\n<p>Consider a mixed turbofan with a fixed bypass ratio and airflow. Increasing the overall pressure ratio of the compression system raises the combustor entry temperature. Therefore, at a fixed fuel flow there is an increase in (HP) turbine rotor inlet temperature. Although the higher temperature rise across the compression system implies a larger temperature drop over the turbine system, the mixed nozzle temperature is unaffected, because the same amount of heat is being added to the system. There is, however, a rise in nozzle pressure, because overall pressure ratio increases faster than the turbine expansion ratio, causing an increase in the hot mixer entry pressure. Consequently, net thrust increases, whilst specific fuel consumption (fuel flow\/net thrust) decreases. A similar trend occurs with unmixed turbofans.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u8003\u8651\u4e00\u4e2a\u5177\u6709\u56fa\u5b9a\u526f\u63a8\u529b\u6bd4\u548c\u7a7a\u6c14\u6d41\u91cf\u7684\u6df7\u5408\u6da1\u6247\u53d1\u52a8\u673a\u3002\u589e\u52a0\u538b\u7f29\u7cfb\u7edf\u7684\u603b\u538b\u6bd4\u4f1a\u63d0\u9ad8\u71c3\u70e7\u5ba4\u8fdb\u53e3\u6e29\u5ea6\u3002\u56e0\u6b64\uff0c\u5728\u56fa\u5b9a\u71c3\u6599\u6d41\u91cf\u7684\u60c5\u51b5\u4e0b\uff0c(HP)\u6da1\u8f6e\u8f6c\u5b50\u8fdb\u53e3\u6e29\u5ea6\u4f1a\u589e\u52a0\u3002\u5c3d\u7ba1\u538b\u7f29\u7cfb\u7edf\u6e29\u5ea6\u5347\u9ad8\u610f\u5473\u7740\u6da1\u8f6e\u7cfb\u7edf\u6e29\u5ea6\u964d\u4f4e\u66f4\u5927\uff0c\u4f46\u6df7\u5408\u55b7\u7ba1\u6e29\u5ea6\u4e0d\u53d7\u5f71\u54cd\uff0c\u56e0\u4e3a\u7cfb\u7edf\u4e2d\u6dfb\u52a0\u7684\u70ed\u91cf\u76f8\u540c\u3002\u7136\u800c\uff0c\u55b7\u5634\u538b\u529b\u4e0a\u5347\uff0c\u56e0\u4e3a\u6574\u4f53\u538b\u529b\u6bd4\u589e\u52a0\u5f97\u6bd4\u6da1\u8f6e\u81a8\u80c0\u6bd4\u5feb\uff0c\u5bfc\u81f4\u70ed\u6df7\u5408\u5668\u8fdb\u53e3\u538b\u529b\u589e\u52a0\u3002\u56e0\u6b64\uff0c\u51c0\u63a8\u529b\u589e\u52a0\uff0c\u800c\u6bd4\u6cb9\u8017\uff08\u71c3\u6599\u6d41\u91cf\/\u51c0\u63a8\u529b\uff09\u51cf\u5c11\u3002\u975e\u6df7\u5408\u6da1\u6247\u53d1\u52a8\u673a\u4e5f\u6709\u7c7b\u4f3c\u7684\u8d8b\u52bf\u3002<\/p>\n\n\n\n<p>Turbofan engines can be made more fuel efficient by raising overall pressure ratio and turbine rotor inlet temperature in unison. However, better turbine materials or improved vane\/blade cooling are required to cope with increases in both turbine rotor inlet temperature and compressor delivery temperature. Increasing the latter may require better compressor materials.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u901a\u8fc7\u540c\u65f6\u63d0\u9ad8\u603b\u538b\u6bd4\u548c\u6da1\u8f6e\u8f6c\u5b50\u8fdb\u53e3\u6e29\u5ea6\uff0c\u6da1\u6247\u53d1\u52a8\u673a\u53ef\u4ee5\u5b9e\u73b0\u66f4\u9ad8\u7684\u71c3\u6cb9\u6548\u7387\u3002\u7136\u800c\uff0c\u4e3a\u4e86\u5e94\u5bf9\u6da1\u8f6e\u8f6c\u5b50\u8fdb\u53e3\u6e29\u5ea6\u548c\u538b\u7f29\u673a\u51fa\u53e3\u6e29\u5ea6\u7684\u589e\u52a0\uff0c\u9700\u8981\u66f4\u597d\u7684\u6da1\u8f6e\u6750\u6599\u6216\u6539\u8fdb\u7684\u5bfc\u53f6\/\u53f6\u7247\u51b7\u5374\u6280\u672f\u3002\u589e\u52a0\u540e\u8005\u53ef\u80fd\u9700\u8981\u66f4\u597d\u7684\u538b\u7f29\u673a\u6750\u6599\u3002<\/p>\n\n\n\n<p>The overall pressure ratio can be increased by improving fan (or) LP compressor pressure ratio or HP compressor pressure ratio. If the latter is held constant, the increase in (HP) compressor delivery temperature (from raising overall pressure ratio) implies an increase in HP mechanical speed. However, stressing considerations might limit this parameter, implying, despite an increase in overall pressure ratio, a reduction in HP compressor pressure ratio.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u603b\u538b\u6bd4\u53ef\u4ee5\u901a\u8fc7\u6539\u5584\u98ce\u6247\u6216\u4f4e\u538b\u538b\u7f29\u673a\u538b\u529b\u6bd4\u6216\u9ad8\u538b\u538b\u7f29\u673a\u538b\u529b\u6bd4\u6765\u63d0\u9ad8\u3002\u5982\u679c\u5c06\u9ad8\u538b\u538b\u7f29\u673a\u538b\u529b\u6bd4\u4fdd\u6301\u4e0d\u53d8\uff0c\u5219\u7531\u4e8e\u63d0\u9ad8\u603b\u538b\u6bd4\u800c\u5bfc\u81f4\u7684(HP)\u538b\u7f29\u673a\u51fa\u53e3\u6e29\u5ea6\u589e\u52a0\u610f\u5473\u7740(HP)\u673a\u68b0\u901f\u5ea6\u589e\u52a0\u3002\u7136\u800c\uff0c\u5e94\u8003\u8651\u5230\u5e94\u529b\u7684\u9650\u5236\u53ef\u80fd\u9650\u5236\u6b64\u53c2\u6570\uff0c\u8fd9\u610f\u5473\u7740\u5c3d\u7ba1\u603b\u538b\u6bd4\u589e\u52a0\uff0c\u4f46\u9ad8\u538b\u538b\u7f29\u673a\u538b\u529b\u6bd4\u51cf\u5c0f\u3002<\/p>\n\n\n\n<p>According to simple theory, if the ratio of turbine rotor inlet temperature\/(HP) compressor delivery temperature is maintained, the HP turbine throat area can be retained. However, this assumes that cycle improvements are obtained, while retaining the datum (HP) compressor exit flow function (non-dimensional flow). In practice, changes to the non-dimensional speed of the (HP) compressor and cooling bleed extraction would probably make this assumption invalid, making some adjustment to HP turbine throat area unavoidable. This means the HP turbine nozzle guide vanes would have to be different from the original. In all probability, the downstream LP turbine nozzle guide vanes would have to be changed anyway.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6839\u636e\u7b80\u5355\u7406\u8bba\uff0c\u5982\u679c\u4fdd\u6301\u6da1\u8f6e\u8f6c\u5b50\u8fdb\u53e3\u6e29\u5ea6\u4e0e(HP)\u538b\u7f29\u673a\u51fa\u53e3\u6e29\u5ea6\u7684\u6bd4\u503c\u4e0d\u53d8\uff0c\u5219\u53ef\u4ee5\u4fdd\u6301(HP)\u6da1\u8f6e\u5589\u90e8\u7684\u9762\u79ef\u3002\u7136\u800c\uff0c\u8fd9\u5047\u8bbe\u5728\u4fdd\u6301\u6570\u636e(HP)\u538b\u7f29\u673a\u51fa\u53e3\u6d41\u51fd\u6570\uff08\u65e0\u91cf\u7eb2\u6d41\u91cf\uff09\u7684\u540c\u65f6\uff0c\u53ef\u4ee5\u83b7\u5f97\u5faa\u73af\u6539\u8fdb\u3002\u5b9e\u9645\u4e0a\uff0c(HP)\u538b\u7f29\u673a\u7684\u65e0\u91cf\u7eb2\u901f\u5ea6\u548c\u51b7\u5374\u62bd\u53d6\u53ef\u80fd\u4f1a\u4f7f\u5f97\u8fd9\u4e2a\u5047\u8bbe\u65e0\u6548\uff0c\u4ece\u800c\u4e0d\u53ef\u907f\u514d\u5730\u5bf9(HP)\u6da1\u8f6e\u5589\u90e8\u9762\u79ef\u8fdb\u884c\u4e00\u4e9b\u8c03\u6574\u3002\u8fd9\u610f\u5473\u7740(HP)\u6da1\u8f6e\u5bfc\u53f6\u5fc5\u987b\u4e0e\u6700\u521d\u7684\u8bbe\u8ba1\u4e0d\u540c\u3002\u5f88\u53ef\u80fd\uff0c\u4e0b\u6e38\u7684\u4f4e\u538b\u6da1\u8f6e\u5bfc\u53f6\u4e5f\u5fc5\u987b\u8fdb\u884c\u6539\u53d8\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_24\">5.2 \u63a8\u529b\u589e\u957f | Thrust growth<\/h3>\n\n\n\n<p>Thrust growth is obtained by increasing <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/w\/index.php%3Ftitle%3DCore_power%26action%3Dedit%26redlink%3D1\" target=\"_blank\" rel=\"noreferrer noopener\">core power<\/a>. There are two basic routes available:<br>\u53c2\u8003\u8bd1\u6587\uff1a\u63a8\u529b\u589e\u957f\u662f\u901a\u8fc7\u589e\u52a0\u6838\u5fc3\u529f\u7387\u6765\u5b9e\u73b0\u7684\u3002\u6709\u4e24\u6761\u57fa\u672c\u8def\u7ebf\u53ef\u4f9b\u9009\u62e9:<\/p>\n\n\n\n<ol class=\"wp-block-list\">\n<li>hot route: increase HP turbine rotor inlet temperature<br>\u53c2\u8003\u8bd1\u6587\uff1a\u70ed\u8def\u7ebf:\u63d0\u9ad8\u9ad8\u538b\u6da1\u8f6e\u8f6c\u5b50\u5165\u53e3\u6e29\u5ea6<\/li>\n\n\n\n<li>cold route: increase core mass flow<br>\u53c2\u8003\u8bd1\u6587\uff1a\u51b7\u8def\u7ebf:\u589e\u52a0\u5806\u82af\u8d28\u91cf\u6d41\u91cf<\/li>\n<\/ol>\n\n\n\n<p>Both routes require an increase in the combustor fuel flow and, therefore, the heat energy added to the core stream.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u8fd9\u4e24\u79cd\u9014\u5f84\u90fd\u9700\u8981\u589e\u52a0\u71c3\u70e7\u5ba4\u7684\u71c3\u6599\u6d41\u91cf\uff0c\u56e0\u6b64\uff0c\u70ed\u91cf\u589e\u52a0\u5230\u6838\u5fc3\u6d41\u3002<\/p>\n\n\n\n<p>The hot route may require changes in turbine blade\/vane materials or better blade\/vane cooling. The cold route can be obtained by one of the following:<br>\u53c2\u8003\u8bd1\u6587\uff1a\u70ed\u8def\u7ebf\u53ef\u80fd\u9700\u8981\u6539\u53d8\u6da1\u8f6e\u53f6\u7247\/\u53f6\u7247\u6750\u6599\u6216\u66f4\u597d\u7684\u53f6\u7247\/\u53f6\u7247\u51b7\u5374\u3002\u51b7\u8def\u7531\u53ef\u4ee5\u901a\u8fc7\u4ee5\u4e0b\u65b9\u5f0f\u83b7\u53d6:<\/p>\n\n\n\n<ol class=\"wp-block-list\">\n<li>adding booster stages to the LP\/IP compression<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5c06\u52a9\u63a8\u5668\u7ea7\u6dfb\u52a0\u5230LP\/IP\u538b\u7f29\u4e2d<\/li>\n\n\n\n<li>adding a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Zero-stage\" target=\"_blank\" rel=\"noreferrer noopener\">zero-stage<\/a> to the HP compression<br>\u53c2\u8003\u8bd1\u6587\uff1a\u4e3aHP\u538b\u7f29\u6dfb\u52a0\u96f6\u7ea7<\/li>\n\n\n\n<li>improving the compression process, without adding stages (e.g. higher fan hub pressure ratio)<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6539\u8fdb\u538b\u7f29\u8fc7\u7a0b\uff0c\u65e0\u9700\u589e\u52a0\u7ea7(\u5982\u63d0\u9ad8\u98ce\u673a\u8f6e\u6bc2\u538b\u529b\u6bd4)<\/li>\n<\/ol>\n\n\n\n<p>all of which increase both overall pressure ratio and core airflow.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6240\u6709\u8fd9\u4e9b\u90fd\u589e\u52a0\u4e86\u603b\u538b\u6bd4\u548c\u6838\u5fc3\u6c14\u6d41\u3002<\/p>\n\n\n\n<p>Alternatively, the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/w\/index.php%3Ftitle%3DCore_size%26action%3Dedit%26redlink%3D1\" target=\"_blank\" rel=\"noreferrer noopener\">core size<\/a> can be increased, to raise core airflow, without changing overall pressure ratio. This route is expensive, since a new (upflowed) turbine system (and possibly a larger IP compressor) is also required.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6216\uff0c\u53ef\u4ee5\u589e\u52a0\u6838\u5fc3\u5c3a\u5bf8\uff0c\u4ee5\u63d0\u9ad8\u6838\u5fc3\u6c14\u6d41\uff0c\u800c\u4e0d\u6539\u53d8\u603b\u538b\u6bd4\u3002\u8fd9\u6761\u8def\u5f84\u662f\u6602\u8d35\u7684\uff0c\u56e0\u4e3a\u8fd8\u9700\u8981\u4e00\u4e2a\u65b0\u7684\uff08\u4e0a\u5347\u5f0f\uff09\u6da1\u8f6e\u7cfb\u7edf\uff08\u53ef\u80fd\u8fd8\u9700\u8981\u4e00\u4e2a\u66f4\u5927\u7684\u4e2d\u538b\u538b\u7f29\u673a\uff09\u3002<\/p>\n\n\n\n<p>Changes must also be made to the fan to absorb the extra core power. On a civil engine, jet noise considerations mean that any significant increase in take-off thrust must be accompanied by a corresponding increase in fan mass flow (to maintain a T\/O specific thrust of about 30 lbf\/lb\/s).<br>\u53c2\u8003\u8bd1\u6587\uff1a\u8fd8\u5fc5\u987b\u5bf9\u98ce\u6247\u8fdb\u884c\u6539\u53d8\uff0c\u4ee5\u5438\u6536\u989d\u5916\u7684\u6838\u5fc3\u529f\u7387\u3002\u5728\u6c11\u7528\u53d1\u52a8\u673a\u4e0a\uff0c\u5c04\u6d41\u566a\u58f0\u8003\u8651\u56e0\u7d20\u610f\u5473\u7740\u4efb\u4f55\u663e\u8457\u589e\u52a0\u7684\u8d77\u98de\u63a8\u529b\u90fd\u5fc5\u987b\u4f34\u968f\u7740\u98ce\u6247\u8d28\u91cf\u6d41\u91cf\u7684\u76f8\u5e94\u589e\u52a0\uff08\u4ee5\u4fdd\u6301\u7ea6\u4e3a30\u78c5\/\u78c5\/\u79d2\u7684\u8d77\u98de\u6bd4\u63a8\u529b\uff09\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_25\">5.3 \u6280\u672f\u8ba8\u8bba | Technical discussion<\/h3>\n\n\n\n<p>1. Specific thrust (net thrust\/intake airflow) is an important parameter for turbofans and jet engines in general. Imagine a fan (driven by an appropriately sized electric motor) operating within a pipe, which is connected to a propelling nozzle. It is fairly obvious, the higher the fan pressure ratio (fan discharge pressure\/fan inlet pressure), the higher the jet velocity and the corresponding specific thrust. Now imagine we replace this set-up with an equivalent turbofan \u2013 same airflow and same fan pressure ratio. Obviously, the core of the turbofan must produce sufficient power to drive the fan via the low-pressure (LP) turbine. If we choose a low (HP) turbine inlet temperature for the gas generator, the core airflow needs to be relatively high to compensate. The corresponding bypass ratio is therefore relatively low. If we raise the turbine inlet temperature, the core airflow can be smaller, thus increasing bypass ratio. Raising turbine inlet temperature tends to increase thermal efficiency and, therefore, improve <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Fuel_efficiency\" target=\"_blank\" rel=\"noreferrer noopener\">fuel efficiency<\/a>.