Analytical research on connecting structure of composite material satellite bearing cylinder

doi:10.7527/S1000-6893.2021.25161

CIOMP OpenIR

	Analytical research on connecting structure of composite material satellite bearing cylinder
	C. Yu; B. Liu; C. Li and C. Xue
	2022
发表期刊	Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
ISSN	10006893
卷号	43 期号:3
摘要	The connection structure damage of large satellite bearing cylinders is a key issue requiring consideration in the design.Taking the connection structure of a carbon fiber composite satellite bearing cylinder as the research object, we use the ABAQUS finite element software to establish the progressive damage model of the composite material laminate bolt connection.Based on the Hashin failure criterion and the Tserpes material performance degradation criterion, the Fortran language is adopted to develop the UMAT subroutine for the second time to study the failure mechanism of the bearing cylinder laminate bolt connection and the rubber-screw hybrid connection.In addition, the simulation analysis of the stiffness of the bolted connection structure is used to explore the impact on the mechanical properties of the satellite bearing cylinder test piece.The results show that the simulation of the satellite bearing cylinder test piece using the bolt connection structure stiffness for simulation modeling is closer to the experimental value, and compared with the MPC connection, the error is reduced by 4%-9%, indicating that this method better meets the requirements of simulation analysis.This analysis method provides reference for the mechanical property analysis of the composite satellite bearing cylinder connection structure and finite element simulation analysis of the multi-bolt connection structure, and is applicable for mechanical analysis of satellites with connected structures. 2022, Beihang University Aerospace Knowledge Press. All right reserved.
DOI	10.7527/S1000-6893.2021.25161
URL	查看原文
收录类别	ei
引用统计
文献类型	期刊论文
条目标识符	http://ir.ciomp.ac.cn/handle/181722/66417
专题	中国科学院长春光学精密机械与物理研究所
推荐引用方式 GB/T 7714	C. Yu,B. Liu,C. Li and C. Xue. Analytical research on connecting structure of composite material satellite bearing cylinder[J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2022,43(3).
APA	C. Yu,B. Liu,&C. Li and C. Xue.(2022).Analytical research on connecting structure of composite material satellite bearing cylinder.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,43(3).
MLA	C. Yu,et al."Analytical research on connecting structure of composite material satellite bearing cylinder".Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica 43.3(2022).

条目包含的文件		下载所有文件
文件名称/大小	文献类型	版本类型	开放类型	使用许可
Analytical research （9303KB）	期刊论文	出版稿	开放获取	CC BY-NC-SA	浏览下载