Volume 23 Issue 2
Feb.  2008
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HUANG Guo-ping, LIANG De-wang, HE Zhi-qiang. Comparison of technical characteristics of APU and micro turbine engines for large aircraft[J]. Journal of Aerospace Power, 2008, 23(2): 383-388.
Citation: HUANG Guo-ping, LIANG De-wang, HE Zhi-qiang. Comparison of technical characteristics of APU and micro turbine engines for large aircraft[J]. Journal of Aerospace Power, 2008, 23(2): 383-388.
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Comparison of technical characteristics of APU and micro turbine engines for large aircraft

  • 1.

    The Institute of Micro-Engine, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

  • 2.

    Grand China Express Limited company, Tianjin 300300, China

  • Received Date: 2007-07-17
  • Rev Recd Date: 2007-12-06
  • Publish Date: 2008-02-28
    Abstract
  • The overall design and technical characteristics of micro turbine engines(MTE) and auxiliary power unit(APU) were analyzed comparatively,and their similarities and differences were summarized.The results show that: the output powers of MTEand APUare equivalent.Moreover,the technologies of such two power systems are similar in terms of the designs or manufacturing of engines and their main components.MTEhas higher performance index,and APUpresents higher reliability, economic efficiency and longer service life through conservative design.So,a technical approach to develop Chinese APUbased on the technology of MTEhas been proposed.

     

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    • References(6)
  • [1]
    黄国平,温泉,李博,等.微型涡轮发动机顶层设计研究[J].航空动力学报,2003,18(6):832-838.HUANG Guoping,WEN Quan,LI Bo,et al.Top level design of micro turbine jet engine[J].Journal of Aerospace Power,2003,18(6):832-838.
    [2]
    施荣,陈兢.低成本精确打击武器系统[J].国防科技,2004,20(10):6-10.
    [3]
    Yoshida H,Matsunuma T,Norihiko IKI,et al.Micro gas turbine with ceramic rotor[c]//Vienna,Austria:Proceedings of ASME Turbo Expo,GT2004-53493,2004.
    [4]
    黄治国,单鹏,王延荣.微型涡喷发动机结构设计研究[J].北京航空航天学报,2004,30(3):206-209.HUANG Zhiguo,SHAN Peng,WANG Yanrong.Structural design study of a micro-turbojet engine[J].Journal of Beijing University of Aeronautics and Astronautics,2004,30(3):206-209.
    [5]
    熊庆荣,雷雨冰,黄国平,等.厘米级微型蒸发管式燃烧室性能实验研究[J].航空动力学报,2007.22(5):733-738.XIONG Qingrong,LEI Yubing,HUANG Guoping,et al.Experimental research on a centimeter-scale micro combustor with vaporizing tube[J].Journal of Aerospace Power,2007,22(5):733-738.
    [6]
    夏晨,黄国平,梁德旺.微型斜流式涡轮数值分析与设计[C]//中国航空学会第六届动力年会论文集.南京:中国航空学会动力分会,2006.
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