Volume 27 Issue 5
May  2012
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Article Navigation >  Journal of Aerospace Power  > 2012  >  27(5): 1185-1193
DING Shui-ting, QIU Tian, LIU Xiao-feng, LIU Chuan-kai, Gong Lei. FHA method for FADEC system based on aero-thermodynamics model[J]. Journal of Aerospace Power, 2012, 27(5): 1185-1193.
Citation: DING Shui-ting, QIU Tian, LIU Xiao-feng, LIU Chuan-kai, Gong Lei. FHA method for FADEC system based on aero-thermodynamics model[J]. Journal of Aerospace Power, 2012, 27(5): 1185-1193.
shu

FHA method for FADEC system based on aero-thermodynamics model

  • 1.

    Beijing Key Laboratory on Safety of Integrated Aircraft and Propulsion Systems, Airworthiness Technologies Research Center, National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • 2.

    School of Transportation Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 2011-06-17
  • Publish Date: 2012-05-28
    Abstract
  • Starting from the airworthiness regulations related to full authority digital engine control(FADEC) system,considering the general principle of functional hazard assessment(FHA) and characteristics of FADEC system,the essential points of FHA for FADEC system were drew.According to the tool and data requirements,a hazard assessment for variable bleed valve (VBV) control function was conducted by using the aero-engine aero-thermodynamics model.The results indicate that:(1) This model could identify engine effect of FADEC system function failure.(2) Model analysis method of functional hazard for FADEC system which could determine engine effect hazard level through quantitative analysis,provides visual information for the assessment and could be a supplement for expert experience.

     

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