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5bf9\u4e8e\u6da1\u6247\u53d1\u52a8\u673a\u548c\u55b7\u6c14\u53d1\u52a8\u673a\u6765\u8bf4\uff0c\u6bd4\u63a8\u529b\uff08\u51c0\u63a8\u529b\/\u8fdb\u6c14\u6c14\u6d41\uff09\u662f\u4e00\u4e2a\u91cd\u8981\u7684\u53c2\u6570\u3002\u60f3\u8c61\u4e00\u4e2a\u7531\u9002\u5f53\u5c3a\u5bf8\u7684\u7535\u52a8\u673a\u9a71\u52a8\u7684\u98ce\u6247\uff0c\u5728\u4e0e\u4e00\u4e2a\u63a8\u8fdb\u55b7\u5634\u8fde\u63a5\u7684\u7ba1\u9053\u5185\u8fd0\u884c\u3002\u5f88\u660e\u663e\uff0c\u98ce\u6247\u538b\u6bd4\uff08\u98ce\u6247\u6392\u6c14\u538b\u529b\/\u98ce\u6247\u8fdb\u6c14\u538b\u529b\uff09\u8d8a\u9ad8\uff0c\u55b7\u6c14\u901f\u5ea6\u8d8a\u9ad8\uff0c\u76f8\u5e94\u7684\u6bd4\u63a8\u529b\u4e5f\u8d8a\u9ad8\u3002\u73b0\u5728\u60f3\u8c61\u6211\u4eec\u7528\u4e00\u4e2a\u7b49\u6548\u7684\u6da1\u6247\u4ee3\u66ff\u8fd9\u4e2a\u8bbe\u5907\u2014\u2014\u76f8\u540c\u7684\u6c14\u6d41\u548c\u76f8\u540c\u7684\u98ce\u6247\u538b\u6bd4\u3002\u663e\u7136\uff0c\u6da1\u6247\u7684\u6838\u5fc3\u5fc5\u987b\u901a\u8fc7\u4f4e\u538b\uff08LP\uff09\u6da1\u8f6e\u4ea7\u751f\u8db3\u591f\u7684\u529f\u7387\u6765\u9a71\u52a8\u98ce\u6247\u3002\u5982\u679c\u6211\u4eec\u9009\u62e9\u4e00\u4e2a\u8f83\u4f4e\u7684\uff08HP\uff09\u6da1\u8f6e\u8fdb\u53e3\u6e29\u5ea6\u4f5c\u4e3a\u6c14\u4f53\u53d1\u751f\u5668\uff0c\u6838\u5fc3\u6c14\u6d41\u9700\u8981\u76f8\u5bf9\u8f83\u9ad8\u6765\u8fdb\u884c\u8865\u507f\u3002\u56e0\u6b64\uff0c\u76f8\u5e94\u7684\u65c1\u8def\u6bd4\u76f8\u5bf9\u8f83\u4f4e\u3002\u5982\u679c\u6211\u4eec\u63d0\u9ad8\u6da1\u8f6e\u8fdb\u53e3\u6e29\u5ea6\uff0c\u6838\u5fc3\u6c14\u6d41\u53ef\u4ee5\u66f4\u5c0f\uff0c\u4ece\u800c\u589e\u52a0\u65c1\u8def\u6bd4\u3002\u63d0\u9ad8\u6da1\u8f6e\u8fdb\u53e3\u6e29\u5ea6\u5f80\u5f80\u4f1a\u589e\u52a0\u70ed\u6548\u7387\uff0c\u56e0\u6b64\u63d0\u9ad8\u71c3\u6cb9\u6548\u3002<\/p>\n\n\n\n<p>2. Naturally, as altitude increases, there is a decrease in air density and, therefore, the net thrust of an engine. There is also a flight speed effect, termed thrust lapse rate. Consider the approximate equation for net thrust again:<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5f53\u6d77\u62d4\u589e\u52a0\u65f6\uff0c\u7a7a\u6c14\u5bc6\u5ea6\u51cf\u5c0f\uff0c\u56e0\u6b64\u53d1\u52a8\u673a\u7684\u51c0\u63a8\u529b\u4e5f\u4f1a\u51cf\u5c0f\u3002\u8fd8\u6709\u4e00\u79cd\u98de\u884c\u901f\u5ea6\u6548\u5e94\uff0c\u88ab\u79f0\u4e3a\u63a8\u529b\u8870\u51cf\u7387\u3002\u518d\u8003\u8651\u51c0\u63a8\u529b\u7684\u8fd1\u4f3c\u65b9\u7a0b\uff1a<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/pic1.zhimg.com\/80\/v2-41eb82fff9a4befb0ffb0bff602654c8_720w.webp\" alt=\"\"\/><\/figure>\n\n\n\n<p>With a high specific thrust (e.g., fighter) engine, the jet velocity is relatively high, so intuitively one can see that increases in flight velocity have less of an impact upon net thrust than a medium specific thrust (e.g., trainer) engine, where the jet velocity is lower. The impact of thrust lapse rate upon a low specific thrust (e.g., civil) engine is even more severe. At high flight speeds, high-specific-thrust engines can pick up net thrust through the ram rise in the intake, but this effect tends to diminish at supersonic speeds because of shock wave losses.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5bf9\u4e8e\u9ad8\u6bd4\u63a8\u529b\uff08\u4f8b\u5982\u6218\u6597\u673a\uff09\u53d1\u52a8\u673a\uff0c\u55b7\u6c14\u901f\u5ea6\u76f8\u5bf9\u8f83\u9ad8\uff0c\u56e0\u6b64\u76f4\u89c2\u4e0a\u53ef\u4ee5\u770b\u51fa\uff0c\u98de\u884c\u901f\u5ea6\u7684\u589e\u52a0\u5bf9\u51c0\u63a8\u529b\u7684\u5f71\u54cd\u8f83\u5c0f\uff0c\u800c\u5bf9\u4e8e\u4e2d\u7b49\u6bd4\u63a8\u529b\uff08\u4f8b\u5982\u6559\u7ec3\u673a\uff09\u53d1\u52a8\u673a\u6765\u8bf4\uff0c\u55b7\u6c14\u901f\u5ea6\u8f83\u4f4e\uff0c\u5bf9\u51c0\u63a8\u529b\u7684\u5f71\u54cd\u8f83\u5927\u3002\u5bf9\u4e8e\u4f4e\u6bd4\u63a8\u529b\uff08\u4f8b\u5982\u6c11\u7528\uff09\u53d1\u52a8\u673a\u6765\u8bf4\uff0c\u63a8\u529b\u8870\u51cf\u7387\u7684\u5f71\u54cd\u66f4\u52a0\u4e25\u91cd\u3002\u5728\u9ad8\u901f\u98de\u884c\u65f6\uff0c\u9ad8\u6bd4\u63a8\u529b\u53d1\u52a8\u673a\u53ef\u4ee5\u901a\u8fc7\u8fdb\u6c14\u9053\u7684\u6c14\u6d41\u4e0a\u5347\u6765\u589e\u52a0\u51c0\u63a8\u529b\uff0c\u4f46\u5728\u8d85\u97f3\u901f\u901f\u5ea6\u4e0b\uff0c\u7531\u4e8e\u6fc0\u6ce2\u635f\u5931\uff0c\u8fd9\u79cd\u6548\u5e94\u4f1a\u51cf\u5f31\u3002<\/p>\n\n\n\n<p>3. Thrust growth on civil turbofans is usually obtained by increasing fan airflow, thus preventing the jet noise becoming too high. However, the larger fan airflow requires more power from the core. This can be achieved by raising the overall pressure ratio (combustor inlet pressure\/intake delivery pressure) to induce more airflow into the core and by increasing turbine inlet temperature. Together, these parameters tend to increase core thermal efficiency and improve fuel efficiency.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6c11\u7528\u6da1\u6247\u53d1\u52a8\u673a\u901a\u5e38\u901a\u8fc7\u589e\u52a0\u98ce\u6247\u6c14\u6d41\u6765\u5b9e\u73b0\u63a8\u529b\u589e\u957f\uff0c\u4ece\u800c\u9632\u6b62\u55b7\u6c14\u566a\u58f0\u8fc7\u9ad8\u3002\u7136\u800c\uff0c\u66f4\u5927\u7684\u98ce\u6247\u6c14\u6d41\u9700\u8981\u66f4\u591a\u6838\u5fc3\u90e8\u5206\u7684\u52a8\u529b\u3002\u8fd9\u53ef\u4ee5\u901a\u8fc7\u63d0\u9ad8\u603b\u538b\u6bd4\uff08\u71c3\u70e7\u5668\u8fdb\u53e3\u538b\u529b\/\u8fdb\u6c14\u9053\u8fdb\u53e3\u538b\u529b\uff09\u6765\u5b9e\u73b0\uff0c\u4ee5\u4fc3\u4f7f\u66f4\u591a\u6c14\u6d41\u8fdb\u5165\u6838\u5fc3\uff0c\u5e76\u589e\u52a0\u6da1\u8f6e\u8fdb\u53e3\u6e29\u5ea6\u3002\u8fd9\u4e9b\u53c2\u6570\u5171\u540c\u589e\u52a0\u4e86\u6838\u5fc3\u70ed\u6548\u7387\uff0c\u5e76\u63d0\u9ad8\u4e86\u71c3\u6cb9\u6548\u7387\u3002<\/p>\n\n\n\n<p>4. Some high-bypass-ratio civil turbofans use an extremely low area ratio (less than 1.01), convergent-divergent, nozzle on the bypass (or mixed exhaust) stream, to control the fan working line. The nozzle acts as if it has variable geometry. At low flight speeds the nozzle is unchoked (less than a Mach number of unity), so the exhaust gas speeds up as it approaches the throat and then slows down slightly as it reaches the divergent section. Consequently, the nozzle exit area controls the fan match and, being larger than the throat, pulls the fan working line slightly away from surge. At higher flight speeds, the ram rise in the intake increases nozzle pressure ratio to the point where the throat becomes choked (M=1.0). Under these circumstances, the throat area dictates the fan match and, being smaller than the exit, pushes the fan working line slightly towards surge. This is not a problem, since fan surge margin is much better at high flight speeds.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u4e00\u4e9b\u9ad8\u6db5\u9053\u6bd4\u7684\u6c11\u7528\u6da1\u6247\u53d1\u52a8\u673a\u5728\u65c1\u901a\uff08\u6216\u6df7\u5408\u6392\u6c14\uff09\u6d41\u4e0a\u4f7f\u7528\u4e86\u4e00\u4e2a\u6781\u4f4e\u7684\u9762\u79ef\u6bd4\uff08\u5c0f\u4e8e1.01\uff09\u7684\u6536\u655b-\u6269\u5f20\u55b7\u5634\uff0c\u4ee5\u63a7\u5236\u98ce\u6247\u7684\u5de5\u4f5c\u7ebf\u3002\u8fd9\u4e2a\u55b7\u5634\u7684\u4f5c\u7528\u5c31\u50cf\u662f\u5177\u6709\u53ef\u53d8\u51e0\u4f55\u5f62\u72b6\u4e00\u6837\u3002\u5728\u4f4e\u98de\u884c\u901f\u5ea6\u4e0b\uff0c\u55b7\u5634\u5904\u4e8e\u975e\u7a92\u606f\u72b6\u6001\uff08\u9a6c\u8d6b\u6570\u5c0f\u4e8e1\uff09\uff0c\u56e0\u6b64\u6392\u6c14\u6c14\u4f53\u5728\u63a5\u8fd1\u5589\u90e8\u65f6\u52a0\u901f\uff0c\u7136\u540e\u5728\u8fbe\u5230\u6269\u5f20\u6bb5\u65f6\u7565\u5fae\u51cf\u901f\u3002\u56e0\u6b64\uff0c\u55b7\u5634\u51fa\u53e3\u9762\u79ef\u63a7\u5236\u4e86\u98ce\u6247\u7684\u5339\u914d\uff0c\u7531\u4e8e\u6bd4\u5589\u90e8\u5927\uff0c\u4f7f\u5f97\u98ce\u6247\u5de5\u4f5c\u7ebf\u7565\u5fae\u8fdc\u79bb\u6fc0\u6da1\u3002\u5728\u66f4\u9ad8\u7684\u98de\u884c\u901f\u5ea6\u4e0b\uff0c\u8fdb\u6c14\u9053\u7684\u6c14\u6d41\u4e0a\u5347\u589e\u52a0\u4e86\u55b7\u5634\u7684\u538b\u529b\u6bd4\uff0c\u4f7f\u5f97\u5589\u90e8\u88ab\u7a92\u606f\uff08M=1.0\uff09\u3002\u5728\u8fd9\u79cd\u60c5\u51b5\u4e0b\uff0c\u5589\u90e8\u9762\u79ef\u51b3\u5b9a\u4e86\u98ce\u6247\u7684\u5339\u914d\uff0c\u7531\u4e8e\u6bd4\u51fa\u53e3\u5c0f\uff0c\u4f7f\u5f97\u98ce\u6247\u5de5\u4f5c\u7ebf\u7565\u5fae\u9760\u8fd1\u6fc0\u6da1\u3002\u8fd9\u5e76\u4e0d\u662f\u4e00\u4e2a\u95ee\u9898\uff0c\u56e0\u4e3a\u5728\u9ad8\u98de\u884c\u901f\u5ea6\u4e0b\uff0c\u98ce\u6247\u7684\u6fc0\u6da1\u4f59\u91cf\u8981\u597d\u5f97\u591a\u3002<\/p>\n\n\n\n<p>5. The off-design behaviour of turbofans is illustrated under <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Compressor_map\" target=\"_blank\" rel=\"noreferrer noopener\">compressor map<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbine_map\" target=\"_blank\" rel=\"noreferrer noopener\">turbine map<\/a>.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5728\u538b\u6c14\u673a\u56fe\u548c\u6da1\u8f6e\u56fe\u4e24\u79cd\u60c5\u51b5\u4e0b\u9610\u8ff0\u4e86\u6da1\u6247\u7684\u975e\u8bbe\u8ba1\u7279\u6027\u3002<\/p>\n\n\n\n<p>6. Because modern civil turbofans operate at low specific thrust, they require only a single fan stage to develop the required fan pressure ratio. The desired overall pressure ratio for the engine cycle is usually achieved by multiple axial stages on the core compression. Rolls-Royce tend to split the core compression into two with an intermediate pressure (IP) supercharging the HP compressor, both units being driven by turbines with a single stage, mounted on separate shafts. Consequently, the HP compressor need develop only a modest pressure ratio (e.g., ~4.5:1). US civil engines use much higher HP compressor pressure ratios (e.g., ~23:1 on the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_GE90\" target=\"_blank\" rel=\"noreferrer noopener\">General Electric GE90<\/a>) and tend to be driven by a two-stage HP turbine. Even so, there are usually a few IP axial stages mounted on the LP shaft, behind the fan, to further supercharge the core compression system. Civil engines have multi-stage LP turbines, the number of stages being determined by the bypass ratio, the amount of IP compression on the LP shaft and the LP turbine blade speed.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u7531\u4e8e\u73b0\u4ee3\u6c11\u7528\u6da1\u6247\u53d1\u52a8\u673a\u7684\u6bd4\u63a8\u529b\u8f83\u4f4e\uff0c\u6240\u4ee5\u53ea\u9700\u8981\u4e00\u4e2a\u98ce\u6247\u7ea7\u6765\u8fbe\u5230\u6240\u9700\u7684\u98ce\u6247\u538b\u529b\u6bd4\u3002\u901a\u5e38\uff0c\u53d1\u52a8\u673a\u5faa\u73af\u7684\u671f\u671b\u603b\u538b\u6bd4\u662f\u901a\u8fc7\u6838\u5fc3\u538b\u7f29\u4e2d\u7684\u591a\u4e2a\u8f74\u5411\u7ea7\u6765\u5b9e\u73b0\u7684\u3002\u52b3\u65af\u83b1\u65af\u516c\u53f8\u503e\u5411\u4e8e\u5c06\u6838\u5fc3\u538b\u7f29\u5206\u6210\u4e24\u90e8\u5206\uff0c\u4e2d\u95f4\u538b\u529b\uff08IP\uff09\u589e\u538b\u9ad8\u538b\uff08HP\uff09\u538b\u7f29\u673a\uff0c\u8fd9\u4e24\u4e2a\u90e8\u4ef6\u7531\u5355\u7ea7\u6da1\u8f6e\u9a71\u52a8\uff0c\u5b89\u88c5\u5728\u5355\u72ec\u7684\u8f74\u4e0a\u3002\u56e0\u6b64\uff0cHP\u538b\u7f29\u673a\u53ea\u9700\u8fbe\u5230\u9002\u5ea6\u7684\u538b\u529b\u6bd4\uff08\u4f8b\u5982\uff0c\u7ea6\u4e3a4.5:1\uff09\u3002\u7f8e\u56fd\u7684\u6c11\u7528\u53d1\u52a8\u673a\u4f7f\u7528\u66f4\u9ad8\u7684HP\u538b\u7f29\u673a\u538b\u529b\u6bd4\uff08\u4f8b\u5982\uff0c\u901a\u7528\u7535\u6c14GE90\u7684\u538b\u529b\u6bd4\u7ea6\u4e3a23:1\uff09\uff0c\u5e76\u4e14\u503e\u5411\u4e8e\u7531\u4e24\u7ea7HP\u6da1\u8f6e\u9a71\u52a8\u3002\u5373\u4fbf\u5982\u6b64\uff0c\u5728\u98ce\u6247\u540e\u9762\u7684LP\u8f74\u4e0a\u901a\u5e38\u4ecd\u7136\u6709\u4e00\u4e9bIP\u8f74\u5411\u7ea7\uff0c\u8fdb\u4e00\u6b65\u589e\u538b\u6838\u5fc3\u538b\u7f29\u7cfb\u7edf\u3002\u6c11\u7528\u53d1\u52a8\u673a\u5177\u6709\u591a\u7ea7LP\u6da1\u8f6e\uff0c\u7ea7\u6570\u7531\u65c1\u901a\u6bd4\u3001LP\u8f74\u4e0a\u7684IP\u538b\u7f29\u91cf\u548cLP\u6da1\u8f6e\u53f6\u7247\u901f\u5ea6\u6765\u786e\u5b9a\u3002<\/p>\n\n\n\n<p>7. Because military engines usually have to be able to fly very fast at sea level, the limit on HP compressor delivery temperature is reached at a fairly modest design overall pressure ratio, compared with that of a civil engine. Also the fan pressure ratio is relatively high, to achieve a medium to high specific thrust. Consequently, modern military turbofans usually have only 5 or 6 HP compressor stages and require only a single-stage HP turbine. Low-bypass-ratio military turbofans usually have one LP turbine stage, but higher bypass ratio engines need two stages. In theory, by adding IP compressor stages, a modern military turbofan HP compressor could be used in a civil turbofan derivative, but the core would tend to be too small for high thrust applications.