Volume 34 Issue 11
Nov.  2019
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ZHANG You, ZHANG Binshan, WU Feng. Six-component stand design and vector thrust positioning[J]. Journal of Aerospace Power, 2019, 34(11): 2324-2330. doi: 10.13224/j.cnki.jasp.2019.11.003
Citation: ZHANG You, ZHANG Binshan, WU Feng. Six-component stand design and vector thrust positioning[J]. Journal of Aerospace Power, 2019, 34(11): 2324-2330. doi: 10.13224/j.cnki.jasp.2019.11.003

Six-component stand design and vector thrust positioning

doi: 10.13224/j.cnki.jasp.2019.11.003
  • Received Date: 2019-05-15
  • Publish Date: 2019-11-28
  • Based on the screw theory, some basic design principles of six-component thrust stand were described to ensure its effectiveness. This proved that it was improper mathematically to predict the vector thrust by multiplying the inverse static mapping matrix with the reading of sensors, and only three forces and three moments of the vector thrust can be obtained, but the action point cannot be accurately positioned. In order to find the action point, an experimental method denoted as circular deflection method was proposed, at least three tests about thrusts of same axial angle and different direction angles were needed.Finally, the validity of the proposed method was verified by examples. The numerical result showed that the weights of the engine and the floating frame seriously affected the positioning of action point, so the gravity influence must be eliminated before using this method.

     

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  • [1]
    梁春华,张仁,沈迪刚.国外航空发动机推力矢量喷管技术的发展研究[J].航空发动机,1998,24(1):49-55.LIANG Chunhua,ZHANG Ren,SHEN Digang.The development of foreign aeroengine vectoring exhaust nozzle[J].Aeroengine,1998,24(1):49-55.(in Chinese)
    [2]
    CAPONE F,SMERECZNIAK P,SPETNAGEL D,et al.Comparative investigation of multi-plane thrust vectoring nozzles[R].AIAA 92-3263,1992.
    [3]
    赵景芸,金捷.推力矢量技术的研究与发展[J].燃气涡轮试验与研究,1999,12(1):51-54.ZHAO Jingyun,JIN Jie.Development andinvestigation of thrust-vectoring technology[J].Gas Turbine Experiment and esearch,1999,12(1):51-54.(in Chinese)
    [4]
    ASHLEY S.Thrust vectoring:a new angle to air superiority[J].Mechanical Engineering,1995,117(1):58-64.
    [5]
    汤伟,黄勇,傅澔.推力矢量对飞机大迎角动态气动特性的影响[J].航空学报,2018,39(4):121648.1-121648.7.TANG Wei,HUANG Yong,FU Hao.Effect of thrust vector on dynamic aerodynamic characteristics of air craft at high angle of attack[J].Acta Aeronautica et Astronautica Sinica,2018,39(4):2018,39(4):121648.1-121648.7.(in Chinese)
    [6]
    RUNYAN R B,RYND J P,SEELY J F.Thrust stand design principles[R].Nashville,TN:AIAA 17th Aerospace Ground Testing Conference,1992.
    [7]
    赵永生,姚建涛,候雨雷,等.并联结构六维传感器[M].北京:国防工业出版社,2014.
    [8]
    于常安,王罗,何显中,等.航空矢量喷管测试平台用六分量盒式天平结构设计[J].航空动力学报,2016,31(1):23-30.YU Changan,WANG Luo,HE Xianzhong,et al.Design on structure of six-component box balance for the aero-engine vector nozzle measuring platform[J].Journal of Aerospace Power,2016,31(1):23-30.(in Chinese)
    [9]
    湛华海.航空发动机矢量喷管六分量测力系统研制[D].重庆大学,2008.ZHAN Huahai.Development of six-component balance system for measuring plane engine vector nozzle[D].Chongqing:Chongqing University,2008.(in Chinese)
    [10]
    廉筱纯,吴虎.航空发动机原理[M].西安:西北工业大学出版社,2005.
    [11]
    黄真.高等空间机构学[M].北京:高等教育出版社,2006.
    [12]
    王勖成.有限单元法[M].北京:清华大学出版社,2003.
    [13]
    李慧剑,杜国君,胡宇达,等.理论力学[M].北京:科学出版社,2015.
    [14]
    张有,吴锋,何培垒.航空发动机推力测量台架原理误差分析[J].航空发动机,2016,42(4):76-80.ZHANG You,WU Feng,HE Peilei.Principle errors analysis of thrust measurement test bench system for aeroengine[J].Aeroengine 2016,42(4):76-80.(in Chinese)
    [15]
    赵志刚,李建鹏,刘洋,等.三环驱动轴对称推力矢量喷管逆运动学分析[J].航空动力学报,2018,33(1):24-29.ZHAO Zhigang,LI Jianpeng,LIU Yang,et al.Design on structure of six-component box balance for the aero-engine vector nozzle measuring platform[J].Journal of Aerospace Power,2018,33(1):24-29.(in Chinese)
    [16]
    屈裕安,谢寿生,宋志平.矢量喷管控制对发动机性能的影响[J].航空动力学报,2004,19(3):300-304.QU Yuan,XIE Shousheng,SONG Zhiping.The effect of thrust vector control on the performance of turbofan engine[J].Journal of Aerospace Power,2004,19(3):300-304.(in Chinese)
    [17]
    罗华云,赖传兴,王月贵,等.喷管模型试验器六分量天平校准技术[J].航空动力学报,2013,28(1):67-76.LUO Huayun,LAI Chuanxin,WANG Yuegui,et al.Six component balance calibration technology for nozzle model testing facility[J].Journal of Aerospace Power,2013,28(1):67-76.(in Chinese)
    [18]
    付尧明,王强,额日其太,等.矢量喷管六分量测力试验台的研制[J].实验流体力学,2002,16(1):87-93.FU Yaoming,WANG Qiang,Eriqitai,et al.Development of the six-component force-measuring balance for thrust vectoring nozzle testing[J].Journal of Experiments in Fluid Mechanics,2002,16(1):87-93.(in Chinese)
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