Volume 28 Issue 8
Aug.  2013
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CHEN Xiao-lei, GUO Ying-qing, ZHANG Shu-gang. Intelligent emergency control system of a certain turbofan engine[J]. Journal of Aerospace Power, 2013, 28(8): 1897-1904.
Citation: CHEN Xiao-lei, GUO Ying-qing, ZHANG Shu-gang. Intelligent emergency control system of a certain turbofan engine[J]. Journal of Aerospace Power, 2013, 28(8): 1897-1904.

Intelligent emergency control system of a certain turbofan engine

  • Received Date: 2012-07-20
  • Publish Date: 2013-08-28
  • Taking a certain turbofan engine as an example,the emergency control of aero-engine was introduced,and two emergency control modes were given:overthrust control and fast response control.The simulation results show that after constraint release,overthrust control can provide an additional 16.6% of the engine's thrust,but at the same time,the temperature of turbine inlet rises by 10.8%;and under fast response control,the rise time of low pressure rotor reduces to 1.675s from 2s,however the stability margin of compressor decreases by 6.05% and the thermo-mechanical fatigue life of the turbine guide vane declines by 5.16%.

     

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  • [1]
    Jonckheere E A,Yu G.Propulsion control of crippled aircraft by H model matching[J].Transactions on Control Systems Technology,1999,7(2):142-159.
    [2]
    Ochi Y,Kanai K.Automatic approach and landing for propulsion controlled aircraft by H control [C]//Proceedings of IEEE Conference on Control Applications.Piscataway,US:IEEE,1999:997-1110.
    [3]
    Jonckheere E A,Yu G,Chien C.Gain scheduling for lateral motion of propulsion controlled aircraft using neural networks [C]//Proceedings of the American Control Conference.Albuquerque,US:IEEE,1997:3321-3325.
    [4]
    Bates D G,Gatley S L,Postlethwaite I,et al.Robust integrated flight and propulsion control (IFPC) of an experimental STOVL aircraft [C]//Proceedings of IEEE Conference on Decision and Control.Tampa,US:IEEE,1998:4220-4221.
    [5]
    Ochi Y.Flight control system design for propulsion-controlled aircraft[J].Journal of Aerospace Engineering,2005,129(4):329-340.
    [6]
    Gatley S L,Harefors M,Bates D G.On the robustness properties of H integrated flight and propulsion controllers for a large transport aircraft [C]//Proceedings of IEEE Conference on Control Applications.Piscataway,US:IEEE,2002:138-143.
    [7]
    Burken J J,Maine T A,Jr Burcham F W,et al.Longitudinal emergency control system using thrust modulation demonstrated on an MD-11 airplane [R].AIAA-96-3062,1996.
    [8]
    Bokovic J D,Mehra R K.Intelligent adaptive control of a tailless advanced fighter aircraft under wing damage[J].Journal of Guidance,Control,and Dynamics,2000,23(5):876-884.
    [9]
    KrishnaKumar K,Limes G,Gundy B K,et al.An adaptive critic approach to reference model adaptation [R].AIAA 2003-5790,2003.
    [10]
    Turso J A,Lawrence C,Litt J S.Reduced-order modeling and wavelet analysis of turbofan engine structural response due to foreign object damage (FOD) events[J].Journal of Engineering for Gas Turbines and Power,2007,129(3):814-826.
    [11]
    Jaw L C,Van H T,Mink G R.Simulation of an intelligent engine control system for aircraft under adverse conditions [R].AIAA 2007-2810,2007.
    [12]
    Guo T H,Jonathan S L.Resilient propulsion control research for the NASA integerated resilient aircraft control(IRAC) project [R].NASA/TM-2007-214940,2007.
    [13]
    Csank J T,Chin J C,May R D,et al.Implementation of enhanced propulsion control modes for emergency flight operation [R].NASA/TM-2011-217038,2011.
    [14]
    Csank J T,May R D,Litt J S,et al.A sensitivity study of commercial aircraft engine response for emergency situations [R].NASA/TM-2011-217004,2011.
    [15]
    Csank J T,May R D,Gou T,et al.The effect of modified control limits on the performance of a generic commercial aircraft engine [R].NASA/TM-2012-217261,2012.
    [16]
    王海泉.航空发动机H鲁棒控制器设计及仿真验证 [D].西安:西北工业大学,2009. WANG Haiquan.H robust controller design for aero-engine and simulation [D].Xi'an:Northwestern Polytechnical University,2009.
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