• DocumentCode
    3049349
  • Title

    Thermodynamic characteristics analysis of a high temperature fuel flow-rate control valve

  • Author

    Song, Kai ; Li, Songjing

  • Author_Institution
    Fluid Control & Autom. Dept., Harbin Inst. of Technol., Harbin, China
  • fYear
    2010
  • fDate
    8-10 June 2010
  • Firstpage
    1333
  • Lastpage
    1338
  • Abstract
    High temperature flow-rate control valve is a key component to control the flow rate of fuel supply for aerospace engines. A high temperature fuel flow-rate control valve, pilot-controlled by a high pressure pneumatic system, is developed in this paper. The construction and working principle of the valve are introduced. The thermodynamic mathematical models of the valve are built and the thermodynamic characteristics are simulated by using the 3D finite element analysis method under the condition that the material of the valve elements is a high temperature alloy. Then both of the steady-state and transient temperature field distribution inside the spool and valve body are studied. Also the thermal stress and thermal strain of the valve are calculated.
  • Keywords
    aerospace engines; finite element analysis; flow control; fuel systems; pneumatic systems; pressure control; temperature control; temperature distribution; thermal stresses; thermodynamics; valves; 3D finite element analysis; aerospace engine; fuel supply; high pressure pneumatic system; high temperature alloy; high temperature fuel flow-rate control valve; pilot-control; spool; steady-state temperature field distribution; thermal strain; thermal stress; thermodynamic characteristics analysis; thermodynamic mathematical model; transient temperature field distribution; valve body; Finite element methods; Heat transfer; Heating; Strain; Stress; Thermal stresses; Valves; finite element analysis; flow-rate control valve; high temperature fuel; thermal strain;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4244-6043-4
  • Electronic_ISBN
    978-1-4244-7505-6
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2010.5633602
  • Filename
    5633602