TAPS燃烧室燃油喷嘴设计特点分析  

Analysis of Fuel Nozzle Design Characteristics for TAPS Combustor

作　　者：李杰[1] 

机构地区：[1]西安航空发动机(集团)有限公司,西安710021

出　　处：《航空发动机》2010年第5期59-61,55,共4页Aeroengine

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。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.

关 键 词：TAPS燃烧室 燃油喷嘴 结构设计 

分 类 号：V263.6[航空宇航科学与技术—航空宇航制造工程]