Volume 39 Issue 4
Apr.  2024
Turn off MathJax
Article Contents
ZHANG Hongzhi, SONG Bifeng, SUN Zhongchao, et al. Design and dynamic performance analysis of multi-degree-of-freedom flapping wing driving mechanism[J]. Journal of Aerospace Power, 2024, 39(4):20210492 doi: 10.13224/j.cnki.jasp.20210492
Citation: ZHANG Hongzhi, SONG Bifeng, SUN Zhongchao, et al. Design and dynamic performance analysis of multi-degree-of-freedom flapping wing driving mechanism[J]. Journal of Aerospace Power, 2024, 39(4):20210492 doi: 10.13224/j.cnki.jasp.20210492

Design and dynamic performance analysis of multi-degree-of-freedom flapping wing driving mechanism

doi: 10.13224/j.cnki.jasp.20210492
  • Received Date: 2021-09-05
    Available Online: 2023-12-07
  • In order to realize the movement of the micro flapping-wing aircrafts’ wings along the complex trajectory, a flap-sweep multi-degree-of-freedom flapping-wing driving mechanism was designed. In view of the problem that the inertial force and elastic deformation of the mechanism’s transmission components affect the actuators’ driving force during the high-frequency motion, a rigid-flexible coupling dynamic model of the mechanism was established. At the same time, a dynamic performance factor that can quantify the difference between the driving force required by the actuators and its ideal value was proposed. Finally, combined with the orthogonal experiment, the influence of each thin-plate-component’s thickness on the dynamic performance of the mechanism was studied. The research results showed that the thin-plate-component subjecting to the out-of-plane load had a great influence on the dynamic performance of the driving mechanism, and the longer transmission chain’s force-transmission-path and the closer position to the actuators indicated the more significant impact; the flapping motion performance of the driving mechanism was stronger than the sweeping motion performance; In addition, the dynamic performance of the driving mechanism was not positively related to the thin-plate-component’s thickness.

     

  • loading
  • [1]
    BONTEMPS A,VANNESTE T,PAQUET J B,et al. Design and performance of an insect-inspired nano air vehicle[J]. Smart Materials and Structures,2013,22(1): 014008.1-014008.13.
    [2]
    YAN Xiaojun,QI Mingjing,LIN Liwei. Self-lifting artificial insect wings via electrostatic flapping actuators[C]//2015 28th IEEE International Conference on Micro Electro Mechanical Systems. Piscataway,US: IEEE,2015: 22-25.
    [3]
    杨艺,车云龙. 毫米级静电微扑翼驱动器的结构设计、工艺与测试[J]. 传感器与微系统,2018,37(1): 91-95. YANG Yi,CHE Yunlong. Structure design,fabrication and testing of millimeter-scale electrostatic micro flapping-wing actuator[J]. Transducer and Microsystem Technologies,2018,37(1): 91-95. (in Chinese doi: 10.13873/J.1000-9787(2018)01-0091-05

    YANG Yi, CHE Yunlong. Structure design, fabrication and testing of millimeter-scale electrostatic micro flapping-wing actuator[J]. Transducer and Microsystem Technologies, 2018, 37(1): 91-95. (in Chinese) doi: 10.13873/J.1000-9787(2018)01-0091-05
    [4]
    PENG Yuxin,LIU Li,ZHANG Yangkun,et al. A smooth impact drive mechanism actuation method for flapping wing mechanism of bio-inspired micro air vehicles[J]. Microsystem Technologies,2018,24(2): 935-941.
    [5]
    PHILLIPS N,KNOWLES K. Positive and negative spanwise flow development on an insect-like rotating wing[J]. Journal of Aircraft,2013,50(5): 1321-1332.
    [6]
    ORLOWSKI C T,GIRARD A R. Dynamics,stability,and control analyses of flapping wing micro-air vehicles[J]. Progress in Aerospace Sciences,2012,51: 18-30.
    [7]
    从梦磊,李君兰. 基于空间RURS机构的三维仿生扑翼机构设计与分析[J]. 航空动力学报,2019,34(3): 692-700. CONG Menglei,LI Junlan. Design and analysis of three-dimensional bio-inspired flapping wing mechanism based on spatial RURS linkage[J]. Journal of Aerospace Power,2019,34(3): 692-700. (in Chinese doi: 10.13224/j.cnki.jasp.2019.03.022

