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高推重比航空发动机调节规律分析
引用本文:朱之丽,李东.高推重比航空发动机调节规律分析[J].航空动力学报,1998,13(2):153-156,219.
作者姓名:朱之丽  李东
作者单位:北京航空航天大学
摘    要:针对先进高推重比涡扇发动机采用的调节规律进行了研究。通过对采用不同调节规律下的混合加力涡扇发动机非安装性能进行对比,分析了高推重比发动机采用的调节规律的优越性。

关 键 词:涡轮风扇发动机  调节  分析  性能
收稿时间:5/1/1997 12:00:00 AM
修稿时间:9/1/1997 12:00:00 AM

ANALYSIS OF CONTROL SCHEDULES FOR HIGH THRUST-WEIGHT RATIO TURBOFAN ENGINE
Zhu Zhili and Li Dong.ANALYSIS OF CONTROL SCHEDULES FOR HIGH THRUST-WEIGHT RATIO TURBOFAN ENGINE[J].Journal of Aerospace Power,1998,13(2):153-156,219.
Authors:Zhu Zhili and Li Dong
Institution:4th Dept.Beijing University of Aeronautics and Astronautics,Beijing 100083;4th Dept.Beijing University of Aeronautics and Astronautics,Beijing 100083
Abstract:It is important to design a suitable control schedule for aircraft engine in order to exploit its full performance potentiality and to enhance its reliability.Comparison and analysis of uninstalled performance of engine with different control schedules are carried out in this paper.The result indicates that the control schedules for the modern high thrust-weight ratio turbofan are superior significantly to the traditional control schedules of engine in enhancement performance at high speed and improvement of the working conditions of the hot section components.
Keywords:Turbofan engines  Control  Analysis  Performance
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