Design and Analysis of the Driving Mechanism of Multi-DOF Flapping Wing Aircrafts

wang Wang; Xiaoxu Pang

doi:10.16578/j.issn.1004.2539.2022.06.012

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Design and Analysis of the Driving Mechanism of Multi-DOF Flapping Wing Aircrafts

Design· Calculation | 更新时间：2022-10-04

- Design and Analysis of the Driving Mechanism of Multi-DOF Flapping Wing Aircrafts
- Journal of Mechanical Transmission Vol. 46, Issue 6, Pages: 78-84(2022)
- 作者机构：
  
  1.山西机电职业技术学院机械工程系，山西长治 046011
  2.河南科技大学机电工程学院，河南洛阳 471003
- 作者简介：
- 基金信息：
- DOI：10.16578/j.issn.1004.2539.2022.06.012
  CLC：
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王望,庞晓旭.多自由度扑翼飞行器驱动机构的设计与分析[J].机械传动,2022,46(06):78-84.

Wang wang,Pang Xiaoxu.Design and Analysis of the Driving Mechanism of Multi-DOF Flapping Wing Aircrafts[J].Journal of Mechanical Transmission,2022,46(06):78-84.
王望,庞晓旭.多自由度扑翼飞行器驱动机构的设计与分析[J].机械传动,2022,46(06):78-84. DOI： 10.16578/j.issn.1004.2539.2022.06.012.

Wang wang,Pang Xiaoxu.Design and Analysis of the Driving Mechanism of Multi-DOF Flapping Wing Aircrafts[J].Journal of Mechanical Transmission,2022,46(06):78-84. DOI： 10.16578/j.issn.1004.2539.2022.06.012.

摘要

为了提高扑翼飞行器的飞行性能，借鉴中小型鸟类的飞行运动特征，设计了一种基于空间连杆机构的新型多自由度扑翼机构。首先，通过运动学分析建立了扑翼飞行器驱动机构的运动学模型；然后，在Adams仿真软件中建立了扑翼机构仿真分析模型，对理论分析进行了验证。结果表明，所设计的驱动机构通过单自由度驱动就能够实现扑动、扭转、偏转多个自由度耦合运动。其中，上扑动极限为34.65°、下扑动极限为-29.66°，最大扭转角为15.05°，最小扭转角为-14.9°，偏转角范围为-5.01°~5.21°；输出的“8”字形轨迹与中小型鸟类飞行时的翼尖轨迹相同，具有良好的气动性能。仿真得到的运动学参数与理论计算一致，验证了理论计算的正确性。

Abstract

In order to improve the flight performance of flapping wing aircrafts，a multi-DOF flapping wing mechanism based on space four-bar mechanism is designed by referring to the flight motion characteristics of small and medium-sized birds. Firstly，a kinematic model of the flapping wing driving mechanism is established through kinematic analysis. Then，a simulation model of the flapping wing mechanism is established in Adams to verify the theoretical analysis. The results show that， the design of a driving mechanism with single degree-of-freedom drive can realize the flutter，torsion，deflection multi-degree-of-freedom coupling movement，and the upper flutter limit is 34.65°，the lower flutter limit is -29.66°，the maximum torsion angle is 15.05°，the minimum torsion angle is -14.9°，the deflection angle range is -5.01°~5.21°； the track wich an "8" word output is the same as that of flying wing tips of small and medium-sized birds，which shows a good aerodynamic performance. The kinematic parameters obtained by simulation are in agreement with the theoretical calculation，which verifies the correctness of the theoretical calculation.

关键词

扑翼飞行器多自由度驱动机构运动学分析Adams

Keywords

Flapping wing aircraftsMulti-degree-of-freedomDriving mechanismKinematic analysisAdams

references

杨永刚，苏汉平.基于XFlow多自由度仿鸟扑翼飞行器气动仿真［J］.系统仿真学报，2018，30（6）：2162-2167.

