Volume 33 Issue 1
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Analysis on inverse kinematics of the three rings supporting and driving axialsymmetric vectoring exhaust nozzle[J]. Journal of Aerospace Power, 2018, 33(1): 24-29. doi: 10.13224/j.cnki.jasp.2018.01.003
Citation: Analysis on inverse kinematics of the three rings supporting and driving axialsymmetric vectoring exhaust nozzle[J]. Journal of Aerospace Power, 2018, 33(1): 24-29. doi: 10.13224/j.cnki.jasp.2018.01.003
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Analysis on inverse kinematics of the three rings supporting and driving axialsymmetric vectoring exhaust nozzle

doi: 10.13224/j.cnki.jasp.2018.01.003
  • Received Date: 2016-06-12
  • Publish Date: 2018-01-28
    Abstract
  • The three rings supporting and driving axialsymmetric vectoring exhaust nozzle mechanism was divided into three submodules. Spatial position analysis method, analytic geometry, and coordinate transformation method were applied to analyze the upper, middle and lower modules. A complete inverse kinematics model of axialsymmetric vectoring exhaust nozzle was established by each submodules. The experiment and computer simulation results showed that the mechanics design was reasonable and kinematics modeling was effective, the accuracy of the result was 98%, providing an important reference for the optimization design and control of the three rings supporting and driving axialsymmetric vectoring exhaust nozzles.

     

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    • References(17)
  • [1]
    GALOR B.Future jet technologies［J］.International Journal of Turbo and JetEngines,2013,30(2):197-198.
    [2]
    CAPONE F,SMERECZNIAK P,SPETNAGEL D,et al.Comparative investigation of multi plane thrust vectoring nozzles［R］.AIAA 92-3263,1992.
    [3]
    CLER D L,MASON M L.Experimental investigation of sphericalconvergentflap thrustvectoring two dimensional plug nozzles［R］.AIAA 93-2431,1993.
    [4]
    WILLIAMS R G,VITTAL B R.Fluidic thrust vectoring and throat control exhaust nozzle［R］.AIAA2002-4060,2002.
    [5]
    HAUER T A,LIPPMEIER W C,WOOD J M.Axisymmetric vectoring exhaust nozzle thermal shield:US5485959［P］.1996-01-23.
    [6]
    THAYER E B.Gas turbine vectoring nozzle:US5335489［P］.1994-08-09.
    [7]
    李晓明,伏宇.轴对称矢量喷管机构优化设计［J］.燃气涡轮试验与研究,2006,19(3):133-143.LI Xiaoming,FU Yu.Optimum design of AVEN mechanism［J］.Gas Turbine Experiment and Research,2006,19(3):133-143.(in Chinese)
    [8]
    丁凯锋,樊思齐.矢量喷管与发动机的共同工作研究［J］.航空动力学报,2000,15(1):96-98.DING Kaifeng,FAN Siqi.A study on cooperating between thrust vectoring nozzle and aeroengine［J］.Journal of Aerospace Power,2000,15(1):96-98.(in Chinese)
    [9]
    WANG Yuxin,WANG Yiming.Inverse kinematics of variable geometry parallel manipulator［J］.Mechanism and Machine Theory,2005,40(2):141-155.
    [10]
    王玉新.喷气发动机轴对称推力矢量喷管［M］.北京:国防工业出版社,2006:1-19.
    [11]
    王玉新,王仪明,李雨桐.轴对称推力矢量喷管载荷变形的控制补偿［J］.航空动力学报,2007,22(10):1685-1689.WANG Yuxin,WANG Yiming,LI Yutong.Load deformation compensation of the axis symmetric vectoring exhaust nozzle［J］.Journal of Aerospace Power,2007,22(10):1685-1689.(in Chinese)
    [12]
    LI H,GOSSELIN C M,RICHARD M J,et al.Analytic form of the sixdimensional singularity locus of the general goughstewart platform［J］.Journal of Mechanical Design,2005,128(1):279-287.
    [13]
    BANDYOPADHYAY S,GHOSAL A.Analysis of configuration space singularities of closedloop mechanisms and parallel manipulators［J］.Mechanism and Machine Theory,2004,39(5):519-544.
    [14]
    CHOUDHURY A P,GHOSAL B A.Singularity and controllability analysis of parallel manipulators and closedloop mechanisms［J］.Mechanism and Machine Theory,2000,35(10):1455-1479.
    [15]
    HUANG Z,CHEN L H,LI Y W.The singularity principle and property of stewart parallel manipulator［J］.Journal of Robotic Systems,2003,20(4):163-176.
    [16]
    SAITO T,FUJIMOTO T.Numerical studies of shock vector control for deflecting nozzle exhaust flows［M］.Berlin:Springer,2009:985-990.
    [17]
    王立峰,张津,唐海龙.推力矢量控制飞行的仿真研究［J］.航空动力学报,2000,15(4):427-430.WANG Lifeng,ZHANG Jin,TANG Hailong.Simulation of vector thrust control flight［J］.Journal of Aerospace Power,2000,15(4):427-430.(in Chinese)
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