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u7531\u4e8e\u519b\u7528\u53d1\u52a8\u673a\u901a\u5e38\u9700\u8981\u5728\u6d77\u5e73\u9762\u4e0a\u4ee5\u975e\u5e38\u9ad8\u7684\u901f\u5ea6\u98de\u884c\uff0c\u4e0e\u6c11\u7528\u53d1\u52a8\u673a\u76f8\u6bd4\uff0cHP\u538b\u7f29\u673a\u4f20\u9012\u6e29\u5ea6\u7684\u9650\u5236\u5728\u76f8\u5bf9\u8f83\u4f4e\u7684\u8bbe\u8ba1\u603b\u538b\u6bd4\u4e0b\u5c31\u4f1a\u8fbe\u5230\u3002\u6b64\u5916\uff0c\u4e3a\u4e86\u5b9e\u73b0\u4e2d\u5230\u9ad8\u7684\u6bd4\u63a8\u529b\uff0c\u98ce\u6247\u538b\u6bd4\u76f8\u5bf9\u8f83\u9ad8\u3002\u56e0\u6b64\uff0c\u73b0\u4ee3\u519b\u7528\u6da1\u6247\u53d1\u52a8\u673a\u901a\u5e38\u53ea\u67095\u62166\u4e2aHP\u538b\u7f29\u673a\u7ea7\u522b\uff0c\u53ea\u9700\u8981\u5355\u7ea7HP\u6da1\u8f6e\u3002\u4f4e\u65c1\u901a\u6bd4\u7684\u519b\u7528\u6da1\u6247\u53d1\u52a8\u673a\u901a\u5e38\u53ea\u6709\u4e00\u4e2aLP\u6da1\u8f6e\u7ea7\u522b\uff0c\u800c\u9ad8\u65c1\u901a\u6bd4\u7684\u53d1\u52a8\u673a\u5219\u9700\u8981\u4e24\u4e2a\u7ea7\u522b\u3002\u7406\u8bba\u4e0a\uff0c\u901a\u8fc7\u589e\u52a0IP\u538b\u7f29\u673a\u7ea7\u6570\uff0c\u73b0\u4ee3\u519b\u7528\u6da1\u6247\u53d1\u52a8\u673a\u7684HP\u538b\u7f29\u673a\u53ef\u4ee5\u7528\u4e8e\u6c11\u7528\u6da1\u6247\u7684\u884d\u751f\u578b\u53f7\uff0c\u4f46\u6838\u5fc3\u5f80\u5f80\u5bf9\u4e8e\u9ad8\u63a8\u529b\u5e94\u7528\u6765\u8bf4\u592a\u5c0f\u3002<\/p>\n\n\n\n<h2 class=\"wp-block-heading\" id=\"h_659034614_26\">6. \u63d0\u5347 | Improvements<\/h2>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_27\">6.1 \u7a7a\u6c14\u52a8\u529b\u5b66\u6a21\u578b | Aerodynamic modelling<\/h3>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Aerodynamics\" target=\"_blank\" rel=\"noreferrer noopener\">Aerodynamics<\/a> is a mix of <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Speed_of_sound\" target=\"_blank\" rel=\"noreferrer noopener\">subsonic<\/a>, <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Transonic\" target=\"_blank\" rel=\"noreferrer noopener\">transonic<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Supersonic\" target=\"_blank\" rel=\"noreferrer noopener\">supersonic<\/a> airflow on a single fan\/<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Gas_compressor\" target=\"_blank\" rel=\"noreferrer noopener\">gas compressor<\/a> blade in a modern turbofan. The airflow past the blades has to be maintained within close angular limits to keep the air flowing against an increasing pressure. Otherwise the air will come back out of the intake.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-LN161021-49\" target=\"_blank\" rel=\"noreferrer noopener\">[49]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u73b0\u4ee3\u6da1\u6247\u53d1\u52a8\u673a\u7684\u6c14\u52a8\u7279\u6027\u662f\u4e9a\u97f3\u901f\u3001\u8de8\u97f3\u901f\u548c\u8d85\u97f3\u901f\u6c14\u6d41\u5728\u5355\u4e2a\u98ce\u6247\/\u6c14\u4f53\u538b\u7f29\u673a\u53f6\u7247\u4e0a\u7684\u6df7\u5408\u3002\u4e3a\u4e86\u4fdd\u6301\u6c14\u6d41\u987a\u7740\u9010\u6e10\u589e\u52a0\u7684\u538b\u529b\u6d41\u52a8\uff0c\u5fc5\u987b\u5728\u63a5\u8fd1\u7684\u89d2\u5ea6\u9650\u5236\u4e0b\u7ef4\u6301\u6c14\u6d41\u901a\u8fc7\u53f6\u7247\u3002\u5426\u5219\uff0c\u6c14\u6d41\u5c06\u4f1a\u4ece\u8fdb\u6c14\u53e3\u9006\u6d41\u51fa\u6765\u3002<\/p>\n\n\n\n<p>The <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/FADEC\" target=\"_blank\" rel=\"noreferrer noopener\">Full Authority Digital Engine Control<\/a> (FADEC) needs accurate data for controlling the engine. The critical <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbine\" target=\"_blank\" rel=\"noreferrer noopener\">turbine<\/a> inlet temperature (TIT) is too harsh an environment, at 1,700 \u00b0C (3,100 \u00b0F) and 17 bar (250 psi), for reliable <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Temperature_sensor\" target=\"_blank\" rel=\"noreferrer noopener\">sensors<\/a>. Therefore, during development of a new engine type a relation is established between a more easily measured temperature like <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Exhaust_gas\" target=\"_blank\" rel=\"noreferrer noopener\">exhaust gas<\/a> temperature and the TIT. Monitoring the exhaust gas temperature is then used to make sure the engine does not run too hot.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-LN161021-49\" target=\"_blank\" rel=\"noreferrer noopener\">[49]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u5168\u6743\u6570\u5b57\u5f0f\u53d1\u52a8\u673a\u63a7\u5236\u7cfb\u7edf\uff08FADEC\uff09\u9700\u8981\u51c6\u786e\u7684\u6570\u636e\u6765\u63a7\u5236\u53d1\u52a8\u673a\u3002\u5173\u952e\u7684\u6da1\u8f6e\u8fdb\u53e3\u6e29\u5ea6\uff08TIT\uff09\u5bf9\u4e8e\u53ef\u9760\u4f20\u611f\u5668\u6765\u8bf4\u662f\u4e00\u4e2a\u8fc7\u4e8e\u6076\u52a3\u7684\u73af\u5883\uff0c\u6e29\u5ea6\u9ad8\u8fbe1,700\u00b0C\uff083,100\u00b0F\uff09\uff0c\u538b\u529b\u8fbe\u523017\u5df4\uff08250\u78c5\/\u5e73\u65b9\u82f1\u5bf8\uff09\u3002\u56e0\u6b64\uff0c\u5728\u5f00\u53d1\u65b0\u578b\u53d1\u52a8\u673a\u65f6\uff0c\u9700\u8981\u5efa\u7acb\u6392\u6c14\u6e29\u5ea6\u7b49\u66f4\u5bb9\u6613\u6d4b\u91cf\u7684\u6e29\u5ea6\u4e0eTIT\u4e4b\u95f4\u7684\u5173\u7cfb\u3002\u76d1\u6d4b\u6392\u6c14\u6e29\u5ea6\u7136\u540e\u7528\u4e8e\u786e\u4fdd\u53d1\u52a8\u673a\u4e0d\u4f1a\u8fc7\u70ed\u8fd0\u884c\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_28\">6.2 \u53f6\u7247\u6280\u672f | Blade technology<\/h3>\n\n\n\n<p>A 100 g (3.5 oz) <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbine\" target=\"_blank\" rel=\"noreferrer noopener\">turbine<\/a> blade is subjected to 1,700 \u00b0C (3,100 \u00b0F), at 17 bar (250 psi) and a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Centrifugal_force\" target=\"_blank\" rel=\"noreferrer noopener\">centrifugal force<\/a> of 40 kN (9,000 lbf), well above the point of <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Plastic_deformation\" target=\"_blank\" rel=\"noreferrer noopener\">plastic deformation<\/a> and even above the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Melting_point\" target=\"_blank\" rel=\"noreferrer noopener\">melting point<\/a>. Exotic <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Alloy\" target=\"_blank\" rel=\"noreferrer noopener\">alloys<\/a>, sophisticated <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Air_cooling\" target=\"_blank\" rel=\"noreferrer noopener\">air cooling<\/a> schemes and special mechanical design are needed to keep the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Physical_stress\" target=\"_blank\" rel=\"noreferrer noopener\">physical stresses<\/a> within the strength of the material. <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rotating_seal\" target=\"_blank\" rel=\"noreferrer noopener\">Rotating seals<\/a> must withstand harsh conditions for 10 years, 20,000 missions and rotating at 10 to 20,000 rpm.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-LN161021-49\" target=\"_blank\" rel=\"noreferrer noopener\">[49]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u4e00\u4e2a100\u514b\uff083.5\u76ce\u53f8\uff09\u7684\u6da1\u8f6e\u53f6\u7247\u627f\u53d7\u77401,700\u00b0C\uff083,100\u00b0F\uff09\u7684\u9ad8\u6e29\uff0c17\u5df4\uff08250\u78c5\/\u5e73\u65b9\u82f1\u5bf8\uff09\u7684\u9ad8\u538b\u548c40\u5343\u725b\uff089,000\u78c5\u529b\uff09\u7684\u79bb\u5fc3\u529b\uff0c\u8fdc\u8d85\u8fc7\u5851\u6027\u53d8\u5f62\u70b9\u751a\u81f3\u8d85\u8fc7\u7194\u70b9\u3002\u9700\u8981\u4f7f\u7528\u7279\u6b8a\u7684\u5408\u91d1\u3001\u590d\u6742\u7684\u7a7a\u6c14\u51b7\u5374\u65b9\u6848\u548c\u7279\u6b8a\u7684\u673a\u68b0\u8bbe\u8ba1\u6765\u4f7f\u7269\u7406\u5e94\u529b\u4fdd\u6301\u5728\u6750\u6599\u7684\u5f3a\u5ea6\u8303\u56f4\u5185\u3002\u65cb\u8f6c\u5bc6\u5c01\u4ef6\u5fc5\u987b\u80fd\u591f\u5728\u8270\u82e6\u73af\u5883\u4e0b\u5de5\u4f5c10\u5e74\uff0c\u5b8c\u621020,000\u6b21\u4efb\u52a1\uff0c\u5e76\u4ee510\u81f320,000\u8f6c\/\u5206\u949f\u7684\u901f\u5ea6\u65cb\u8f6c\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_29\"><strong>6.3 \u98ce\u6247\u53f6\u7247 | Fan blades<\/strong><\/h3>\n\n\n\n<p>Fan blades have been growing as jet engines have been getting bigger: each fan blade carries the equivalent of nine <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Double-decker_bus\" target=\"_blank\" rel=\"noreferrer noopener\">double-decker buses<\/a> and swallows air the equivalent volume of a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Squash_court\" target=\"_blank\" rel=\"noreferrer noopener\">squash court<\/a> every second. Advances in <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Computational_fluid_dynamics\" target=\"_blank\" rel=\"noreferrer noopener\">computational fluid dynamics<\/a> (CFD) modelling have permitted complex, 3D curved shapes with very wide <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Chord_%28aeronautics%29\" target=\"_blank\" rel=\"noreferrer noopener\">chord<\/a>, keeping the fan capabilities while minimizing the blade count to lower costs. Coincidentally, the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Bypass_ratio\" target=\"_blank\" rel=\"noreferrer noopener\">bypass ratio<\/a> grew to achieve higher <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Propulsive_efficiency\" target=\"_blank\" rel=\"noreferrer noopener\">propulsive efficiency<\/a> and the fan diameter increased.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-MRO28sep2017-50\" target=\"_blank\" rel=\"noreferrer noopener\">[50]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u968f\u7740\u55b7\u6c14\u53d1\u52a8\u673a\u7684\u5c3a\u5bf8\u8d8a\u6765\u8d8a\u5927\uff0c\u98ce\u6247\u53f6\u7247\u4e5f\u5728\u4e0d\u65ad\u589e\u957f\uff1a\u6bcf\u4e2a\u98ce\u6247\u53f6\u7247\u76f8\u5f53\u4e8e\u4e5d\u8f86\u53cc\u5c42\u5df4\u58eb\u7684\u8d1f\u8f7d\uff0c\u5e76\u4e14\u6bcf\u79d2\u5438\u5165\u76f8\u5f53\u4e8e\u4e00\u4e2a\u58c1\u7403\u573a\u7684\u7a7a\u6c14\u4f53\u79ef\u3002\u8ba1\u7b97\u6d41\u4f53\u529b\u5b66\uff08CFD\uff09\u5efa\u6a21\u7684\u8fdb\u6b65\u4f7f\u5f97\u53ef\u4ee5\u8bbe\u8ba1\u590d\u6742\u7684\u3001\u4e09\u7ef4\u66f2\u9762\u7684\u53f6\u7247\uff0c\u5177\u6709\u975e\u5e38\u5bbd\u7684\u5f26\u957f\uff0c\u65e2\u53ef\u4ee5\u4fdd\u6301\u98ce\u6247\u7684\u6027\u80fd\uff0c\u53c8\u80fd\u5c3d\u91cf\u51cf\u5c11\u53f6\u7247\u6570\u91cf\u4ee5\u964d\u4f4e\u6210\u672c\u3002\u5de7\u5408\u7684\u662f\uff0c\u65c1\u901a\u6bd4\u589e\u52a0\u4ee5\u63d0\u9ad8\u63a8\u8fdb\u6548\u7387\uff0c\u98ce\u6247\u76f4\u5f84\u4e5f\u589e\u52a0\u4e86\u3002<\/p>\n\n\n\n<p>Rolls-Royce pioneered the hollow, <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Titanium\" target=\"_blank\" rel=\"noreferrer noopener\">titanium<\/a> wide-chord fan blade in the 1980s for aerodynamic efficiency and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Foreign_object_damage\" target=\"_blank\" rel=\"noreferrer noopener\">foreign object damage<\/a> resistance in the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/RB211\" target=\"_blank\" rel=\"noreferrer noopener\">RB211<\/a> then for the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_Trent\" target=\"_blank\" rel=\"noreferrer noopener\">Trent<\/a>. <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/GE_Aviation\" target=\"_blank\" rel=\"noreferrer noopener\">GE Aviation<\/a> introduced <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Carbon_fiber_composite\" target=\"_blank\" rel=\"noreferrer noopener\">carbon fiber composite<\/a> fan blades on the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/GE90\" target=\"_blank\" rel=\"noreferrer noopener\">GE90<\/a> in 1995, manufactured today with a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Carbon-fiber_tape\" target=\"_blank\" rel=\"noreferrer noopener\">carbon-fiber tape-layer<\/a> process. GE partner <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Safran\" target=\"_blank\" rel=\"noreferrer noopener\">Safran<\/a> developed a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/3D_weaving\" target=\"_blank\" rel=\"noreferrer noopener\">3D woven<\/a> technology with <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Albany_Engineered_Composites\" target=\"_blank\" rel=\"noreferrer noopener\">Albany Composites<\/a> for the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/CFM56\" target=\"_blank\" rel=\"noreferrer noopener\">CFM56<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/CFM_LEAP\" target=\"_blank\" rel=\"noreferrer noopener\">CFM LEAP<\/a> engines.