| TAPS燃烧室燃油喷嘴设计特点分析 |
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| 引用本文： | 李杰.TAPS燃烧室燃油喷嘴设计特点分析[J].航空发动机,2010,36(5):59-61,55. |
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| 作者姓名： | 李杰 |
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| 作者单位： | 西安航空发动机（集团）有限公司,西安710021 |
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| 摘 要： | 创新的、清洁燃烧的TAPS燃烧室由美国GE公司研发,在CFM56-7B发动机上得到验证后,成功地应用到新一代商用涡扇发动机GEnx上。对TAPS燃烧室做了简要介绍,对其燃油喷嘴的结构特点进行了概括性分析,并提出了启迪与思考。
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| 关 键 词： | TAPS燃烧室 燃油喷嘴 结构设计 |
Analysis of Fuel Nozzle Design Characteristics for TAPS Combustor |
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| Authors: | LI Jie |
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| Institution: | LI Jie(Xi＇an Aeroengine(Group) Ltd.,Xi＇an 710021,China) |
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| Abstract: | An innovative,and clean-burning TAPS combustor was developed by the General Electric Corporation.It was demonstrated in the CFM56-7B engine,and was applied to the new generation commercial turbofan engine GEnx successfully.The TAPS combustor was introduced briefly,its fuel nozzle structure characteristics were analyzed generally,and the enlightment and thought were provided. |
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| Keywords: | TAPS Combustor Fuel Nozzle structure design |
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