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大型民用飞机辅助动力装置性能仿真
引用本文:赵运生,胡骏,吴铁鹰,陈娟娟.大型民用飞机辅助动力装置性能仿真[J].航空动力学报,2011,26(7):1590-1598.
作者姓名:赵运生  胡骏  吴铁鹰  陈娟娟
作者单位:南京航空航天大学能源与动力学院,南京,210016
摘    要:分析典型辅助动力装置(APU)系统的结构和气动热力学过程,采用面向对象的数值仿真方法,利用C++程序建立了APU各部件类;针对某150座级民用飞机选用的APU型号,将部件类组成具体的APU整机数学模型.依照此型APU的运行工况,完成了气动热力计算和非设计点性能计算,得到其设计点性能参数及用于飞机环境控制和主发起动模式下...

关 键 词:辅助动力装置(APU)  非设计点性能  数值仿真  面向对象  稳态特性
收稿时间:6/8/2010 12:00:00 AM
修稿时间:2010/11/2 0:00:00

Performance simulation of large civil aircraft auxiliary power unit
ZHAO Yun-sheng,HU Jun,WU Tie-ying and CHEN Juan-juan.Performance simulation of large civil aircraft auxiliary power unit[J].Journal of Aerospace Power,2011,26(7):1590-1598.
Authors:ZHAO Yun-sheng  HU Jun  WU Tie-ying and CHEN Juan-juan
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
Abstract:By analyzing the structure and aerothermodynamics processes of the typical auxiliary power unit (APU),this paper used object-oriented technology and C++ program to design the classes of APU components.In order to simulate a 150-class civil aircraft APU model,instances of the component classes were assembled.According to the APU operating conditions,the thermodynamic and off-design performance calculations were completed,the design state performance and operating envelope about aircraft environment control and main engine start models,as well as altitude-speed,temperature and load characteristics,were obtained accordingly.
Keywords:auxiliary power unit(APU)  off-design performance  numerical simulation  object-oriented  steady-state characteristic
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