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-MRO28sep2017-50\" target=\"_blank\" rel=\"noreferrer noopener\">[50]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u7f57\u5c14\u65af\u00b7\u7f57\u4f0a\u65af\uff08Rolls-Royce\uff09\u5728\u4e0a\u4e16\u7eaa80\u5e74\u4ee3\u4e3a\u4e86\u63d0\u9ad8\u7a7a\u6c14\u52a8\u529b\u6548\u7387\u548c\u62b5\u6297\u5f02\u7269\u635f\u4f24\uff0c\u5728RB211\u53d1\u52a8\u673a\u4e0a\u9996\u521b\u4e86\u7a7a\u5fc3\u7684\u949b\u5408\u91d1\u5bbd\u5f26\u98ce\u6247\u53f6\u7247\uff0c\u4e4b\u540e\u53c8\u5728\u7279\u4f26\u7279\uff08Trent\uff09\u53d1\u52a8\u673a\u4e0a\u91c7\u7528\u4e86\u8fd9\u4e00\u6280\u672f\u3002GE\u822a\u7a7a\u516c\u53f8\u4e8e1995\u5e74\u5728GE90\u53d1\u52a8\u673a\u4e0a\u5f15\u5165\u4e86\u78b3\u7ea4\u7ef4\u590d\u5408\u6750\u6599\u98ce\u6247\u53f6\u7247\uff0c\u76ee\u524d\u4f7f\u7528\u78b3\u7ea4\u7ef4\u5e26\u5c42\u5de5\u827a\u8fdb\u884c\u5236\u9020\u3002GE\u7684\u5408\u4f5c\u4f19\u4f34\u8d5b\u5cf0\u516c\u53f8\uff08Safran\uff09\u4e0eAlbany Composites\u5171\u540c\u5f00\u53d1\u4e86\u4e00\u79cd\u7528\u4e8eCFM56\u548cCFM LEAP\u53d1\u52a8\u673a\u7684\u4e09\u7ef4\u7f16\u7ec7\u6280\u672f\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_30\">6.4 \u672a\u6765\u7684\u8fdb\u6b65 | Future progress<\/h3>\n\n\n\n<p>Engine cores are shrinking as they are operating at higher <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Overall_pressure_ratio\" target=\"_blank\" rel=\"noreferrer noopener\">pressure ratios<\/a> and becoming more efficient, and become smaller compared to the fan as bypass ratios increase. Blade <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Tip_clearance\" target=\"_blank\" rel=\"noreferrer noopener\">tip clearances<\/a> are harder to maintain at the exit of the high-pressure compressor where blades are 0.5 in (13 mm) high or less; <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Structural_system\" target=\"_blank\" rel=\"noreferrer noopener\">backbone<\/a> bending further affects clearance control as the core is proportionately longer and thinner and the fan to low-pressure turbine driveshaft is in constrained space within the core.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-AvWeek26Mar2015-51\" target=\"_blank\" rel=\"noreferrer noopener\">[51]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u968f\u7740\u53d1\u52a8\u673a\u7684\u5de5\u4f5c\u538b\u529b\u6bd4\u589e\u52a0\u548c\u6548\u7387\u63d0\u9ad8\uff0c\u53d1\u52a8\u673a\u6838\u5fc3\u6b63\u5728\u7f29\u5c0f\uff0c\u5e76\u4e14\u4e0e\u98ce\u6247\u76f8\u6bd4\uff0c\u6838\u5fc3\u5728\u65c1\u901a\u6bd4\u589e\u52a0\u65f6\u53d8\u5f97\u66f4\u5c0f\u3002\u5728\u9ad8\u538b\u538b\u7f29\u673a\u51fa\u53e3\u5904\uff0c\u53f6\u7247\u5c16\u7aef\u95f4\u9699\u7684\u7ef4\u62a4\u66f4\u52a0\u56f0\u96be\uff0c\u56e0\u4e3a\u53f6\u7247\u7684\u9ad8\u5ea6\u53ea\u67090.5\u82f1\u5bf8\uff0813\u6beb\u7c73\uff09\u6216\u66f4\u4f4e\uff1b\u9aa8\u67b6\u7684\u5f2f\u66f2\u8fdb\u4e00\u6b65\u5f71\u54cd\u4e86\u95f4\u9699\u63a7\u5236\uff0c\u56e0\u4e3a\u6838\u5fc3\u90e8\u5206\u76f8\u5bf9\u8f83\u957f\u800c\u8584\uff0c\u800c\u98ce\u6247\u4e0e\u4f4e\u538b\u6da1\u8f6e\u9a71\u52a8\u8f74\u5219\u4f4d\u4e8e\u6838\u5fc3\u5185\u7684\u53d7\u9650\u7a7a\u95f4\u5185\u3002<\/p>\n\n\n\n<p>For <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney<\/a> VP technology and environment <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Alan_H._Epstein\" target=\"_blank\" rel=\"noreferrer noopener\">Alan Epstein<\/a> &#8220;Over the history of commercial aviation, we have gone from 20% to 40% [cruise efficiency], and there is a consensus among the engine community that we can probably get to 60%&#8221;.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-AvWeek8Aug2017-52\" target=\"_blank\" rel=\"noreferrer noopener\">[52]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u666e\u60e0\u516c\u53f8\u6280\u672f\u4e0e\u73af\u5883\u526f\u603b\u88c1\u827e\u4f26\u00b7\u7231\u6cfc\u65af\u5766\u8868\u793a\uff1a\u201c\u5728\u5546\u4e1a\u822a\u7a7a\u5386\u53f2\u4e0a\uff0c\u6211\u4eec\u7684\u5de1\u822a\u6548\u7387\u4ece20%\u63d0\u9ad8\u5230\u4e8640%\uff0c\u53d1\u52a8\u673a\u754c\u666e\u904d\u8ba4\u4e3a\u6211\u4eec\u53ef\u80fd\u53ef\u4ee5\u8fbe\u523060%\u7684\u6548\u7387\u3002\u201d<\/p>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Geared_turbofan\" target=\"_blank\" rel=\"noreferrer noopener\">Geared turbofans<\/a> and further fan <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Overall_pressure_ratio\" target=\"_blank\" rel=\"noreferrer noopener\">pressure ratio<\/a> reductions will continue to improve <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Propulsive_efficiency\" target=\"_blank\" rel=\"noreferrer noopener\">propulsive efficiency<\/a>. The second phase of the FAA&#8217;s Continuous Lower Energy, Emissions and Noise (CLEEN) program is targeting for the late 2020s reductions of 33% fuel burn, 60% emissions and 32 dB EPNdb noise compared with the 2000s state-of-the-art.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-faa-cleen-53\" target=\"_blank\" rel=\"noreferrer noopener\">[53]<\/a> In summer 2017 at <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/NASA_Glenn_Research_Center\" target=\"_blank\" rel=\"noreferrer noopener\">NASA Glenn Research Center<\/a> in <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Cleveland%2C_Ohio\" target=\"_blank\" rel=\"noreferrer noopener\">Cleveland, Ohio<\/a>, Pratt has finished testing a very-low-pressure-ratio fan on a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/PW1000G\" target=\"_blank\" rel=\"noreferrer noopener\">PW1000G<\/a>, resembling an <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Open_rotor\" target=\"_blank\" rel=\"noreferrer noopener\">open rotor<\/a> with fewer blades than the PW1000G&#8217;s 20.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-AvWeek8Aug2017-52\" target=\"_blank\" rel=\"noreferrer noopener\">[52]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u901a\u8fc7\u9f7f\u8f6e\u6da1\u8f6e\u98ce\u6247\u548c\u8fdb\u4e00\u6b65\u964d\u4f4e\u98ce\u6247\u538b\u529b\u6bd4\uff0c\u63a8\u8fdb\u6548\u7387\u5c06\u7ee7\u7eed\u5f97\u5230\u63d0\u9ad8\u3002\u7f8e\u56fd\u8054\u90a6\u822a\u7a7a\u7ba1\u7406\u5c40FAA\uff09\u201c\u6301\u7eed\u4f4e\u80fd\u3001\u4f4e\u6392\u653e\u548c\u4f4e\u566a\u97f3\u201d\uff08CLEEN\uff09\u8ba1\u5212\u7684\u7b2c\u4e8c\u9636\u6bb5\u65e8\u5728\u57282020\u5e74\u4ee3\u540e\u671f\u76f8\u6bd4\u4e8e2000\u5e74\u4ee3\u7684\u5148\u8fdb\u6280\u672f\u6c34\u5e73\uff0c\u5b9e\u73b0\u71c3\u6cb9\u71c3\u70e7\u964d\u4f4e33%\u3001\u6392\u653e\u964d\u4f4e60%\u548c\u566a\u97f3\u964d\u4f4e32 dB EPNdb\u7684\u76ee\u6807\u30022017\u5e74\u590f\u5b63\uff0c\u5728\u4fc4\u4ea5\u4fc4\u5dde\u514b\u5229\u592b\u5170\u7684NASA\u683c\u4f26\u7814\u7a76\u4e2d\u5fc3\uff0c\u666e\u60e0\u516c\u53f8\u5df2\u7ecf\u5b8c\u6210\u4e86\u5bf9PW1000G\u53d1\u52a8\u673a\u4e0a\u7684\u4e00\u4e2a\u975e\u5e38\u4f4e\u538b\u6bd4\u98ce\u6247\u7684\u6d4b\u8bd5\uff0c\u8be5\u98ce\u6247\u7c7b\u4f3c\u4e8e\u5177\u6709\u8f83\u5c11\u53f6\u7247\u7684\u5f00\u653e\u5f0f\u8f6c\u5b50\uff0c\u5c11\u4e8ePW1000G\u768420\u7247\u53f6\u7247\u3002<\/p>\n\n\n\n<p>The weight and size of the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Nacelle\" target=\"_blank\" rel=\"noreferrer noopener\">nacelle<\/a> would be reduced by a short duct inlet, imposing higher aerodynamic turning loads on the blades and leaving less space for soundproofing, but a lower-pressure-ratio fan is slower. <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/UTC_Aerospace_Systems\" target=\"_blank\" rel=\"noreferrer noopener\">UTC Aerospace Systems<\/a> Aerostructures will have a full-scale ground test in 2019 of its low-drag Integrated Propulsion System with a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Thrust_reverser\" target=\"_blank\" rel=\"noreferrer noopener\">thrust reverser<\/a>, improving fuel burn by 1% and with 2.5-3 EPNdB lower noise.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-AvWeek8Aug2017-52\" target=\"_blank\" rel=\"noreferrer noopener\">[52]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u901a\u8fc7\u4f7f\u7528\u8f83\u77ed\u7684\u8fdb\u6c14\u9053\uff0c\u53d1\u52a8\u673a\u5916\u58f3\u7684\u91cd\u91cf\u548c\u5c3a\u5bf8\u53ef\u4ee5\u51cf\u5c0f\uff0c\u4f46\u8fd9\u4f1a\u7ed9\u53f6\u7247\u65bd\u52a0\u66f4\u9ad8\u7684\u7a7a\u6c14\u52a8\u529b\u5b66\u8f6c\u5411\u8d1f\u8f7d\uff0c\u5e76\u4e14\u7559\u4e0b\u8f83\u5c11\u7684\u7a7a\u95f4\u7528\u4e8e\u9694\u97f3\u3002\u7136\u800c\uff0c\u4f4e\u538b\u6bd4\u98ce\u6247\u7684\u8f6c\u901f\u8f83\u6162\u3002UTC\u822a\u7a7a\u822a\u5929\u7cfb\u7edf\u516c\u53f8\u7684\u822a\u7a7a\u7ed3\u6784\u90e8\u95e8\u5c06\u57282019\u5e74\u8fdb\u884c\u5176\u4f4e\u963b\u529b\u7efc\u5408\u63a8\u8fdb\u7cfb\u7edf\u7684\u5168\u5c3a\u5bf8\u5730\u9762\u6d4b\u8bd5\uff0c\u8be5\u7cfb\u7edf\u914d\u5907\u4e86\u4e00\u4e2a\u63a8\u529b\u53cd\u5411\u5668\uff0c\u71c3\u6cb9\u6d88\u8017\u964d\u4f4e\u4e861%\uff0c\u566a\u97f3\u964d\u4f4e\u4e862.5-3 EPNdB\u3002<\/p>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Safran\" target=\"_blank\" rel=\"noreferrer noopener\">Safran<\/a> can probably deliver another 10\u201315% in fuel efficiency through the mid-2020s before reaching an <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Asymptote\" target=\"_blank\" rel=\"noreferrer noopener\">asymptote<\/a>, and next will have to introduce a breakthrough: to increase the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Bypass_ratio\" target=\"_blank\" rel=\"noreferrer noopener\">bypass ratio<\/a> to 35:1 instead of 11:1 for the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/CFM_LEAP\" target=\"_blank\" rel=\"noreferrer noopener\">CFM LEAP<\/a>, it is demonstrating a counterrotating <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Open_rotor\" target=\"_blank\" rel=\"noreferrer noopener\">open rotor<\/a> unducted fan (propfan) in <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Istres%2C_France\" target=\"_blank\" rel=\"noreferrer noopener\">Istres, France<\/a>, under the European <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Clean_Sky\" target=\"_blank\" rel=\"noreferrer noopener\">Clean Sky<\/a> technology program. <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Computational_fluid_dynamics\" target=\"_blank\" rel=\"noreferrer noopener\">Modeling<\/a> advances and high <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Specific_strength\" target=\"_blank\" rel=\"noreferrer noopener\">specific strength<\/a> materials may help it succeed where previous attempts failed. When noise levels will be within current standards and similar to the Leap engine, 15% lower fuel burn will be available and for that Safran is testing its controls, vibration and operation, while <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Airframe\" target=\"_blank\" rel=\"noreferrer noopener\">airframe<\/a> integration is still challenging.