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可折展扑翼飞行器瞬态折展机构设计与运动特性分析

ZHANG Jie HOU Yu YOU Chang LI Chenjiarui

机械科学与技术2025,Vol.44Issue(12):2047-2053,7.
机械科学与技术2025,Vol.44Issue(12):2047-2053,7.DOI:10.13433/j.cnki.1003-8728.20230302

可折展扑翼飞行器瞬态折展机构设计与运动特性分析

Design and Kinematics Characteristics of Transient Folding Mechanism for Flapping Wing Aircraft

ZHANG Jie 1HOU Yu 2YOU Chang 1LI Chenjiarui1

作者信息

  • 1. The Ministry of Education Key Laboratory of Metallurgical Equipment and Control Technology,Wuhan University of Science and Technology,Wuhan 430081,China
  • 2. The Ministry of Education Key Laboratory of Metallurgical Equipment and Control Technology,Wuhan University of Science and Technology,Wuhan 430081,China||Hubei Key Laboratory of Mechanical Transmission and Manufacturing Engineering,Wuhan University of Science and Technology,Wuhan 430081,China
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摘要

Abstract

Collapsible flapping wing aircraft is a kind of flapping wing aircraft whose wings can be folded and expanded.Researching the kinematic characteristics of transient folding mechanism is of great significance for improving the bionic degree and flight performance of flapping wing aircraft.Aiming at the problems such as low folding rate,inability to realize multi-segment folding and lower folding speed of flapping wing aircraft,a transient folding mechanism for two-stage wing folding of flapping wing aircraft was designed in this paper.The mathematical motion model of the transient folding mechanism was constructed.The motion characteristics of the transient folding mechanism was analyzed by MATLAB and ADAMS co-simulation.It is concluded that the flapping rate of the aircraft wings is 85.9%and the deployment time is 0.32 s.The design objective was satisfied,and the rationality of the research method was verified.The study laid a foundation for the performance improvement and practical application of collapsible flapping wing aircraft in the future.

关键词

扑翼飞行器/瞬态折展机构/联合仿真/数学模型/运动特性

Key words

flapping-wing aircraft/transient folding mechanism/co-simulation/mathematical models/kinematics characteristic

分类

机械制造

引用本文复制引用

ZHANG Jie,HOU Yu,YOU Chang,LI Chenjiarui..可折展扑翼飞行器瞬态折展机构设计与运动特性分析[J].机械科学与技术,2025,44(12):2047-2053,7.

基金项目

国家自然科学基金项目(52075397) (52075397)

机械科学与技术

OA北大核心

1003-8728

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