首页 | 本学科首页   官方微博 | 高级检索  
     检索      

带涡轮级间次燃烧室混排涡扇发动机的超声速性能研究
引用本文:屠秋野,孙泽晖,牟锦辉,蔡元虎.带涡轮级间次燃烧室混排涡扇发动机的超声速性能研究[J].航空计算技术,2010,40(4):14-17.
作者姓名:屠秋野  孙泽晖  牟锦辉  蔡元虎
作者单位:1. 西北工业大学,动力与能源学院,陕西,西安,710072
2. 中国飞行试验研究院,陕西,西安,710089
基金项目:教育部高校博士点新教师基金资助项目,航空科学基金资助项目 
摘    要:为了满足超声速客机长时间巡航飞行的推力需求,研究了混排ITB(inter-stage turbine burn-er)涡扇发动机的性能参数随高、低压转子转速的变化关系,并采用调节高、低压转子转速作为双变量控制规律,获得了混排ITB涡扇发动机主要的性能参数随转子转速的变化关系。采用双转速控制的组合调节方案,混排ITB发动机在超声速飞行条件下实现了宽广而且连续的推力输出。

关 键 词:涡轮级间次燃烧室  超声速性能  双转速控制

Super-sonic Performance Research on Mixed Exhaust Turbofan Engine with Inter-stage Turbine Burner
TU Qiu-ye,SUN Ze-hui,MOU Jin-hui,CAI Yuan-hu.Super-sonic Performance Research on Mixed Exhaust Turbofan Engine with Inter-stage Turbine Burner[J].Aeronautical Computer Technique,2010,40(4):14-17.
Authors:TU Qiu-ye  SUN Ze-hui  MOU Jin-hui  CAI Yuan-hu
Institution:1.Northwestern Polytechnical University,Xi′an 710072,China;2.China Flying Test Academy,Xi′an 710089,China)
Abstract:To meet the thrust requirment as super sonic airplane cruising for long time,this study investigated the relations between performance parameters and rotor speeds of mixed exhaust turbofan engine with inter-stage turbine burner,adopted regulating high and low rotor speeds as control law of two variables,and obtained the relations of main performance parameters and rotor speeds.With the combined solution of dual-rotor speed control,the ITB engine realized the extensive and consecutive thrust outputs during s...
Keywords:inter-stage turbine burner  super sonic performance  dual-rotor speed control  
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号