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-AvWeek8Aug2017-52\" target=\"_blank\" rel=\"noreferrer noopener\">[52]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u52302020\u5e74\u4ee3\u4e2d\u671f\uff0c\u8428\u5f17\u5170\u516c\u53f8\u53ef\u80fd\u53ef\u4ee5\u901a\u8fc7\u5f15\u5165\u4e00\u9879\u7a81\u7834\u6027\u6280\u672f\uff0c\u5c06\u71c3\u6cb9\u6548\u7387\u518d\u63d0\u9ad810-15%\u3002\u4ed6\u4eec\u8ba1\u5212\u5c06\u526f\u63a8\u529b\u6bd4\u63d0\u9ad8\u523035:1\uff0c\u800c\u4e0d\u662fCFM LEAP\u53d1\u52a8\u673a\u768411:1\u3002\u4ed6\u4eec\u6b63\u5728\u6cd5\u56fd\u4f0a\u65af\u7279\u5c14\u8fdb\u884c\u4e00\u4e2a\u53cd\u5411\u65cb\u8f6c\u7684\u5f00\u653e\u5f0f\u8f6c\u5b50\u65e0\u7f69\u98ce\u6247\uff08propfan\uff09\u7684\u5c55\u793a\uff0c\u8be5\u9879\u76ee\u662f\u6b27\u6d32Clean Sky\u6280\u672f\u8ba1\u5212\u7684\u4e00\u90e8\u5206\u3002\u901a\u8fc7\u6a21\u62df\u8fdb\u5c55\u548c\u9ad8\u7279\u6b8a\u5f3a\u5ea6\u6750\u6599\uff0c\u4ed6\u4eec\u53ef\u80fd\u80fd\u591f\u5728\u4ee5\u524d\u7684\u5c1d\u8bd5\u4e2d\u5931\u8d25\u7684\u5730\u65b9\u53d6\u5f97\u6210\u529f\u3002\u5f53\u566a\u97f3\u6c34\u5e73\u7b26\u5408\u5f53\u524d\u6807\u51c6\u5e76\u4e0eLeap\u53d1\u52a8\u673a\u76f8\u4f3c\u65f6\uff0c\u5c06\u53ef\u5b9e\u73b015%\u7684\u71c3\u6cb9\u71c3\u70e7\u964d\u4f4e\u3002\u4e3a\u6b64\uff0c\u8428\u5f17\u5170\u516c\u53f8\u6b63\u5728\u6d4b\u8bd5\u5176\u63a7\u5236\u3001\u632f\u52a8\u548c\u64cd\u4f5c\uff0c\u4f46\u673a\u8eab\u6574\u5408\u4ecd\u7136\u5177\u6709\u6311\u6218\u6027\u3002<\/p>\n\n\n\n<p>For <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/GE_Aviation\" target=\"_blank\" rel=\"noreferrer noopener\">GE Aviation<\/a>, the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Energy_density\" target=\"_blank\" rel=\"noreferrer noopener\">energy density<\/a> of jet fuel still maximises the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Breguet_range_equation\" target=\"_blank\" rel=\"noreferrer noopener\">Breguet range equation<\/a> and higher pressure ratio cores; lower pressure ratio fans, low-loss inlets and lighter structures can further improve thermal, transfer and propulsive efficiency. Under the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/U.S._Air_Force\" target=\"_blank\" rel=\"noreferrer noopener\">U.S. Air Force<\/a>\u2019s <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Adaptive_Engine_Transition_Program\" target=\"_blank\" rel=\"noreferrer noopener\">Adaptive Engine Transition Program<\/a>, adaptive <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Thermodynamic_cycle\" target=\"_blank\" rel=\"noreferrer noopener\">thermodynamic cycles<\/a> will be used for the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Sixth-generation_jet_fighter\" target=\"_blank\" rel=\"noreferrer noopener\">sixth-generation jet fighter<\/a>, based on a modified <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Brayton_cycle\" target=\"_blank\" rel=\"noreferrer noopener\">Brayton cycle<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Constant_volume\" target=\"_blank\" rel=\"noreferrer noopener\">Constant volume<\/a> combustion. <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Additive_manufacturing\" target=\"_blank\" rel=\"noreferrer noopener\">Additive manufacturing<\/a> in the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/General_Electric_Advanced_Turboprop\" target=\"_blank\" rel=\"noreferrer noopener\">advanced turboprop<\/a> will reduce weight by 5% and fuel burn by 20%.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-AvWeek8Aug2017-52\" target=\"_blank\" rel=\"noreferrer noopener\">[52]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u5bf9\u4e8eGE\u822a\u7a7a\u516c\u53f8\u6765\u8bf4\uff0c\u55b7\u6c14\u71c3\u6599\u7684\u80fd\u91cf\u5bc6\u5ea6\u4ecd\u7136\u6700\u5927\u5316\u4e86\u5e03\u96f7\u76d6\u8328\u822a\u7a0b\u65b9\u7a0b\u548c\u66f4\u9ad8\u538b\u529b\u6bd4\u7684\u6838\uff1b\u8f83\u4f4e\u538b\u529b\u6bd4\u7684\u98ce\u6247\u3001\u4f4e\u635f\u8017\u7684\u8fdb\u6c14\u9053\u548c\u66f4\u8f7b\u7684\u7ed3\u6784\u53ef\u4ee5\u8fdb\u4e00\u6b65\u63d0\u9ad8\u70ed\u80fd\u3001\u4f20\u70ed\u548c\u63a8\u529b\u6548\u7387\u3002\u5728\u7f8e\u56fd\u7a7a\u519b\u7684\u81ea\u9002\u5e94\u53d1\u52a8\u673a\u8fc7\u6e21\u8ba1\u5212\u4e0b\uff0c\u81ea\u9002\u5e94\u70ed\u529b\u5faa\u73af\u5c06\u7528\u4e8e\u7b2c\u516d\u4ee3\u55b7\u6c14\u5f0f\u6218\u6597\u673a\uff0c\u57fa\u4e8e\u6539\u8fdb\u7684\u5e03\u96f7\u987f\u5faa\u73af\u548c\u6052\u5bb9\u71c3\u70e7\u3002\u5148\u8fdb\u6da1\u8f6e\u87ba\u65cb\u6868\u53d1\u52a8\u673a\u4e2d\u7684\u589e\u6750\u5236\u9020\u5c06\u51cf\u8f7b\u91cd\u91cf5%\u5e76\u964d\u4f4e\u71c3\u6cb9\u71c3\u70e720%\u3002<\/p>\n\n\n\n<p>Rotating and static <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Ceramic_matrix_composite\" target=\"_blank\" rel=\"noreferrer noopener\">ceramic matrix composite<\/a> (CMC) parts operates 500 \u00b0F (260 \u00b0C) hotter than metal and are one-third its weight. With $21.9 million from the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Air_Force_Research_Laboratory\" target=\"_blank\" rel=\"noreferrer noopener\">Air Force Research Laboratory<\/a>, GE is investing $200 million in a CMC facility in <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Huntsville%2C_Alabama\" target=\"_blank\" rel=\"noreferrer noopener\">Huntsville, Alabama<\/a>, in addition to its <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Asheville%2C_North_Carolina\" target=\"_blank\" rel=\"noreferrer noopener\">Asheville, North Carolina<\/a> site, mass-producing <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Silicon_carbide\" target=\"_blank\" rel=\"noreferrer noopener\">silicon carbide<\/a> matrix with silicon-carbide fibers in 2018. CMCs will be used ten times more by the mid-2020s: the CFM LEAP requires 18 CMC turbine shrouds per engine and the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/GE9X\" target=\"_blank\" rel=\"noreferrer noopener\">GE9X<\/a> will use it in the combustor and for 42 HP turbine nozzles.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-AvWeek8Aug2017-52\" target=\"_blank\" rel=\"noreferrer noopener\">[52]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u65cb\u8f6c\u548c\u9759\u6b62\u7684\u9676\u74f7\u57fa\u590d\u5408\u6750\u6599\uff08CMC\uff09\u96f6\u90e8\u4ef6\u7684\u8fd0\u884c\u6e29\u5ea6\u6bd4\u91d1\u5c5e\u9ad8500\u00b0F\uff08260\u00b0C\uff09\uff0c\u91cd\u91cf\u53ea\u6709\u5176\u4e09\u5206\u4e4b\u4e00\u3002GE\u6b63\u5728\u4ece\u7a7a\u519b\u7814\u7a76\u5b9e\u9a8c\u5ba4\u83b7\u5f972190\u4e07\u7f8e\u5143\u7684\u8d44\u91d1\uff0c\u5728\u4e9a\u62c9\u5df4\u9a6c\u5dde\u4ea8\u8328\u7ef4\u5c14\u5efa\u7acb\u4e00\u5ea7CMC\u8bbe\u65bd\uff0c\u6b64\u5916\u8fd8\u6709\u4f4d\u4e8e\u5317\u5361\u7f57\u6765\u7eb3\u5dde\u963f\u4ec0\u7ef4\u5c14\u7684\u5de5\u5382\u30022018\u5e74\uff0cGE\u5c06\u5f00\u59cb\u5927\u89c4\u6a21\u751f\u4ea7\u7845\u78b3\u5316\u7269\u57fa\u4f53\u548c\u78b3\u5316\u7845\u7ea4\u7ef4\u7684CMC\u3002\u52302020\u5e74\u4ee3\u4e2d\u671f\uff0cCMC\u7684\u4f7f\u7528\u91cf\u5c06\u589e\u52a0\u5341\u500d\uff1aCFM LEAP\u53d1\u52a8\u673a\u6bcf\u4e2a\u9700\u898118\u4e2aCMC\u6da1\u8f6e\u7f69\uff0c\u800cGE9X\u53d1\u52a8\u673a\u5c06\u5728\u71c3\u70e7\u5ba4\u548c42\u4e2a\u9ad8\u538b\u6da1\u8f6e\u55b7\u5634\u4e2d\u4f7f\u7528CMC\u6750\u6599\u3002<\/p>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_Plc\" target=\"_blank\" rel=\"noreferrer noopener\">Rolls-Royce Plc<\/a> aim for a 60:1 pressure ratio core for the 2020s <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Ultrafan\" target=\"_blank\" rel=\"noreferrer noopener\">Ultrafan<\/a> and began ground tests of its 100,000 hp (75,000 kW) gear for 100,000 lbf (440 kN) and 15:1 bypass ratios. Nearly <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Stoichiometric\" target=\"_blank\" rel=\"noreferrer noopener\">stoichiometric<\/a> turbine entry temperatures approaches the theoretical limit and its impact on emissions has to be balanced with environmental performance goals. Open rotors, lower pressure ratio fans and potentially <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Distributed_propulsion\" target=\"_blank\" rel=\"noreferrer noopener\">distributed propulsion<\/a> offer more room for better propulsive efficiency. Exotic cycles, <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Heat_exchanger\" target=\"_blank\" rel=\"noreferrer noopener\">heat exchangers<\/a> and pressure gain\/constant volume combustion can improve <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Thermodynamic_efficiency\" target=\"_blank\" rel=\"noreferrer noopener\">thermodynamic efficiency<\/a>. Additive manufacturing could be an enabler for <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Intercooler\" target=\"_blank\" rel=\"noreferrer noopener\">intercooler<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Recuperator\" target=\"_blank\" rel=\"noreferrer noopener\">recuperators<\/a>. Closer airframe integration and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Hybrid_electric_vehicle%23Aircraft\" target=\"_blank\" rel=\"noreferrer noopener\">hybrid<\/a> or <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Electric_aircraft\" target=\"_blank\" rel=\"noreferrer noopener\">electric aircraft<\/a> can be combined with gas turbines.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-AvWeek8Aug2017-52\" target=\"_blank\" rel=\"noreferrer noopener\">[52]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u52b3\u65af\u83b1\u65af\u516c\u53f8\u7684\u76ee\u6807\u662f\u57282020\u5e74\u4ee3\u7684Ultrafan\u53d1\u52a8\u673a\u4e2d\u5b9e\u73b060:1\u7684\u538b\u529b\u6bd4\u6838\u5fc3\uff0c\u5e76\u5df2\u5f00\u59cb\u5bf9\u517610\u4e07\u9a6c\u529b\uff0875,000\u5343\u74e6\uff09\u7684\u9f7f\u8f6e\u8fdb\u884c100,000\u78c5\uff08440\u5343\u725b\u987f\uff09\u548c15:1\u7684\u526f\u63a8\u529b\u6bd4\u7684\u5730\u9762\u6d4b\u8bd5\u3002\u63a5\u8fd1\u5316\u5b66\u8ba1\u91cf\u7684\u6da1\u8f6e\u8fdb\u53e3\u6e29\u5ea6\u63a5\u8fd1\u7406\u8bba\u6781\u9650\uff0c\u5176\u5bf9\u6392\u653e\u7684\u5f71\u54cd\u5fc5\u987b\u4e0e\u73af\u5883\u6027\u80fd\u76ee\u6807\u76f8\u5e73\u8861\u3002\u5f00\u653e\u5f0f\u8f6c\u5b50\u3001\u8f83\u4f4e\u538b\u529b\u6bd4\u7684\u98ce\u6247\u548c\u6f5c\u5728\u7684\u5206\u5e03\u5f0f\u63a8\u8fdb\u6280\u672f\u63d0\u4f9b\u4e86\u66f4\u591a\u6539\u5584\u63a8\u529b\u6548\u7387\u7684\u7a7a\u95f4\u3002\u5f02\u7c7b\u5faa\u73af\u3001\u70ed\u4ea4\u6362\u5668\u548c\u589e\u538b\/\u6052\u5bb9\u71c3\u70e7\u53ef\u4ee5\u63d0\u9ad8\u70ed\u529b\u5b66\u6548\u7387\u3002\u589e\u6750\u5236\u9020\u6280\u672f\u53ef\u4ee5\u4e3a\u4e2d\u51b7\u5668\u548c\u56de\u6536\u5668\u63d0\u4f9b\u53ef\u80fd\u3002\u66f4\u7d27\u5bc6\u7684\u673a\u8eab\u6574\u5408\u548c\u6df7\u5408\u52a8\u529b\u6216\u7535\u52a8\u98de\u673a\u53ef\u4ee5\u4e0e\u71c3\u6c14\u6da1\u8f6e\u76f8\u7ed3\u5408\u3002<\/p>\n\n\n\n<p>Current Rolls-Royce engines have a 72\u201382% propulsive efficiency and 42\u201349% thermal efficiency for a 0.63\u20130.49 lb\/lbf\/h (64,000\u201350,000 g\/kN\/h) <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Thrust_specific_fuel_consumption\" target=\"_blank\" rel=\"noreferrer noopener\">TSFC<\/a> at Mach 0.8, and aim for theoretical limits of 95% for open rotor propulsive efficiency and 60% for thermal efficiency with stoichiometric <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbine\" target=\"_blank\" rel=\"noreferrer noopener\">turbine<\/a> entry temperature and 80:1 <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Overall_pressure_ratio\" target=\"_blank\" rel=\"noreferrer noopener\">overall pressure ratio<\/a> for a 0.35 lb\/lbf\/h (36,000 g\/kN\/h) TSFC<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-54\" target=\"_blank\" rel=\"noreferrer noopener\">[54]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u76ee\u524d\u52b3\u65af\u83b1\u65af\u7684\u53d1\u52a8\u673a\u5728Mach 0.8\u4e0b\u5177\u670972-82%\u7684\u63a8\u529b\u6548\u7387\u548c42-49%\u7684\u70ed\u6548\u7387\uff0c\u71c3\u6cb9\u6d88\u8017\u7387\u4e3a0.63-0.49\u78c5\/\u5343\u78c5\u63a8\u529b\/\u5c0f\u65f6\uff0864,000-50,000\u514b\/\u5343\u725b\u987f\/\u5c0f\u65f6\uff09\u3002\u52b3\u65af\u83b1\u65af\u7684\u76ee\u6807\u662f\u5728\u5177\u6709\u5316\u5b66\u8ba1\u91cf\u6da1\u8f6e\u8fdb\u53e3\u6e29\u5ea6\u548c80:1\u603b\u538b\u529b\u6bd4\u7684\u60c5\u51b5\u4e0b\uff0c\u5b9e\u73b0\u5f00\u653e\u8f6c\u5b50\u7684\u63a8\u529b\u6548\u7387\u8fbe\u523095%\uff0c\u70ed\u6548\u7387\u8fbe\u523060%\uff0c\u71c3\u6cb9\u6d88\u8017\u7387\u4e3a0.35\u78c5\/\u5343\u78c5\u63a8\u529b\/\u5c0f\u65f6\uff0836,000\u514b\/\u5343\u725b\u987f\/\u5c0f\u65f6\uff09\u3002<\/p>\n\n\n\n<p>As