AEROSPACE CHINA

中国航天科技集团有限公司主管

中国航天系统科学与工程研究院主办

ISSN 1671-0940

CN 11-4673/V

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AEROSPACE CHINA ›› 2021, Vol. 22 ›› Issue (2): 59-64.doi: 10.3969/j.issn.1671-0940.2021.02.007

• 专刊 • 上一篇    下一篇

Study of Finite Element Analysis on Launch Vehicle Connection Structural Strength

  

  • 出版日期:2021-08-10 发布日期:2021-08-10

Study of Finite Element Analysis on Launch Vehicle Connection Structural Strength

  1. Beijing Institute of Astronautical Systems Engineering, Beijing 100076
  • Online:2021-08-10 Published:2021-08-10
  • About author:WU Hao (1981– ), received her Ph.D. degree from the Beijing University, and currently works at the Beijing Institute of Astronautical Systems Engineering, engaged in structural design and strength analysis.

Abstract: The strength of the connection structure has always been a key issue in the structural design of a launch vehicle. In this paper, the finite element analysis method is used for the strength of typical connection structures of a new launch vehicle. The research scope includes the inter-stage connection structure and the bundle connection structure. Aiming at establishing the strength of these two connection structures under flight conditions, we built a refined finite element model, simulated the bolt tensile test and obtained a calculation criteria, and carried out finite element analysis of the connection structures under flight conditions. As a result, we not only established the analysis and evaluation method of the connection structures based on the refined finite element modeling analysis, but also provided a fast numerical simulation design method for the development of the launch vehicle’s connection structures, which greatly improved the design efficiency and reduced the design risk.

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