Volume 26 Issue 9
Sep.  2011
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CHANG Bo-bo, SU San-mai, LIU Tie-geng, LIU Mei-feng. Model and numerical simulation of auxiliary power unit[J]. Journal of Aerospace Power, 2011, 26(9): 2122-2127.
Citation: CHANG Bo-bo, SU San-mai, LIU Tie-geng, LIU Mei-feng. Model and numerical simulation of auxiliary power unit[J]. Journal of Aerospace Power, 2011, 26(9): 2122-2127.
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Model and numerical simulation of auxiliary power unit

  • 1.

    School of Power and Energy, Northwestern Polytechnical University, Xi'an 71007

  • 2.

    China Aviation Powerplant Research Institute, Aviation Industry Corporation of China, Zhuzhou Hunan 410003, China

  • Received Date: 2010-09-25
  • Rev Recd Date: 2011-01-18
  • Publish Date: 2011-09-28
    Abstract
  • In order to supporting auxiliary power unit (APU) design,the widely used APU with load compressor in structure was discussed and modeled.Firstly,the structural characteristics and regulation law are introduced and then how the load compressor works on APU was analyzed.Finally the mathematic model of APU was established based on components.Take a kind of APU as the object for numerical simulation and then compare with the actual test data.The results show that the dynamic simulation error is less than 5%.The mathematic model of APU is suitable for engineering usage.

     

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    • References(12)
  • [1]
    Rodger C,Johnson D C.APU fuel efficiency and afford ability for commercial aircraft .AIAA 1987- 1907,1987.
    [2]
    Cristian A.A novel start system for an aircraft auxiliary power unit //Energy Conversion Engineering Conference and Exhibit.Las Vegas,NV,USA:IECEC 2000,1:7-11.
    [3]
    Dimitry G,Kevin D ,Dinkar M.Model-based diagnostics for an aircraft auxiliary power unit //IEEE Conference on Control Applications.Glasgow:IEEE,2002:215-219.
    [4]
    Rodgers C.Performance of single shaft load compressor auxiliary power units .AIAA-1983-1159,1983.
    [5]
    Rodgers C.Auxiliary power units for current and future air craft .SAE Technical Paper,912059,1991.
    [6]
    Rodgers C.Secondary power system for advanced fighter . AIAA 1985-1280,1985.
    [7]
    金中平.辅助动力装置及其标准发展综述[J].航空标准化与质量,1998(4):19-22. JIN Zhongping.The auxiliary power uints and its development[J].Aeronautic Standardization & Quality,1998(4):19-22.(in Chinese)
    [8]
    《航空发动机设计手册》总编委会.航空发动机设计手册(第十四册)[M].北京:航空工业出版社,2000.
    [9]
    宋静波.波音737飞机动力装置:CFM56-3 & APU[M].广州:中山大学出版社,2008.
    [10]
    廉小纯.航空燃气轮机原理(上、下册)[M].北京:国防工业出版社,2001.
    [11]
    骆广琦,桑增产,王如根,等.航空燃气涡轮发动机数值仿真[M].北京:国防工业出版社,2007.
    [12]
    樊思齐.航空发动机控制(下册)[M].西安:西北工业大学出版社,2008.
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