teething troubles may not show up until several thousand hours, the latest turbofans technical problems disrupt <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Airline\" target=\"_blank\" rel=\"noreferrer noopener\">airlines<\/a> operations and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Aerospace_manufacturer\" target=\"_blank\" rel=\"noreferrer noopener\">manufacturers<\/a> deliveries while production rates are rising sharply. <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Trent_1000\" target=\"_blank\" rel=\"noreferrer noopener\">Trent 1000<\/a> cracked blades <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Aircraft_on_ground\" target=\"_blank\" rel=\"noreferrer noopener\">grounded<\/a> almost 50 <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Boeing_787\" target=\"_blank\" rel=\"noreferrer noopener\">Boeing 787s<\/a> and reduced <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/ETOPS\" target=\"_blank\" rel=\"noreferrer noopener\">ETOPS<\/a> to 2.3 hours down from 5.5, costing <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_plc\" target=\"_blank\" rel=\"noreferrer noopener\">Rolls-Royce plc<\/a> almost $950 million. <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/PW1000G\" target=\"_blank\" rel=\"noreferrer noopener\">PW1000G<\/a> knife-edge seal fractures have caused <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney<\/a> to fall way behind in deliveries, leaving about 100 engineless <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/A320neo\" target=\"_blank\" rel=\"noreferrer noopener\">A320neos<\/a> waiting for their powerplants. The <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/CFM_LEAP\" target=\"_blank\" rel=\"noreferrer noopener\">CFM LEAP<\/a> introduction was smoother but a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Ceramic_composite\" target=\"_blank\" rel=\"noreferrer noopener\">ceramic composite<\/a> HP Turbine coating is prematurely lost, necessitating a new design, causing 60 A320neo engine removal for modification, as deliveries are up to six weeks late.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-SeattleTimes15jun2018-55\" target=\"_blank\" rel=\"noreferrer noopener\">[55]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u7531\u4e8e\u4e00\u4e9b\u6280\u672f\u95ee\u9898\u53ef\u80fd\u8981\u5230\u6570\u5343\u5c0f\u65f6\u540e\u624d\u4f1a\u663e\u73b0\uff0c\u6700\u65b0\u7684\u6da1\u6247\u53d1\u52a8\u673a\u7684\u6280\u672f\u95ee\u9898\u6270\u4e71\u4e86\u822a\u7a7a\u516c\u53f8\u7684\u8fd0\u8425\u548c\u5236\u9020\u5546\u7684\u4ea4\u4ed8\uff0c\u800c\u751f\u4ea7\u7387\u5374\u5728\u6025\u5267\u4e0a\u5347\u3002\u7279\u4f26\u72791000\u53d1\u52a8\u673a\u7684\u53f6\u7247\u5f00\u88c2\u5bfc\u81f4\u8fd150\u67b6\u6ce2\u97f3787\u505c\u98de\uff0c\u5e76\u5c06ETOPS\u4ece5.5\u5c0f\u65f6\u964d\u4f4e\u52302.3\u5c0f\u65f6\uff0c\u7ed9\u52b3\u65af\u83b1\u65af\u516c\u53f8\u9020\u6210\u4e86\u8fd19.5\u4ebf\u7f8e\u5143\u7684\u635f\u5931\u3002PW1000G\u53d1\u52a8\u673a\u7684\u5200\u53e3\u5bc6\u5c01\u88c2\u7eb9\u5bfc\u81f4\u666e\u60e0\u516c\u53f8\u7684\u4ea4\u4ed8\u5927\u5927\u5ef6\u8fdf\uff0c\u7ea6\u6709100\u67b6\u6ca1\u6709\u53d1\u52a8\u673a\u7684A320neo\u7b49\u5f85\u7740\u5b89\u88c5\u52a8\u529b\u88c5\u7f6e\u3002CFM LEAP\u7684\u63a8\u51fa\u76f8\u5bf9\u987a\u5229\uff0c\u4f46\u9676\u74f7\u590d\u5408\u6750\u6599\u9ad8\u538b\u6da1\u8f6e\u6d82\u5c42\u8fc7\u65e9\u5931\u6548\uff0c\u9700\u8981\u8fdb\u884c\u65b0\u7684\u8bbe\u8ba1\uff0c\u5bfc\u81f460\u67b6A320neo\u53d1\u52a8\u673a\u9700\u8981\u8fdb\u884c\u4fee\u6539\uff0c\u4ea4\u4ed8\u65f6\u95f4\u5ef6\u8fdf\u4e86\u6700\u591a\u516d\u5468\u3002<\/p>\n\n\n\n<p>On a widebody, <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Safran\" target=\"_blank\" rel=\"noreferrer noopener\">Safran<\/a> estimates 5\u201310% of fuel could be saved by reducing power intake for hydraulic systems, while swapping to electrical power could save 30% of weight, as initiated on the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Boeing_787\" target=\"_blank\" rel=\"noreferrer noopener\">Boeing 787<\/a>, while <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_plc\" target=\"_blank\" rel=\"noreferrer noopener\">Rolls-Royce plc<\/a> hopes for up to 5%.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-56\" target=\"_blank\" rel=\"noreferrer noopener\">[56]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1aSafran\u4f30\u8ba1\uff0c\u5728\u5bbd\u4f53\u98de\u673a\u4e0a\uff0c\u901a\u8fc7\u51cf\u5c11\u6db2\u538b\u7cfb\u7edf\u7684\u52a8\u529b\u8f93\u5165\uff0c\u53ef\u4ee5\u8282\u77015-10%\u7684\u71c3\u6cb9\uff0c\u800c\u8f6c\u5411\u4f7f\u7528\u7535\u529b\u53ef\u4ee5\u8282\u770130%\u7684\u91cd\u91cf\uff0c\u6b63\u5982\u6ce2\u97f3787\u6240\u91c7\u53d6\u7684\u63aa\u65bd\uff0c\u800c\u52b3\u65af\u83b1\u65af\u516c\u53f8\u5219\u5e0c\u671b\u80fd\u591f\u8fbe\u52305%\u7684\u8282\u7701\u3002<\/p>\n\n\n\n<h2 class=\"wp-block-heading\" id=\"h_659034614_31\">7. \u5236\u9020\u5546 | Manufacturers<\/h2>\n\n\n\n<p><em>Main article: <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/List_of_turbofan_manufacturers\" target=\"_blank\" rel=\"noreferrer noopener\">List of turbofan manufacturers<\/a><\/em><br><em>\u4e3b\u6761\u76ee\uff1a\u6da1\u8f6e\u98ce\u6247\u53d1\u52a8\u673a\u5236\u9020\u5546\u5217\u8868<\/em><\/p>\n\n\n\n<p>The turbofan engine market is dominated by <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/GE_Aircraft_Engines\" target=\"_blank\" rel=\"noreferrer noopener\">General Electric<\/a>, <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Rolls-Royce_plc\" target=\"_blank\" rel=\"noreferrer noopener\">Rolls-Royce plc<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Pratt_%2526_Whitney\" target=\"_blank\" rel=\"noreferrer noopener\">Pratt &amp; Whitney<\/a>, in order of market share. General Electric and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Safran_Aircraft_Engines\" target=\"_blank\" rel=\"noreferrer noopener\">Safran<\/a> of France have a joint venture, <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/CFM_International\" target=\"_blank\" rel=\"noreferrer noopener\">CFM International<\/a>. Pratt &amp; Whitney also have a joint venture, <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/International_Aero_Engines\" target=\"_blank\" rel=\"noreferrer noopener\">International Aero Engines<\/a> with <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Japanese_Aero_Engine_Corporation\" target=\"_blank\" rel=\"noreferrer noopener\">Japanese Aero Engine Corporation<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/MTU_Aero_Engines\" target=\"_blank\" rel=\"noreferrer noopener\">MTU Aero Engines<\/a> of Germany, specializing in engines for the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Airbus_A320_family\" target=\"_blank\" rel=\"noreferrer noopener\">Airbus A320 family<\/a>. Pratt &amp; Whitney and General Electric have a joint venture, <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Engine_Alliance\" target=\"_blank\" rel=\"noreferrer noopener\">Engine Alliance<\/a> selling a range of engines for aircraft such as the <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Airbus_A380\" target=\"_blank\" rel=\"noreferrer noopener\">Airbus A380<\/a>.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6da1\u6247\u53d1\u52a8\u673a\u5e02\u573a\u7684\u4e3b\u5bfc\u5730\u4f4d\u7531\u901a\u7528\u7535\u6c14\u3001\u52b3\u65af\u83b1\u65af\u516c\u53f8\u548c\u666e\u60e0\u516c\u53f8\u4f9d\u636e\u5e02\u573a\u4efd\u989d\u6392\u540d\u786e\u5b9a\u3002\u901a\u7528\u7535\u6c14\u4e0e\u6cd5\u56fd\u8d5b\u5cf0\u6709\u4e00\u4e2a\u5408\u8d44\u4f01\u4e1a\uff0c\u5373CFM\u56fd\u9645\u516c\u53f8\u3002\u666e\u60e0\u516c\u53f8\u4e5f\u4e0e\u65e5\u672c\u822a\u7a7a\u53d1\u52a8\u673a\u516c\u53f8\u548c\u5fb7\u56fdMTU\u822a\u7a7a\u53d1\u52a8\u673a\u6709\u4e00\u4e2a\u5408\u8d44\u4f01\u4e1a\uff0c\u4e13\u95e8\u751f\u4ea7\u7a7a\u5ba2A320\u7cfb\u5217\u98de\u673a\u7684\u53d1\u52a8\u673a\u3002\u666e\u60e0\u516c\u53f8\u548c\u901a\u7528\u7535\u6c14\u8fd8\u6709\u4e00\u4e2a\u5408\u8d44\u4f01\u4e1a\uff0c\u5373\u53d1\u52a8\u673a\u8054\u76df\uff08Engine Alliance\uff09\uff0c\u9500\u552e\u4e00\u7cfb\u5217\u9002\u7528\u4e8e\u7a7a\u5ba2A380\u7b49\u98de\u673a\u7684\u53d1\u52a8\u673a\u3002<\/p>\n\n\n\n<p>For <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Airliner\" target=\"_blank\" rel=\"noreferrer noopener\">airliners<\/a> and <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Cargo_aircraft\" target=\"_blank\" rel=\"noreferrer noopener\">cargo aircraft<\/a>, the in-service fleet in 2016 is 60,000 engines and should grow to 103,000 in 2035 with 86,500 deliveries according to <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Flight_Global\" target=\"_blank\" rel=\"noreferrer noopener\">Flight Global<\/a>. A majority will be medium-thrust engines for <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Narrow-body_aircraft\" target=\"_blank\" rel=\"noreferrer noopener\">narrow-body aircraft<\/a> with 54,000 deliveries, for a fleet growing from 28,500 to 61,000. High-thrust engines for <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Wide-body_aircraft\" target=\"_blank\" rel=\"noreferrer noopener\">wide-body aircraft<\/a>, worth 40\u201345% of the market by value, will grow from 12,700 engines to over 21,000 with 18,500 deliveries. The <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Regional_jet\" target=\"_blank\" rel=\"noreferrer noopener\">regional jet<\/a> engines below 20,000 lb (89 kN) fleet will grow from 7,500 to 9,000 and the fleet of <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turboprop\" target=\"_blank\" rel=\"noreferrer noopener\">turboprops<\/a> for airliners will increase from 9,400 to 10,200. The manufacturers <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Market_share\" target=\"_blank\" rel=\"noreferrer noopener\">market share<\/a> should be led by CFM with 44% followed by Pratt &amp; Whitney with 29% and then Rolls-Royce and General Electric with 10% each.<a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Turbofan%23cite_note-57\" target=\"_blank\" rel=\"noreferrer noopener\">[57]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u6839\u636eFlight Global\u7684\u6570\u636e\uff0c2016\u5e74\u6c11\u822a\u5ba2\u673a\u548c\u8d27\u8fd0\u98de\u673a\u7684\u5728\u5f79\u53d1\u52a8\u673a\u6570\u91cf\u4e3a60,000\u53f0\uff0c\u9884\u8ba1\u52302035\u5e74\u5c06\u589e\u81f3103,000\u53f0\uff0c\u4ea4\u4ed8\u4e3a86,500\u53f0\u5927\u90e8\u5206\u53d1\u52a8\u673a\u5c06\u7528\u4e8e\u7a84\u4f53\u98de\u673a\uff0c\u4ea4\u4ed8\u6570\u91cf\u4e3a54,000\u53f0\uff0c\u4f7f\u5f97\u8be5\u7c7b\u98de\u673a\u7684\u5728\u5f79\u53d1\u52a8\u673a\u6570\u91cf\u4ece28,500\u53f0\u589e\u81f361,000\u53f0\u3002\u7528\u4e8e\u5bbd\u4f53\u98de\u673a\u7684\u5927\u63a8\u529b\u53d1\u52a8\u673a\uff08\u4ef7\u503c\u5360\u5e02\u573a\u603b\u503c\u768440-45%\uff09\u5c06\u4ece12,700\u53f0\u589e\u81f321,000\u53f0\uff0c\u4ea4\u4ed8\u6570\u91cf\u4e3a18,500\u53f0\u300220,000\u78c5\uff0889 kN\uff09\u4ee5\u4e0b\u7684\u5730\u533a\u5ba2\u673a\u53d1\u52a8\u673a\u6570\u91cf\u5c06\u4ece7,500\u53f0\u589e\u81f39,000\u53f0\uff0c\u800c\u4f9b\u6c11\u822a\u98de\u673a\u4f7f\u7528\u7684\u6da1\u6868\u53d1\u52a8\u673a\u7684\u6570\u91cf\u5c06\u4ece9,400\u53f0\u589e\u81f310,200\u53f0\u3002\u5236\u9020\u5546\u7684\u5e02\u573a\u4efd\u989d\u5c06\u7531CFM\u9886\u5148\uff0c\u5360\u6bd444%\uff0c\u5176\u6b21\u662f\u666e\u60e0\u516c\u53f8\uff0c\u5360\u6bd429%\uff0c\u52b3\u65af\u83b1\u65af\u548c\u901a\u7528\u7535\u6c14\u5404\u536010%\u3002<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"h_659034614_32\">7.1 \u6b63\u5728\u751f\u4ea7\u7684\u5546\u7528\u6da1\u8f6e\u98ce\u6247 | Commercial turbofans in production<\/h3>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/pic2.zhimg.com\/80\/v2-4e9f3717cd44fccce43bbbb60c8b85e1_720w.webp\" alt=\"\"\/><\/figure>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/pic1.zhimg.com\/80\/v2-eb2c5828d2c127a073a3d915cc2e2098_720w.webp\" alt=\"\"\/><\/figure>\n\n\n\n<h2 class=\"wp-block-heading\" id=\"h_659034614_33\"><strong>8. <\/strong>\u6781\u9ad8\u65c1\u901a\u6bd4\u55b7\u6c14\u53d1\u52a8\u673a | <strong>Extreme bypass jet engines<\/strong><\/h2>\n\n\n\n<p>In the 1970s, Rolls-Royce\/SNECMA tested a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/M45SD-02\" target=\"_blank\" rel=\"noreferrer noopener\">M45SD-02<\/a> turbofan fitted with variable-pitch fan blades to improve handling at ultralow fan pressure ratios and to provide thrust reverse down to zero aircraft speed. The engine was aimed at ultraquiet <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/STOL\" target=\"_blank\" rel=\"noreferrer noopener\">STOL<\/a> aircraft operating from city-centre airports.