基于蜜蜂腹部变体机制的空天飞行器仿生变体头锥设计

doi:10.3901/JME.2020.05.047

机械工程学报 ›› 2020, Vol. 56 ›› Issue (5): 47-54.doi: 10.3901/JME.2020.05.047

• 航天重器——空间大型可展机构与装备专刊 • 上一篇下一篇

基于蜜蜂腹部变体机制的空天飞行器仿生变体头锥设计

梁友鉴^1,2, 赵杰亮¹, 阎绍泽¹

1. 清华大学机械系摩擦学国家重点实验室智能生物机械分室北京 100084;
2. 航天东方红卫星有限公司北京 100094

收稿日期:2019-03-04 修回日期:2019-10-29 出版日期:2020-03-05 发布日期:2020-04-23
通讯作者: 阎绍泽(通信作者),男,1964年出生,博士,教授,博士研究生导师。主要研究方向为机械系统动力学、航天动力学与可靠性和智能结构设计与昆虫仿生。E-mail:yansz@mail.tsinghua.edu.cn
作者简介:梁友鉴,男,1991年出生,工程师。主要研究方向为卫星总体设计。E-mail:liangyoujianlw@163.com;赵杰亮,男,1989年出生,助理研究员。主要研究方向为仿生机械、机械设计理论及方法和航天器设计及动力学分析。E-mail:zhaojl2017@mail.tsinghua.edu.cn
基金资助:
国家自然科学基金（51475258，51805293）和北京市自然基金（3184050）资助项目。

Bionic Design of Morphing Nose Cone for Aerospace Vehicle Based on the Deformable Mechanism of Honeybee Abdomen

LIANG Youjian^1,2, ZHAO Jieliang¹, YAN Shaoze¹

1. Division of Intelligent and Biomechanical Systems, State Key Laboratory of Tribology, Tsinghua University, Beijing 100084;
2. DFH Satellite Co., Ltd., Beijing 100094

Received:2019-03-04 Revised:2019-10-29 Online:2020-03-05 Published:2020-04-23

摘要/Abstract

摘要： 头锥在空天飞行器气动外形的优化中起着重要作用，基于蜜蜂腹部的变体机制，设计了仿生变体头锥。利用X射线断层扫描技术和Amira软件对蜜蜂腹部分别进行全息无损扫描与三维重构，试验结果表明，相邻体节之间共有12束肌肉，通过等效将相邻体节间的生理结构演化为并联机构，利用基于螺旋理论的给定末端运动约束的型综合方法对上述机构进一步优化，根据变体头锥的技术指标，选择2（3-SPR）并串联机构作为变体头锥的变形驱动机构，并进行了运动学分析。利用扫描电子显微镜试验研究了节间褶的形态特征和分布规律，通过机构异化将其演化为锥面变胞折展机构。综合2（3-SPR）变形驱动并串联机构、锥面变胞折展机构和壳体，设计了具有分节结构的仿生变体头锥，以适应空天飞行器在不同飞行阶段的构型需求。

关键词: 蜜蜂腹部, 仿生变体头锥, 并联机构, 折展机构, 变胞机构

Abstract: The nose cone of aerospace vehicle plays an important role in optimizing the aerodynamic configuration. A morphing nose cone is designed by mimicking the deformable mechanism of honeybee abdomen. The X-ray phase-contrast imaging technique and Amira software are used to perform the non-destructive scanning and three-dimensional reconstruction on the honeybee abdomen. Experimental results show that there are 12 bundles of muscles between the adjacent segments. A 2(3-SPR) parallel-serial driving mechanism is evolved from the intersegmental structures based on the screw theory and technical specifications, and the kinematic analysis is carried out. The folded intersegmental membrane is studied by using scanning electron microscope analysis technology and a conical metamorphic foldable mechanism is developed by integrating the metamorphic mechanism. Then, a segmental morphing nose cone is designed, which is assembled from 2(3-SPR) parallel-serial driving mechanism, conical metamorphic foldable mechanism and body wall. It is significant for the aerospace vehicle to meet the deformation requirements in different flight stages.

Key words: honeybee abdomen, bionic morphing nose cone, parallel mechanism, foldable mechanism, metamorphic mechanism

中图分类号:

TG156

梁友鉴, 赵杰亮, 阎绍泽. 基于蜜蜂腹部变体机制的空天飞行器仿生变体头锥设计[J]. 机械工程学报, 2020, 56(5): 47-54.

LIANG Youjian, ZHAO Jieliang, YAN Shaoze. Bionic Design of Morphing Nose Cone for Aerospace Vehicle Based on the Deformable Mechanism of Honeybee Abdomen[J]. Journal of Mechanical Engineering, 2020, 56(5): 47-54.

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基于蜜蜂腹部变体机制的空天飞行器仿生变体头锥设计

Bionic Design of Morphing Nose Cone for Aerospace Vehicle Based on the Deformable Mechanism of Honeybee Abdomen

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