• DocumentCode
    2929157
  • Title

    Simulation of Aircraft Fuel Thermal Management System Based on Simulink

  • Author

    Liu Shuang ; Zhuang Damin ; Wanyan Xiaoru

  • Author_Institution
    Sch. of Aeronaut. Sci. & Eng., BeiHang Univ., Beijing, China
  • fYear
    2011
  • fDate
    25-28 March 2011
  • Firstpage
    1
  • Lastpage
    4
  • Abstract
    Aiming at the aircraft fuel system which adopts the technology of vapor cycle cooling system, and uses the fuel as a kind of effective cold source of condensers and other heat exchangers, this paper established the mathematical models of the fuel system and major components. On the basis of Simulink software platform, the simulation module of fuel system was established by developing the S-functions of the major components and the user-defined module library. According to the simulation module, the flow, temperature, pressure, and the import and export parameters of all the major components could be obtained in different given flight situations. The simulation module could also be used in making prediction and supervision of the thermal management and the parameters of each node of the aircraft fuel system, offering some reference for aircraft fuel system design which adopts the technology of vapor cycle cooling.
  • Keywords
    aircraft; fuel systems; heat exchangers; mechanical engineering computing; thermal management (packaging); Simulink software; aircraft fuel thermal management system; condensers; heat exchangers; simulation module; vapor cycle cooling; Aerospace electronics; Aircraft; Atmospheric modeling; Fuel storage; Fuels; Heating; Mathematical model;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Power and Energy Engineering Conference (APPEEC), 2011 Asia-Pacific
  • Conference_Location
    Wuhan
  • ISSN
    2157-4839
  • Print_ISBN
    978-1-4244-6253-7
  • Type

    conf

  • DOI
    10.1109/APPEEC.2011.5748500
  • Filename
    5748500