YANG Yonggang，SU Hanping.Aerodynamic simulation of multi-dof flapping-wing air vehicle of bird-like based on XFlow software［J］.Journal of System Simulation，2008，30（2）：2162-2167.

LIU H.An introduction to flapping wing aerodynaimcs［M］.New York：Cambridge University Press，2013：33-45.

LIU H，RAVI S，KOLOMENSKIY D，et al.Biomechanics and biomimetics in insectinspired flight systems［J］.Philosophical Transactions of the Royal Society B：Biological Sciences，2016，371（1704）：13-15.

周凯.微扑翼飞行器动力学仿真及驱动机构优化设计［D］.西安：西北工业大学，2007：30-42.

ZHOU Kai.Dynamics simulation and optimization design of driving mechanisms of FMAV［D］.Northwestern Polytechnical University，2007：30-42.

侯宇，方宗德，刘岚，等.仿生微扑翼飞行器机构动态分析与工程设计方法［J］.航空学报，2005（2）：173-178.

HOU Yu，FANG Zongde，LIU Lan，et al.Dynamic analysis and engineering design of biomimetic flapping-wing micro air vehicles［J］.Journal of Aerospace Power，Sinica，2005（2）：173-178.

朱保利.多自由度扑翼微型飞行器设计研究［D］.南京：南京航空航天大学，2007：18-31.

ZHU Baoli.Design and research of multi-degree of freedom flapping wing micro-vehicle［D］.Nanjing：Nanjing University of Aeronautics and Astronautics，2007：18-31.

张瑞坤，何畏，王习术，等.偏置式空间RSSR急回仿生扑翼机构优化设计与分析［J］.机械科学与技术，2021，11（3）：200-207.

ZHANG Ruikun，HE Wei，WANG Xishu，et al.Optimal design of RSSR quick-return bionic flapping-wing mechanism in offset space［J］.Mechanical Science and Technology for Aerospace Engineering，2021，11（3）：200-207.

孙茂，吴江浩.昆虫飞行的高升力机理和能耗［J］.北京航空航天大学学报，2003（11）：970-977.

SUN Mao，WU Jianghao.Unsteady lift mechanisms and energetic in flying insects［J］.Journal of Beijing University of Aeronautics and Astronautics，2003（11）：970-977.

孙恒，陈作模.机械原理［M］.6版.北京：高等教育出版社，2001：133-135.

SUN Heng，CHEN Zuomo.Theory of machines and mechanisms［M］.6th Ed.Beijing：Higher Education Press，2001：133-135.

郭建伟，周洋，贺业荣.全转动副空间扑翼机构设计［J］.机械传动，2014，38（5）：74-76.

GUO Jianwei，ZHOU Yang，HE Yerong.Design of pure revolute-joint spatial flapping mechanism［J］.Journal of Mechanical Transmission，2014，38（5）：74-76.

SHYY W，BERG M，LJUNGQVIST D.Flapping and flexible wings for biological and micro air vehicles［J］.Progress in Aerospace Sciences，1999，35（5）：455-505.

DICKINSON M H，LEHMANN F O S，SANJAY P.Wing rotation and the aerodynamic basis of insect flight［J］.Science，1999，284（5422）：1954-1960.

张小俊，胡淑玲.扑翼飞行器平面形状对气动力的影响研究［J］.飞行力学，2015，33（1）：17-20.

ZHANG Xiaojun，HU Shuling.Influence of wing shape on the aerodynamic characteristics of flapping-wing vehicle［J］.Flight Dynamics，2015，33（1）：17-20.

徐一村，宗光华，毕树生，等.空间曲柄摇杆扑翼机构设计分析［J］.航空动力学报，2009，24（1）：204-208.

XU Yicun，ZONG Guanghua，BI Shusheng，et al.Design and analysis of a spatial crank-rocker flapping-wing Mechanism［J］.Journal of Aerospace Power，2009，24（1）：204-208.

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