    CONG Menglei, LI Junlan. Design and analysis of three-dimensional bio-inspired flapping wing mechanism based on spatial RURS linkage[J]. Journal of Aerospace Power, 2019, 34(3): 692-700. (in Chinese) doi: 10.13224/j.cnki.jasp.2019.03.022
    [8]
    DICKINSON M H,LEHMANN F O,SANE S P. Wing rotation and the aerodynamic basis of insect flight[J]. Science,1999,284(5422): 1954-1960.
    [9]
    BAIK Y S,BERNAL L P. Experimental study of pitching and plunging airfoils at low Reynolds numbers[J]. Experiments in Fluids,2012,53(6): 1979-1992.
    [10]
    BERMAN G J,WANG Z J. Energy-minimizing kinematics in hovering insect flight[J]. Journal of Fluid Mechanics,2007,582: 153-168.
    [11]
    DONG Haibo,LIANG Zongxian,HARFF M. Optimal settings of aerodynamic performance parameters in hovering flight[J]. International Journal of Micro Air Vehicles,2009,1(3): 173-181.
    [12]
    LIU Zhiwei,YAN Xiaojun,QI Mingjing,et al. Design of flexible hinges in electromagnetically driven artificial flapping-wing insects for improved lift force[J]. Journal of Micromechanics and Microengineering,2019,29(1): 015011.1-015011.12.
    [13]
    宗光华,贾明,毕树生,等. 扑翼式微型飞行器的升力测量与分析[J]. 机械工程学报,2005,41(8): 120-124. ZONG Guanghua,JIA Ming,BI Shusheng,et al. Measurement and analysis of lift of micro air robot with flapping wings[J]. Journal of Mechanical Engineering,2005,41(8): 120-124. (in Chinese doi: 10.3321/j.issn:0577-6686.2005.08.020

    ZONG Guanghua, JIA Ming, BI Shusheng, et al. Measurement and analysis of lift of micro air robot with flapping wings[J]. Journal of Mechanical Engineering, 2005, 41(8): 120-124. (in Chinese) doi: 10.3321/j.issn:0577-6686.2005.08.020
    [14]
    HINES L,ARABAGI V,SITTI M. Shape memory polymer-based flexure stiffness control in a miniature flapping-wing robot[J]. IEEE Transactions on Robotics,2012,28(4): 987-990.
    [15]
    WIDHIARINI S,PARK J H,YOON B S,et al. Bird-mimetic wing system of flapping-wing micro air vehicle with autonomous flight control capability[J]. Journal of Bionic Engineering,2016,13(3): 458-467.
    [16]
    YOON S, KANG L, JO S. Development of air vehicle with active flapping and twisting of wing[J]. Journal of Bionic Engineering, 2011, 8(1): 1-9.

    YOON S,KANG L,JO S. Development of air vehicle with active flapping and twisting of wing[J]. Journal of Bionic Engineering,2011,8(1): 1-9.
    [17]
    WOOD R J,AVADHANULA S,SAHAI R,et al. Microrobot design using fiber reinforced composites[J]. Journal of Mechanical Design,2008,130(5): 052304.1-052304.11.
    [18]
    SREETHARAN P S,WHITNEY J P,STRAUSS M D,et al. Monolithic fabrication of millimeter-scale machines[J]. Journal of Micromechanics and Microengineering,2012,22(5): 055027.1-055027.6.
    [19]
    PHILLIPS N,KNOWLES K. Effect of flapping kinematics on the mean lift of an insect-like flapping wing[J]. Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering,2011,225(7): 723-736.
    [20]
    FINIO B M,WHITNEY J P,WOOD R J. Stroke plane deviation for a microrobotic fly[C]//2010 IEEE/RSJ International Conference on Intelligent Robots and Systems. Piscataway,US: IEEE,2010: 3378-3385.
    [21]
    WHITNEY J P,WOOD R J. Aeromechanics of passive rotation in flapping flight[J]. Journal of Fluid Mechanics,2010,660: 197-220.
    [22]
    王大燕. 考虑弹簧和运动副间隙的微扑翼飞行器翅翼机构动力学研究[D]. 成都: 西南交通大学,2008: 23-26. WANG Dayan. Research on the dynamics of flapping-wing mechanism with spring and bearing clearance[D]. Chengdu: Southwest Jiaotong University,2008: 23-26. (in Chinese

    WANG Dayan. Research on the dynamics of flapping-wing mechanism with spring and bearing clearance[D]. Chengdu: Southwest Jiaotong University, 2008: 23-26. (in Chinese)
  • 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 (333) PDF downloads(147) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return