受蜜蜂腹部启发的航空航天飞行器变形鼻锥集成变形锁定设计

IF 5.8 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Xiangbing Wu , Jieliang Zhao , Tonghui Fan , Xuemei Chen , Junlan Li , Wenzhong Wang , Shaoze Yan
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引用次数: 0

摘要

利用变形机构主动调整气动外形是提高航天飞行器环境适应性和机动性的有效手段。本文以蜜蜂腹部变形机理为灵感,设计了一种可实现4个水平(2个水平拉伸和2个水平弯曲)和2个方向(z方向和x方向)变形运动的串并联变形鼻锥(MNC)机构。创新地提出了一种变形-锁定一体化设计方法,实现了数控机床任意位置的锁定。基于螺旋理论,完成了机构的支链综合和自由度分析。建立了该机构的运动学和动力学模型,分析了其运动特性和工作空间。针对起步阶段驱动负荷较大的问题,设计了起步阶段驱动转矩补偿方案。补偿后的启动转矩明显减小,转矩曲线更加平滑。有限元分析证实,锁紧链和力自锁机构的设计大大提高了数控机床的轴向刚度。制作了MNC的功能样机,并进行了变形试验。样机可实现8个独立的变形配置过程,任意位置稳定锁定,最大弯曲角度19.65°,最大拉伸79.55 mm,最大拉伸率14.75%,运动偏差<; 3%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Morphing nose cone with integrated deformation-locking design for aerospace vehicle inspired by honeybee abdomen
Active adjustment of aerodynamic shape by morphing mechanisms is an effective means to improve the environmental adaptability and maneuverability of aerospace vehicles. In this paper, inspired by the deformation mechanism of honeybee abdomen, a series-parallel morphing nose cone (MNC) mechanism that can realize deformation motions in four levels (2 levels of stretching and 2 levels of bending) and two directions (z-direction and x-direction) is designed. A deformation-locking integrated design method is innovatively proposed to achieve the locking of MNC at any position. Based on the screw theory, the branch-chain synthesis and degree of freedom (DOF) analysis of the mechanism are completed. The kinematics and dynamics models of the proposed mechanism are constructed, and its motion characteristics and working space are analyzed. Aiming at the problem with the heavier driving burden in the starting stage, the driving torque in the initial stage was designed to be compensated. Compensated start-up torque is significantly reduced, and the torque curve is smoother. Finite element analysis confirmed that the design of the locking chains and the force self-locking mechanism greatly enhances the axial stiffness of the MNC. A functional prototype of MNC is manufactured and the deformation experiments are conducted. The prototype can achieve eight independent morphing configuration processes and stable locking at any position, with a maximum bending angle of 19.65°, a maximum stretching of 79.55 mm, a maximum stretching rate of 14.75 %, and a motion deviation of <3 %.
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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