复合材料科学与工程 ›› 2025, Vol. 0 ›› Issue (7): 49-60.DOI: 10.19936/j.cnki.2096-8000.20250728.007

• 基础与力学性能研究 • 上一篇    下一篇

复合材料外骨骼关节一体化设计及力学行为研究

谢军虎1, 赵英豪1, 郝自清2, 陈磊3*   

  1. 1.中国空空导弹研究院,洛阳 471000;
    2.北京理工大学 宇航学院,北京 100081;
    3.中科院力学所 宽裕飞行工程科学与应用中心,北京 100190
  • 收稿日期:2024-04-29 出版日期:2025-07-28 发布日期:2025-08-22
  • 通讯作者: 陈磊(1988—),男,博士研究生,高级工程师,研究方向为飞行器结构轻量化设计,chenlei@imech.ac.cn。
  • 作者简介:谢军虎(1987—),男,硕士研究生,高级工程师,研究方向为机载导弹发射装置发控系统总体设计。

Integrated design and mechanical behavior of composite exoskeleton joints

XIE Junhu1, ZHAO Yinghao1, HAO Ziqing2, CHEN Lei3*   

  1. 1. China Airborne Missile Academy, Luoyang 471000, China;
    2. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;
    3. Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China
  • Received:2024-04-29 Online:2025-07-28 Published:2025-08-22

摘要: 本文提出一种全新的结构-关节一体化构型方案,利用板壳的屈曲与后屈曲现象,设计了复合材料结构-关节一体化的基本构型,通过最小势能原理,推导了复合材料结构-关节一体化构型在弯曲过程中的回复弯矩,建立了一体化关节几何参数-材料力学性能参数与助力效果(回复力矩)之间的映射关系。采用非接触式全场变形测量系统,搭建了试验平台,验证了助力效果的理论结果,并结合有限元渐进损伤失效分析方法,研究了准静态折叠情况下复合材料结构一体化关节的力学行为与材料损伤演化模式,并进一步研究了不同几何参数对一体化关节稳定支撑和助力效果的影响。该探索性研究在满足无动力背负外骨骼结构-关节体系基本功能性需求的前提下,可大幅减少零件数量、减轻结构重量、降低产品的加工成本。

关键词: 外骨骼关节, 复合材料, 结构-关节一体化

Abstract: This article proposes a new structural joint integration configuration scheme and establishes a nonlinear analytical model for the bending process of C-shaped composite material tape springs. By utilizing the buckling and subsequent buckling phenomena of plates and shells, the basic configuration of composite material structure joint integration is designed. Through the principle of minimum potential energy, the recovery bending moment of the composite material structure joint integration configuration during the bending process is derived, a mapping relationship has been established between the geometric parameters of the integrated joint, material mechanical performance parameters, and the assistance effect (recovery torque). Using a non-contact full field deformation measurement system, an experimental platform was established to verify the theoretical results of the assistance effect. Combined with the finite element progressive damage failure analysis method, the mechanical behavior and material damage evolution mode of the composite structure integrated joint under quasi-static folding were studied. Further research was conducted on the impact of different geometric parameters on the stability support and assistance effects of integrated joints. This exploratory study can significantly reduce the number of parts, reduce the weight of the structure, and reduce the processing cost of the product while meeting the basic functional requirements of the unpowered backpack exoskeleton structure joint system in the early stage.

Key words: exoskeleton joints, composite materials, structure joint integration

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