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TIAN Feilong, DING Hongshuai, ZHENG Hongliang, ZHAN Luoji. Optimal control of thrust for turboprop with engine and propeller integration during takeoff[J]. Journal of Aerospace Power, 2021, 36(9): 2012-2016. doi: 10.13224/j.cnki.jasp.20210804
Citation: TIAN Feilong, DING Hongshuai, ZHENG Hongliang, ZHAN Luoji. Optimal control of thrust for turboprop with engine and propeller integration during takeoff[J]. Journal of Aerospace Power, 2021, 36(9): 2012-2016. doi: 10.13224/j.cnki.jasp.20210804
shu

Optimal control of thrust for turboprop with engine and propeller integration during takeoff

doi: 10.13224/j.cnki.jasp.20210804

  • Aero Engine Control System Institute， Aero Engine Corporation of China，Wuxi Jiangsu 214063，China

  • Received Date: 2020-11-12
  • Publish Date: 2021-09-28
    Abstract
  • An engine and propeller integrated control architecture was proposed for turboprop engine rapid response during takeoff.Throttle lever was used to schedule the fuel control loop and pitch control loop for fast system response.A optimal control strategy for thrust was developed at the very beginning of the takeoff in order to maximize thrust according to the property of propeller.Air speed was selected to schedule the maximum effective power to improve thrust response during takeoff.The simulated result showed that the thrust increased by 2.59% in average during takeoff，and the time accelerated to takeoff was less than 2.5 s by the proposed optimal takeoff thrust control strategy and integrated control architecture.The system dynamic response was enhanced effectively by the designed method.

     

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    • References(18)
  • [1]
    SARAVANAMUTTOO H,ROGERS C,COHEN H.Gas turbine theory[M].New Delhi,India：Pearson Education,Limited,2013.
    [2]
    周盛,顾高墀,潘元杰,等.航空螺旋桨与桨扇[M].北京：国防工业出版社,1994.
    [3]
    刘沛清.空气螺旋桨理论及其应用[M].北京：北京航空航天大学出版社,2006.
    [4]
    时瑞军,周剑波,黄波,等.涡桨发动机控制技术演变及趋势[J].航空动力,2019（4）:39-41.
    [5]
    EASTBURG S R.NATOPS flight manual navy model E-2C aircraft[R].NAVAIR 01-E2AAF-1,2006.
    [6]
    MACLSAAC B,LANGTON R.Gas turbine propulsion systems[M].Chichester，UK：John Wiley and Sons Limited,2011.
    [7]
    WHALLEY R,EBRAHIMI M.Gas turbine propulsion plant control[J].Naval Engineering Journal,2010,114（4）:77-94.
    [8]
    GAERTNER W D.Development-share of MTU aero engines in TP400-D6 propulsion-system for T400M[R].ISABE-2005-1166,2005.
    [9]
    BRUN C L,GODBOY E,BEAUVOIS D,et al.Control laws design of a turboprop engine[J].Applied Mechanics and Materials,2014,704：362-367.
    [10]
    邓志伟,黄向华,田超.涡桨发动机螺旋桨实时建模技术[J].航空动力学报,2014,29（2）:434-440.
    [11]
    廉筱纯,吴虎.航空发动机原理[M].西安：西北工业大学出版社,2008.
    [12]
    JAW C L,MATTINGLY D J.Aircraft engine controls,design,system analysis and health monitoring[M].Reston，US：AIAA,2009.
    [13]
    陈怀容,王曦.一种基于螺旋桨部件特性的螺旋桨建模方法[J].航空动力学报,2017,32（10）：2526-2535.
    [14]
    SCHULTEN J B H M.Advanced propeller performance calculation by a lifting surface method[J].Journal of Propulsion and Power,1996,12（3）：477-485.
    [15]
    田超.航空涡桨发动机建模与控制仿真研究[D].南京：南京航空航天大学,2010.
    [16]
    时培燕,毛宁,杨恒辉,等.涡桨发动机螺旋桨建模与控制系统设计研究[J].计算机测量与控制,2016,24（5）:103-105.
    [17]
    COOK L D.Propeller control at low airspeed[R].AIAA 1965-709,1965.
    [18]
    WALSH P P,FLETCHER P.GAS turbine performance[M].Oxford，UK：Blackwell Science Limited,2004.
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