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u572820\u4e16\u7eaa70\u5e74\u4ee3\uff0c\u52b3\u65af\u83b1\u65af\/\u65af\u5948\u514b\u739b\uff08Rolls-Royce\/SNECMA\uff09\u6d4b\u8bd5\u4e86\u4e00\u6b3e\u642d\u8f7d\u53ef\u53d8\u6868\u53f6\u7684M45SD-02\u6da1\u6247\u53d1\u52a8\u673a\uff0c\u4ee5\u63d0\u9ad8\u5728\u8d85\u4f4e\u98ce\u6247\u538b\u529b\u6bd4\u4e0b\u7684\u64cd\u7eb5\u6027\uff0c\u5e76\u80fd\u5728\u98de\u673a\u901f\u5ea6\u964d\u81f3\u96f6\u65f6\u63d0\u4f9b\u63a8\u529b\u53cd\u5411\u3002\u8be5\u53d1\u52a8\u673a\u4e3b\u8981\u7528\u4e8e\u5728\u5e02\u4e2d\u5fc3\u673a\u573a\u8fd0\u8425\u7684\u8d85\u9759\u7684\u77ed\u8ddd\u79bb\u8d77\u964d\uff08STOL\uff09\u98de\u673a\u3002<\/p>\n\n\n\n<p>In a bid for increased efficiency with speed, a development of the <em>turbofan<\/em> and <em>turboprop<\/em> known as a <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Propfan\" target=\"_blank\" rel=\"noreferrer noopener\">propfan<\/a> engine was created that had an unducted fan. The fan blades are situated outside of the duct, so that it appears like a turboprop with wide scimitar-like blades. Both General Electric and Pratt &amp; Whitney\/Allison demonstrated propfan engines in the 1980s. Excessive cabin noise and relatively cheap jet fuel prevented the engines being put into service. The <a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Progress_D-27\" target=\"_blank\" rel=\"noreferrer noopener\">Progress D-27<\/a> propfan, developed in the U.S.S.R., was the only propfan engine equipped on a production aircraft.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u4e3a\u4e86\u63d0\u9ad8\u901f\u5ea6\u548c\u6548\u7387\uff0c\u6da1\u6247\u53d1\u52a8\u673a\u548c\u6da1\u6868\u53d1\u52a8\u673a\u7684\u4e00\u79cd\u6539\u826f\u578b\u53f7\u88ab\u521b\u5efa\u51fa\u6765\uff0c\u8fd9\u5c31\u662f\u62e5\u6709\u65e0\u62a4\u7f69\u98ce\u6247\u7684\u87ba\u65cb\u6868\u53d1\u52a8\u673a\uff08propfan engine\uff09\u3002\u98ce\u6247\u53f6\u7247\u4f4d\u4e8e\u62a4\u7f69\u4e4b\u5916\uff0c\u770b\u8d77\u6765\u50cf\u662f\u5e26\u6709\u5bbd\u5927\u5f2f\u5200\u5f62\u72b6\u7684\u6da1\u6868\u53d1\u52a8\u673a\u3002\u901a\u7528\u7535\u6c14\u548c\u666e\u62c9\u7279-\u60e0\u7279\u5c3c\/\u7231\u7acb\u4fe1\u572820\u4e16\u7eaa80\u5e74\u4ee3\u5c55\u793a\u4e86\u87ba\u65cb\u6868\u53d1\u52a8\u673a\u7684\u6280\u672f\u3002\u7136\u800c\uff0c\u8fc7\u9ad8\u7684\u673a\u8231\u566a\u97f3\u548c\u76f8\u5bf9\u4fbf\u5b9c\u7684\u55b7\u6c14\u71c3\u6599\u4f7f\u5f97\u8fd9\u79cd\u53d1\u52a8\u673a\u6ca1\u6709\u6295\u5165\u4f7f\u7528\u3002\u82cf\u8054\u7814\u53d1\u7684\u8fdb\u6b65D-27\u87ba\u65cb\u6868\u53d1\u52a8\u673a\u662f\u552f\u4e00\u4e00\u79cd\u5728\u751f\u4ea7\u98de\u673a\u4e0a\u914d\u5907\u7684\u87ba\u65cb\u6868\u53d1\u52a8\u673a\u3002<\/p>\n\n\n\n<h2 class=\"wp-block-heading\" id=\"h_659034614_34\"><strong>9. <\/strong>\u672f\u8bed | <strong>Terminology<\/strong><\/h2>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Afterburner\" target=\"_blank\" rel=\"noreferrer noopener\">Afterburner<\/a> \u52a0\u529b\u71c3\u70e7\u5ba4<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>jetpipe equipped for afterburning<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/659034614\/edit#cite_note-auto-62\">[62]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u4e3a\u52a0\u529b\u71c3\u70e7\u800c\u88c5\u5907\u7684\u55b7\u5c04\u7ba1[62]<\/li>\n<\/ul>\n\n\n\n<p>Augmentor \u6269\u589e\u5668<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>afterburner for turbofan with burning in hot and cold flows<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/659034614\/edit#cite_note-auto-62\">[62]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u5728\u51b7\u70ed\u6d41\u4e2d\u71c3\u70e7\u7684\u6da1\u8f6e\u98ce\u6247\u52a0\u529b\u71c3\u70e7\u5668[62]<\/li>\n<\/ul>\n\n\n\n<p>Bypass \u65c1\u901a<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>that part of the engine as distinct from the core in terms of components and airflow, eg that part of fan blading (fan outer) and stators which pass bypass air, bypass duct, bypass nozzle<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5728\u90e8\u4ef6\u548c\u6c14\u6d41\u65b9\u9762\u4e0e\u53d1\u52a8\u673a\u6838\u5fc3\u4e0d\u540c\u7684\u90a3\u90e8\u5206\uff0c\u5982\u98ce\u6247\u53f6\u7247(\u98ce\u6247\u5916\u90e8)\u548c\u5b9a\u5b50\u901a\u8fc7\u65c1\u901a\u7a7a\u6c14\u3001\u65c1\u901a\u7ba1\u9053\u3001\u65c1\u901a\u55b7\u5634\u7684\u90a3\u90e8\u5206<\/li>\n<\/ul>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Bypass_ratio\" target=\"_blank\" rel=\"noreferrer noopener\">Bypass ratio<\/a> \u65c1\u901a\u6bd4\/\u6db5\u9053\u6bd4<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>bypass air mass flow \/core air mass flow<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/659034614\/edit#cite_note-63\">[63]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u65c1\u901a\u7a7a\u6c14\u8d28\u91cf\u6d41\u91cf\/\u6838\u5fc3\u7a7a\u6c14\u8d28\u91cf\u6d41\u91cf[63]<\/li>\n<\/ul>\n\n\n\n<p>Core \u6838\u5fc3\u673a<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>that part of the engine as distinct from the bypass in terms of components and airflow, eg core cowl, core nozzle, core airflow and associated machinery, combustor and fuel system<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5728\u90e8\u4ef6\u548c\u6c14\u6d41\u65b9\u9762\u4e0e\u65c1\u901a\u901a\u9053\u4e0d\u540c\u7684\u90a3\u90e8\u5206\u53d1\u52a8\u673a\uff0c\u5982\u6838\u5fc3\u6574\u6d41\u7f69\u3001\u6838\u5fc3\u55b7\u5634\u3001\u6838\u5fc3\u6c14\u6d41\u548c\u76f8\u5173\u673a\u68b0\u3001\u71c3\u70e7\u5ba4\u548c\u71c3\u6599\u7cfb\u7edf<\/li>\n<\/ul>\n\n\n\n<p>Core power \u6838\u5fc3\u52a8\u529b<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>also known as &#8220;available energy&#8221; or &#8220;gas horsepower&#8221;. It is used to measure the theoretical (isentropic expansion) shaft work available from a gas generator or core by expanding hot, high pressure gas to ambient pressure. Since the power depends on the pressure and temperature of the gas (and the ambient pressure) a related figure of merit for thrust-producing engines is one which measures the thrust-producing potential from hot, high pressure gas and known as &#8220;stream thrust&#8221;. It is obtained by calculating the velocity obtained with isentropic expansion to atmospheric pressure. The significance of the thrust obtained appears when multiplied by the aircraft velocity to give the thrust work. The thrust work which is potentially available is far less than the gas horsepower due to the increasing waste in the exhaust kinetic energy with increasing pressure and temperature before expansion to atmospheric pressure. The two are related by the propulsive efficiency,<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/659034614\/edit#cite_note-64\">[64]<\/a> a measure of the energy wasted as a result of producing a force (ie thrust) in a fluid by increasing the speed (ie momentum) of the fluid.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u53ef\u7528\u80fd\u91cf\uff08\u4e5f\u79f0\u4e3a\u201c\u6c14\u4f53\u9a6c\u529b\u201d\uff09\u662f\u7528\u4e8e\u8861\u91cf\u6c14\u4f53\u53d1\u751f\u5668\u6216\u6838\u5fc3\u7684\u7406\u8bba\uff08\u7b49\u71b5\u81a8\u80c0\uff09\u8f74\u529f\u7387\uff0c\u901a\u8fc7\u5c06\u9ad8\u6e29\u9ad8\u538b\u6c14\u4f53\u81a8\u80c0\u81f3\u5927\u6c14\u538b\u529b\u6765\u83b7\u5f97\u3002\u7531\u4e8e\u529f\u7387\u53d6\u51b3\u4e8e\u6c14\u4f53\u7684\u538b\u529b\u548c\u6e29\u5ea6\uff08\u4ee5\u53ca\u73af\u5883\u538b\u529b\uff09\uff0c\u8861\u91cf\u4ea7\u751f\u63a8\u529b\u7684\u53d1\u52a8\u673a\u7684\u76f8\u5173\u6307\u6807\u662f\u901a\u8fc7\u7b49\u71b5\u81a8\u80c0\u5230\u5927\u6c14\u538b\u529b\u65f6\u8ba1\u7b97\u5f97\u5230\u7684\u6c14\u6d41\u63a8\u529b\uff08stream thrust\uff09\u3002\u63a8\u529b\u7684\u91cd\u8981\u6027\u4f53\u73b0\u5728\u4e58\u4ee5\u98de\u673a\u901f\u5ea6\u4ee5\u83b7\u5f97\u63a8\u529b\u4f5c\u4e1a\u65f6\u3002\u53ef\u7528\u7684\u63a8\u529b\u4f5c\u4e1a\u8fdc\u8fdc\u5c0f\u4e8e\u6c14\u4f53\u9a6c\u529b\uff0c\u8fd9\u662f\u7531\u4e8e\u5728\u81a8\u80c0\u81f3\u5927\u6c14\u538b\u529b\u4e4b\u524d\uff0c\u6392\u6c14\u52a8\u80fd\u968f\u7740\u538b\u529b\u548c\u6e29\u5ea6\u7684\u589e\u52a0\u800c\u589e\u52a0\u3002\u8fd9\u4e24\u8005\u901a\u8fc7\u63a8\u8fdb\u6548\u7387\u76f8\u5173\uff0c\u63a8\u8fdb\u6548\u7387\u662f\u8861\u91cf\u5728\u6d41\u4f53\u4e2d\u901a\u8fc7\u589e\u52a0\u6d41\u4f53\u901f\u5ea6\uff08\u5373\u52a8\u91cf\uff09\u6765\u4ea7\u751f\u529b\uff08\u5373\u63a8\u529b\uff09\u800c\u6d6a\u8d39\u7684\u80fd\u91cf\u7684\u5ea6\u91cf\u3002<\/li>\n<\/ul>\n\n\n\n<p>Dry<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>engine ratings\/ throttle lever positions below afterburning selection<br>\u53c2\u8003\u8bd1\u6587\uff1a\u53d1\u52a8\u673a\u989d\u5b9a\u503c\/\u6cb9\u95e8\u6746\u4f4d\u7f6e\u4ee5\u4e0b\u52a0\u529b\u71c3\u70e7\u9009\u62e9<\/li>\n<\/ul>\n\n\n\n<p>EGT<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>exhaust gas temperature<br>\u53c2\u8003\u8bd1\u6587\uff1a\u5e9f\u6c14\u6e29\u5ea6<\/li>\n<\/ul>\n\n\n\n<p>EPR<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>engine pressure ratio<br>\u53c2\u8003\u8bd1\u6587\uff1a\u53d1\u52a8\u673a\u538b\u529b\u6bd4<\/li>\n<\/ul>\n\n\n\n<p>Fan \u98ce\u6247<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>turbofan LP compressor<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6da1\u6247\u4f4e\u538b\u538b\u7f29\u673a<\/li>\n<\/ul>\n\n\n\n<p>Fanjet \u6da1\u6247\u98de\u673a<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>turbofan or aircraft powered by turbofan (colloquial)<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/659034614\/edit#cite_note-65\">[65]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u6da1\u8f6e\u98ce\u6247\u6216\u7531\u6da1\u8f6e\u98ce\u6247\u9a71\u52a8\u7684\u98de\u673a(\u53e3\u8bed)[65]<\/li>\n<\/ul>\n\n\n\n<p>Fan pressure ratio \u98ce\u673a\u538b\u529b\u6bd4<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>fan outlet total pressure\/fan inlet total pressure<br>\u53c2\u8003\u8bd1\u6587\uff1a\u98ce\u673a\u51fa\u53e3\u603b\u538b\u529b\/\u98ce\u673a\u8fdb\u53e3\u603b\u538b\u529b<\/li>\n<\/ul>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Flex_temp\" target=\"_blank\" rel=\"noreferrer noopener\">Flex temp<\/a> \u7075\u6d3b\u6e29\u5ea6<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>At reduced take-off weights commercial aircraft can use reduced thrust which increases engine life and reduces maintenance costs. Flex temperature is a higher than actual outside air temperature (OAT) which is input to the engine monitoring computer to achieve the required reduced thrust (also known as &#8220;assumed temperature thrust reduction&#8221;).