Turn off MathJax
Article Contents
ZHANG Jinyao, REN Junxue, XUE Muyao, et al. Theoretical and experimental investigation on measurement error of pivot point excursion of flexible joint[J]. Journal of Aerospace Power, 2022, X(X):20220710 doi: 10.13224/j.cnki.jasp.20220710
Citation: ZHANG Jinyao, REN Junxue, XUE Muyao, et al. Theoretical and experimental investigation on measurement error of pivot point excursion of flexible joint[J]. Journal of Aerospace Power, 2022, X(X):20220710 doi: 10.13224/j.cnki.jasp.20220710

Theoretical and experimental investigation on measurement error of pivot point excursion of flexible joint

doi: 10.13224/j.cnki.jasp.20220710
  • Received Date: 2022-09-20
    Available Online: 2024-01-25
  • In order to quantitatively analyze the measuring error source of pivot point excursion for flexible joint, the pivot point excursion at different vector angles under 10 MPa vessel pressure was calculated using ANSYS software. According to the experimental results of flexible joint, the influences of pendulum rod deformation, horizontal displacement sensor push rod measurement error, push rod measurement error and horizontal deviation of vertical displacement sensor on the measurement results of pivot point excursion were studied respectively. In addition, the influence of the structural error of flexible joint was studied by simulations. Results showed that the measured pivot point excursion was in good agreement with the simulation after correcting four kinds of errors. The error sources in the measurement of pivot point excursion were confirmed, in which the push rod measurement errors of horizontal and vertical displacement sensors accounted for 65.98% of the cylindrical envelope height error, and 77.32% of the cylindrical envelope radius error, respectively. And these led to a great influence on the axial and radial drifts of flexible joint. Moreover, the structural error of flexible joint also affected the measurement of pivot point excursion. The distribution of pivot point excursion caused by the thickness error of elastomers and reinforcements was consistent. The results can provide a theoretical guidance for the error analysis of pivot point excursion measurement of flexible joint.

     

  • loading
  • [1]
    SHANI S,PUTTER S,PERETZ A. Development of a high-performance flexible joint for thrust vector control: AIAA1995-3017[R]. Reston,US: AIAA,1995.
    [2]
    林培基,高峰. 推力矢量对防空导弹作战效能的影响[J]. 飞航导弹,2009(1): 56-57,64. LIN Peiji,GAO Feng. Influence of thrust vector on operational effectiveness of air defense missile[J]. Winged Missiles Journal,2009(1): 56-57,64. (in Chinese

    LIN Peiji, GAO Feng. Influence of thrust vector on operational effectiveness of air defense missile[J]. Winged Missiles Journal, 2009(1): 56-57, 64. (in Chinese)
    [3]
    吉礼超,宋贵宝. 防空导弹控制方法的研究现状及展望[J]. 战术导弹技术,2009(3): 54-59. JI Lichao,SONG Guibao. Current study status and future prospect of control mode of air-defense missile[J]. Tactical Missile Technology,2009(3): 54-59. (in Chinese

    JI Lichao, SONG Guibao. Current study status and future prospect of control mode of air-defense missile[J]. Tactical Missile Technology, 2009(3): 54-59. (in Chinese)
    [4]
    张涵,李旭昌,王宏宇,等. 基于固体火箭发动机技术的防空导弹控制发展综述[J]. 飞航导弹,2013(11): 75-79. ZHANG Han,LI Xuchang,WANG Hongyu,et al. Review on the development of air defense missile control based on solid rocket engine technology[J]. Aerodynamic Missile Journal,2013(11): 75-79. (in Chinese

    ZHANG Han, LI Xuchang, WANG Hongyu, et al. Review on the development of air defense missile control based on solid rocket engine technology[J]. Aerodynamic Missile Journal, 2013(11): 75-79. (in Chinese)
    [5]
    王铮,胡永强. 固体火箭发动机[M]. 北京: 中国宇航出版社,1993. WANG Zheng,HU Yongqiang. Solid rocket motor[M]. Beijing: China Astronautic Press,1993. (in Chinese

    WANG Zheng, HU Yongqiang. Solid rocket motor[M]. Beijing: China Astronautic Press, 1993. (in Chinese)
    [6]
    杨冀英,杜保华. 摆杆形变对柔性接头摆心、摆角数据的影响[J]. 强度与环境,2007,34(1): 55-58. YANG Jiying,DU Baohua. The influence on the pivot point and deflection angle’s test datum from the pendulum shaft’s deformation[J]. Structure & Environment Engineering,2007,34(1): 55-58. (in Chinese

    YANG Jiying, DU Baohua. The influence on the pivot point and deflection angle’s test datum from the pendulum shaft’s deformation[J]. Structure & Environment Engineering, 2007, 34(1): 55-58. (in Chinese)
    [7]
    阮彩霞. 柔性接头摆动实验方法研究[D]. 西安: 西安电子科技大学,2008. RUAN Caixia. Research on the experimental methods for flexible connector swing[D]. Xi’an: Xidian University,2008. (in Chinese

