Volume 27 Issue 3
Mar.  2012
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Article Navigation >  Journal of Aerospace Power  > 2012  >  27(3): 578-587
MAO Yan-hui, LIU Cun-xi, LIU Fu-qiang, FANG Ai-bing, XU Gang. Application of inter-stage turbine burner on aero-engine[J]. Journal of Aerospace Power, 2012, 27(3): 578-587.
Citation: MAO Yan-hui, LIU Cun-xi, LIU Fu-qiang, FANG Ai-bing, XU Gang. Application of inter-stage turbine burner on aero-engine[J]. Journal of Aerospace Power, 2012, 27(3): 578-587.
shu

Application of inter-stage turbine burner on aero-engine

  • 1.

    Key Laboratory of Light-duty Gas-turbine, Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China

  • 2.

    Graduate University of Chinese Academy of Sciences, Beijing 100190, China

  • Received Date: 2011-04-07
  • Rev Recd Date: 2011-09-06
  • Publish Date: 2012-03-28
    Abstract
  • The engine with inter-stage turbine burner was computed in non-ideal cycle with F100-PW229 parameter.The differences of performance and thermal efficiency between inter-stage turbine burner and afterburner were compared;effect of component efficiency on the engine with inter-stage turbine burner was analyzed;combustion efficiency of main burner,inter-stage turbine burner,and after burner were contrasted.The result was different from the computation based on ideal cycle and it shows that thrust specific fuel consumption increases almost the same extent as the specific thrust after using inter-stage turbine burner on subsonic flight and specific thrust increases about 10% on supersonic;the economic performance is worse than base engine,and maneuverability is worse than engine with after burner.Then,the parameter of inter-stage turbine burner engine was optimized.

     

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