F135-PW-600发动机升力系统与整机匹配性能研究  

The matched working performance of the core engine with the lifting system of F135-PW-600

作　　者：姜楠 杨磊 杨大军 

机构地区：[1]中国航空发动机集团有限公司,北京100097 [2]中国航发四川燃气涡轮研究院,成都610500

出　　处：《燃气涡轮试验与研究》2017年第4期7-10,50,共5页Gas Turbine Experiment and Research

基　　金：航空科学基金(2014ZB24008)

摘　　要：对F135-PW-600发动机的升力系统与发动机主机匹配工作性能进行了研究。针对F135-PW-600发动机的工作特点,从分析升力系统工作原理开始,分别分析了升力风扇所需功率、滚转喷管引气流量、尾喷管喉道面积调节和低压涡轮导向器面积调节对整机匹配性能的影响,获得了发动机的基本调节原理。之后根据相关文献中的发动机数据,验算了发动机在常规模式、升力模式和超声巡航状态下的性能,对分析结果进行了验证。为F135-PW-600发动机性能和控制规律分析提供了一种研究方法。The matched working performance of the core engine with the lifting system of F135-PW-600 was studied.Beginning with the analysis of the working principles of the lifting system,influences of required power for lift-fan,the bleed air of roll-nozzle,the adaptation of nozzle throat area and the adaptation of low pressure turbine nozzle area on the matched working performance were analyzed,and then the basic principle was obtained.Through the data from the related references,the research findings were confirmed by checking the engine performance in conventional,lifting and supersonic cruise modes.It provides a research method for the performance and control law analysis of F135-PW-600.

关 键 词：航空发动机 性能仿真 升力风扇 滚转喷管 升力模式 F-35B F135-PW-600 

分 类 号：V231.12[航空宇航科学与技术—航空宇航推进理论与工程]