    RUAN Caixia. Research on the experimental methods for flexible connector swing[D]. Xi’an: Xidian University, 2008. (in Chinese)
    [8]
    王超,任军学,郝文强,等. 柔性接头有效摆心漂移特性[J]. 航空动力学报,2014,29(12): 2993-2999. WANG Chao,REN Junxue,HAO Wenqiang,et al. Characteristics of effective pivot point excursion for flexible joint[J]. Journal of Aerospace Power,2014,29(12): 2993-2999. (in Chinese

    WANG Chao, REN Junxue, HAO Wenqiang, et al. Characteristics of effective pivot point excursion for flexible joint[J]. Journal of Aerospace Power, 2014, 29(12): 2993-2999. (in Chinese)
    [9]
    谢传峰. 动力学[M]. 北京: 高等教育出版社,2002. XIE Chuanfeng. Dynamics[M]. Beijing: Higher Education Press,2002. (in Chinese

    XIE Chuanfeng. Dynamics[M]. Beijing: Higher Education Press, 2002. (in Chinese)
    [10]
    张荣. 机械原理[M]. 武汉: 华中科技大学出版社,2015. ZHANG Rong. Mechanical principle[M]. Wuhan: Huazhong University of Science and Technology Press,2015. (in Chinese

    ZHANG Rong. Mechanical principle[M]. Wuhan: Huazhong University of Science and Technology Press, 2015. (in Chinese)
    [11]
    陈汝训,李志明,黄坚定. 固体火箭发动机设计与研究(下)[M]. 北京: 中国宇航出版社,1992. CHEN Ruxun,LI Zhiming,HUANG Jianding. Design and research of solid rocket motor (Volume 2) [M]. Beijing: China Astronautic Press,1992. (in Chinese

    CHEN Ruxun, LI Zhiming, HUANG Jianding. Design and research of solid rocket motor (Volume 2) [M]. Beijing: China Astronautic Press, 1992. (in Chinese)
    [12]
    张晓光,刘宇,任军学,等. 小型柔性接头推力矢量性能试验[J]. 航空动力学报,2012,27(12): 2836-2841. ZHANG Xiaoguang,LIU Yu,REN Junxue,et al. Experimental investigation of miniature flexible joint thrust vector characteristics[J]. Journal of Aerospace Power,2012,27(12): 2836-2841. (in Chinese

    ZHANG Xiaoguang, LIU Yu, REN Junxue, et al. Experimental investigation of miniature flexible joint thrust vector characteristics[J]. Journal of Aerospace Power, 2012, 27(12): 2836-2841. (in Chinese)
    [13]
    SANTHOSH K V,ROY B K. A smart displacement measuring technique using linear variable displacement transducer[J]. Procedia Technology,2012,4: 854-861. doi: 10.1016/j.protcy.2012.05.140
    [14]
    雷建和,胡廷轩,张栋,等. 基于RBF的LVDT输出标定研究[J]. 测控技术,2016,35(10): 93-96. LEI Jianhe,HU Tingxuan,ZHANG Dong,et al. Research on LVDT output calibration based on RBF[J]. Measurement & Control Technology,2016,35(10): 93-96. (in Chinese

    LEI Jianhe, HU Tingxuan, ZHANG Dong, et al. Research on LVDT output calibration based on RBF[J]. Measurement & Control Technology, 2016, 35(10): 93-96. (in Chinese)
    [15]
    DUNHAM R S,NICKELL R E. Finite element analysis of axisymmetric solids with arbitrary loadings[M]. Berkeley,US: Structural Engineering Laboratory,University of California,1967.
    [16]
    吴文辉,李兵. 推力矢量火箭发动机柔性接头力学特性仿真分析[J]. 水雷战与舰船防护,2015,23(3): 21-26. WU Wenhui,LI Bing. Simulation and analysis on mechanical behavior of flexible joint for thrust vector rocket motor[J]. Mine Warfare & Ship Self-Defence,2015,23(3): 21-26. (in Chinese

    WU Wenhui, LI Bing. Simulation and analysis on mechanical behavior of flexible joint for thrust vector rocket motor[J]. Mine Warfare & Ship Self-Defence, 2015, 23(3): 21-26. (in Chinese)
    [17]
    邹杰,郑庆,童悦,等. 高压载荷下柔性喷管的力学特性试验与有限元分析[J]. 弹箭与制导学报,2019,39(6): 150-154. ZOU Jie,ZHENG Qing,TONG Yue,et al. Experiment studies and numerical analysis of flexible nozzle with high pressure[J]. Journal of Projectiles,Rockets,Missiles and Guidance,2019,39(6): 150-154. (in Chinese

    ZOU Jie, ZHENG Qing, TONG Yue, et al. Experiment studies and numerical analysis of flexible nozzle with high pressure[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2019, 39(6): 150-154. (in Chinese)
    [18]
    SU Hao,REN Junxue,XUE Muyao,et al. Influence of pressure and deflection loads on the critical behavior of flexible joints[J]. Composite Structures,2017,180: 772-781. doi: 10.1016/j.compstruct.2017.08.062
    [19]
    PUGLISI G,SACCOMANDI G. Multi-scale modelling of rubber-like materials and soft tissues: an appraisal[J]. Proceedings Mathematical,Physical,and Engineering Sciences,2016,472(2187): 20160060.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (9) PDF downloads(1) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return