<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/659034614\/edit#cite_note-66\">[66]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u5728\u51cf\u5c0f\u7684\u8d77\u98de\u91cd\u91cf\u4e0b\uff0c\u5546\u7528\u98de\u673a\u53ef\u4ee5\u4f7f\u7528\u51cf\u5c11\u7684\u63a8\u529b\uff0c\u4ece\u800c\u589e\u52a0\u53d1\u52a8\u673a\u5bff\u547d\u5e76\u964d\u4f4e\u7ef4\u62a4\u6210\u672c\u3002\u7075\u6d3b\u6e29\u5ea6\u662f\u9ad8\u4e8e\u5b9e\u9645\u5916\u754c\u6e29\u5ea6\uff08OAT\uff09\u7684\u6e29\u5ea6\uff0c\u8f93\u5165\u5230\u53d1\u52a8\u673a\u76d1\u63a7\u8ba1\u7b97\u673a\u4e2d\uff0c\u4ee5\u5b9e\u73b0\u6240\u9700\u7684\u51cf\u5c11\u63a8\u529b\uff08\u4e5f\u79f0\u4e3a\u201c\u5047\u5b9a\u6e29\u5ea6\u63a8\u529b\u51cf\u5c11\u201d\uff09\u3002<\/li>\n<\/ul>\n\n\n\n<p>Gas generator \u6c14\u4f53\u53d1\u751f\u5668<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>that part of the engine core which provides the hot, high pressure gas for fan-driving turbines (turbofan), for propelling nozzles (turbojet), for propeller- and rotor-driving turbines (turboprop and turboshaft), for industrial and marine power turbines<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/659034614\/edit#cite_note-67\">[67]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u53d1\u52a8\u673a\u6838\u5fc3\u7684\u8fd9\u90e8\u5206\u63d0\u4f9b\u4e86\u71c3\u6599\u71c3\u70e7\u4ea7\u751f\u7684\u9ad8\u6e29\u9ad8\u538b\u6c14\u4f53\uff0c\u7528\u4e8e\u9a71\u52a8\u98ce\u6247\u6da1\u8f6e\uff08\u6da1\u6247\u53d1\u52a8\u673a\uff09\uff0c\u7528\u4e8e\u63a8\u8fdb\u55b7\u5634\uff08\u55b7\u6c14\u5f0f\u53d1\u52a8\u673a\uff09\uff0c\u7528\u4e8e\u9a71\u52a8\u87ba\u65cb\u6868\u548c\u65cb\u7ffc\u7684\u6da1\u8f6e\uff08\u6da1\u6868\u53d1\u52a8\u673a\u548c\u6da1\u8f74\u53d1\u52a8\u673a\uff09\uff0c\u4ee5\u53ca\u5de5\u4e1a\u548c\u8239\u8236\u52a8\u529b\u6da1\u8f6e\u3002<\/li>\n<\/ul>\n\n\n\n<p>HP \u9ad8\u538b<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>high-pressure \u9ad8\u538b<\/li>\n<\/ul>\n\n\n\n<p>Intake ram drag \u8fdb\u6c14\u95f8\u677f\u963b\u529b<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>Loss in momentum of engine stream tube from freestream to intake entrance, ie amount of energy imparted to air required to accelerate air from a stationary atmosphere to aircraft speed.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u53d1\u52a8\u673a\u6d41\u7ba1\u4ece\u81ea\u7531\u6d41\u5230\u8fdb\u6c14\u53e3\u7684\u52a8\u91cf\u635f\u5931\uff0c\u5373\u5c06\u7a7a\u6c14\u4ece\u9759\u6b62\u5927\u6c14\u52a0\u901f\u5230\u98de\u673a\u901f\u5ea6\u6240\u9700\u7684\u4f20\u9012\u7ed9\u7a7a\u6c14\u7684\u80fd\u91cf\u3002<\/li>\n<\/ul>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/IEPR\" target=\"_blank\" rel=\"noreferrer noopener\">IEPR<\/a><\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>integrated engine pressure ratio<br>\u53c2\u8003\u8bd1\u6587\uff1a\u53d1\u52a8\u673a\u7efc\u5408\u538b\u529b\u6bd4<\/li>\n<\/ul>\n\n\n\n<p>IP \u4e2d\u538b<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>intermediate pressure<br>\u53c2\u8003\u8bd1\u6587\uff1a\u4e2d\u538b<\/li>\n<\/ul>\n\n\n\n<p>LP \u4f4e\u538b<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>low-pressure<br>\u53c2\u8003\u8bd1\u6587\uff1a\u4f4e\u538b<\/li>\n<\/ul>\n\n\n\n<p>Net thrust \u51c0\u63a8\u529b<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>nozzle thrust in stationary air (gross thrust) \u2013 engine stream tube ram drag (loss in momentum from freestream to intake entrance, ie amount of energy imparted to air required to accelerate air from a stationary atmosphere to aircraft speed). This is the thrust acting on the airframe.<br>\u53c2\u8003\u8bd1\u6587\uff1a\u63a8\u8fdb\u55b7\u5634\u5728\u9759\u6b62\u7a7a\u6c14\u4e2d\u7684\u63a8\u529b\uff08\u603b\u63a8\u529b\uff09- \u53d1\u52a8\u673a\u6c14\u6d41\u7ba1\u7684\u6c14\u538b\u963b\u529b\uff08\u4ece\u81ea\u7531\u6d41\u5230\u8fdb\u6c14\u53e3\u7684\u52a8\u91cf\u635f\u5931\uff0c\u5373\u4e3a\u5c06\u7a7a\u6c14\u4ece\u9759\u6b62\u5927\u6c14\u52a0\u901f\u5230\u98de\u673a\u901f\u5ea6\u6240\u9700\u7684\u80fd\u91cf\u91cf\uff09\u3002\u8fd9\u662f\u4f5c\u7528\u5728\u673a\u8eab\u4e0a\u7684\u63a8\u529b\u3002<\/li>\n<\/ul>\n\n\n\n<p>Overall pressure ratio \u603b\u538b\u529b\u6bd4<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>combustor inlet total pressure\/intake delivery total pressure<br>\u53c2\u8003\u8bd1\u6587\uff1a\u71c3\u70e7\u5ba4\u8fdb\u6c14\u603b\u538b\u529b\/\u8fdb\u6c14\u8f93\u9001\u603b\u538b\u529b<\/li>\n<\/ul>\n\n\n\n<p>Overall efficiency \u603b\u4f53\u6548\u7387<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>thermal efficiency * propulsive efficiency<br>\u53c2\u8003\u8bd1\u6587\uff1a\u70ed\u6548\u7387*\u63a8\u8fdb\u6548\u7387<\/li>\n<\/ul>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Propulsive_efficiency\" target=\"_blank\" rel=\"noreferrer noopener\">Propulsive efficiency<\/a> \u63a8\u8fdb\u6548\u7387<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>propulsive power\/rate of production of propulsive kinetic energy (maximum propulsive efficiency occurs when jet velocity equals flight velocity, which implies zero net thrust!)<br>\u53c2\u8003\u8bd1\u6587\uff1a\u63a8\u8fdb\u529f\u7387\/\u63a8\u8fdb\u52a8\u80fd\u7684\u4ea7\u751f\u7387(\u6700\u5927\u63a8\u8fdb\u6548\u7387\u53d1\u751f\u5728\u55b7\u5c04\u901f\u5ea6\u7b49\u4e8e\u98de\u884c\u901f\u5ea6\u65f6\uff0c\u8fd9\u610f\u5473\u7740\u51c0\u63a8\u529b\u4e3a\u96f6!)<\/li>\n<\/ul>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Thrust_specific_fuel_consumption\" target=\"_blank\" rel=\"noreferrer noopener\">Specific fuel consumption<\/a> (SFC) \u6bd4\u71c3\u6cb9\u6d88\u8017\u91cf(SFC)<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>total fuel flow\/net thrust (proportional to flight velocity\/overall thermal efficiency)<br>\u53c2\u8003\u8bd1\u6587\uff1a\u603b\u71c3\u6cb9\u6d41\u91cf\/\u51c0\u63a8\u529b(\u4e0e\u98de\u884c\u901f\u5ea6\/\u603b\u70ed\u6548\u7387\u6210\u6b63\u6bd4)<\/li>\n<\/ul>\n\n\n\n<p>Spooling up \u53d1\u52a8\u673a\u5feb\u901f\u589e\u52a0\u8f6c\u901f\u76f4\u5230\u8fbe\u5230\u6b63\u5e38\u8fd0\u884c\u901f\u5ea6\u7684\u8fc7\u7a0b<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>increase in RPM (colloquial)<br>\u53c2\u8003\u8bd1\u6587\uff1a\u8f6c\u901f\u589e\u52a0(\u53e3\u8bed\u5316)<\/li>\n<\/ul>\n\n\n\n<p>Stage loading<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>For a turbine, the purpose of which is to produce power, the loading is an indicator of power developed per lb\/sec of gas (specific power). A turbine stage turns the gas from an axial direction and speeds it up (in the nozzle guide vanes) to turn the rotor most effectively ( rotor blades must produce high lift), the proviso being that this is done efficiently, ie with acceptable losses.<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/659034614\/edit#cite_note-68\">[68]<\/a> For a compressor stage, the purpose of which is to produce a pressure rise, a diffusion process is used. How much diffusion may be allowed ( and pressure rise obtained) before unacceptable flow separation occurs (ie losses) may be regarded as a loading limit.<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/659034614\/edit#cite_note-69\">[69]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u5bf9\u4e8e\u7528\u4e8e\u4ea7\u751f\u52a8\u529b\u7684\u6da1\u8f6e\u673a\u800c\u8a00\uff0c\u8f7d\u8377\u662f\u6307\u6bcf\u78c5\/\u79d2\u6c14\u4f53\u6240\u4ea7\u751f\u7684\u529f\u7387\uff08\u6bd4\u529f\u7387\uff09\u7684\u6307\u6807\u3002\u6da1\u8f6e\u7ea7\u522b\u5c06\u6c14\u4f53\u4ece\u8f74\u5411\u65b9\u5411\u8f6c\u5411\uff0c\u5e76\u5728\u5bfc\u53f6\u4e2d\u52a0\u901f\u6c14\u4f53\u4ee5\u6709\u6548\u5730\u8f6c\u52a8\u8f6c\u5b50\uff08\u8f6c\u5b50\u53f6\u7247\u5fc5\u987b\u4ea7\u751f\u9ad8\u5347\u529b\uff09\uff0c\u524d\u63d0\u662f\u8981\u4ee5\u53ef\u63a5\u53d7\u7684\u635f\u5931\u6548\u7387\u5b8c\u6210\u8fd9\u4e00\u8fc7\u7a0b\u3002\u5bf9\u4e8e\u7528\u4e8e\u4ea7\u751f\u538b\u529b\u5347\u9ad8\u7684\u538b\u6c14\u673a\u7ea7\u522b\u800c\u8a00\uff0c\u4f7f\u7528\u6269\u6563\u8fc7\u7a0b\u3002\u5728\u51fa\u73b0\u4e0d\u53ef\u63a5\u53d7\u7684\u6d41\u52a8\u5206\u79bb\uff08\u5373\u635f\u5931\uff09\u4e4b\u524d\uff0c\u53ef\u4ee5\u5141\u8bb8\u591a\u5c11\u6269\u6563\uff08\u5e76\u83b7\u5f97\u538b\u529b\u5347\u9ad8\uff09\u53ef\u4ee5\u88ab\u89c6\u4e3a\u8d1f\u8f7d\u9650\u5236\u3002<\/li>\n<\/ul>\n\n\n\n<p>Static pressure \u9759\u538b<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>pressure of the fluid which is associated not with its motion but with its state<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/659034614\/edit#cite_note-70\">[70]<\/a> or, alternatively, pressure due to the random motion of the fluid molecules that would be felt or measured if moving with the flow<a href=\"https:\/\/zhuanlan.zhihu.com\/p\/659034614\/edit#cite_note-71\">[71]<\/a><br>\u53c2\u8003\u8bd1\u6587\uff1a\u4e0e\u6d41\u4f53\u8fd0\u52a8\u800c\u975e\u72b6\u6001\u76f8\u5173\u7684\u6d41\u4f53\u538b\u529b[70]\uff0c\u6216\u8005\uff0c\u4e5f\u53ef\u4ee5\u662f\u6d41\u4f53\u5206\u5b50\u968f\u673a\u8fd0\u52a8\u4ea7\u751f\u7684\u538b\u529b\uff0c\u8fd9\u79cd\u538b\u529b\u968f\u7740\u6d41\u4f53\u8fd0\u52a8\u800c\u88ab\u611f\u77e5\u6216\u6d4b\u91cf[71]<\/li>\n<\/ul>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Specific_thrust\" target=\"_blank\" rel=\"noreferrer noopener\">Specific thrust<\/a> \u7279\u5b9a\u7684\u63a8\u529b<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>net thrust\/intake airflow<br>\u53c2\u8003\u8bd1\u6587\uff1a\u51c0\u63a8\u529b\/\u8fdb\u6c14\u6c14\u6d41<\/li>\n<\/ul>\n\n\n\n<p><a href=\"https:\/\/link.zhihu.com\/?target=https%3A\/\/en.wikipedia.org\/wiki\/Thermal_efficiency\" target=\"_blank\" rel=\"noreferrer noopener\">Thermal efficiency<\/a> \u70ed\u6548\u7387<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>rate of production of propulsive kinetic energy\/fuel power<br>\u53c2\u8003\u8bd1\u6587\uff1a\u63a8\u8fdb\u52a8\u80fd\/\u71c3\u6599\u52a8\u529b\u7684\u4ea7\u51fa\u7387<\/li>\n<\/ul>\n\n\n\n<p>Total fuel flow \u71c3\u6599\u603b\u6d41\u91cf<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>combustor (plus any afterburner) fuel flow rate (e.g., lb\/s or g\/s)<br>\u53c2\u8003\u8bd1\u6587\uff1a\u71c3\u70e7\u5ba4(\u52a0\u4e0a\u4efb\u4f55\u52a0\u529b\u71c3\u70e7\u5ba4)\u71c3\u6599\u6d41\u91cf(\u4f8b\u5982\uff0c\u78c5\/\u79d2\u6216\u514b\/\u79d2)<\/li>\n<\/ul>\n\n\n\n<p>Total pressure \u603b\u538b\u5f3a<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>static pressure <strong>plus<\/strong> kinetic energy term<br>\u53c2\u8003\u8bd1\u6587\uff1a\u9759\u538b\u52a0\u4e0a\u52a8\u80fd\u9879<\/li>\n<\/ul>\n\n\n\n<p>Turbine rotor inlet temperature \u6da1\u8f6e\u8f6c\u5b50\u5165\u53e3\u6e29\u5ea6<\/p>\n\n\n\n<ul class=\"wp-block-list\">\n<li>maximum cycle temperature, ie temperature at which work transfer takes place<br>\u53c2\u8003\u8bd1\u6587\uff1a\u6700\u9ad8\u5faa\u73af\u6e29\u5ea6(\u505a\u529f\u4f20\u9012\u65f6\u7684\u6e29\u5ea6)<\/li>\n<\/ul>\n\n\n\n<hr class=\"wp-block-separator has-alpha-channel-opacity\"\/>\n\n\n\n<h2 class=\"wp-block-heading\">\u53c2\u89c1\u3001\u53c2\u8003\u6587\u732e\u3001\u5916\u90e8\u94fe\u63a5<\/h2>\n\n\n\n<p><a href=\"https:\/\/www.cathayvista.net\/zh\/ref-turbofan\" data-type=\"link\" data-id=\"https:\/\/www.cathayvista.net\/zh\/ref-turbofan\">\u8bf7\u70b9\u51fb\u8fd9\u91cc\u8bbf\u95ee\uff08\u8fbd\u89c2\u7f51\u7ad9\uff09<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p>\u4e2d\u6587\u8bcd\u6761\u539f\u6587\u94fe\u63a5\uff08\u65e0\u6cd5\u4ece\u4e2d\u56fd\u5185\u5730\u8bbf\u95ee\uff09\uff1a\u70b9\u51fb [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"closed","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":[],"categories":[48,21],"tags":[11,101,12],"class_list":["post-1399","post","type-post","status-publish","format-standard","hentry","category-fulltext","category-aviation","tag-11","tag-101","tag-12"],"_links":{"self":[{"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/posts\/1399","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/comments?post=1399"}],"version-history":[{"count":0,"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/posts\/1399\/revisions"}],"wp:attachment":[{"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/media?parent=1399"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/categories?post=1399"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/cathayvista.top\/index.php\/wp-json\/wp\/v2\/tags?post=1399"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}