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Dynamics Modeling and Characterization of Sunk Screw Connection Structure in Small Rockets

  • Xiaotian Zhang*
  • , Ruiqing Wang
  • , Xiaogang Li
  • , Chengyang Lu
  • , Zhengkang Wang
  • , Wenlong Wang
  • *此作品的通讯作者
  • Beihang University
  • Science and Technology on Space Physics Laboratory
  • China Aerospace Science and Technology Corporation

科研成果: 期刊稿件文章同行评审

摘要

Bolted flange joints are widely used in engineering structures. Sunk screw connection structures commonly used in small rockets and missiles exhibit significant nonlinear characteristics when subjected to forces. In this article, a study of the dynamic characteristics of sunk screw connection is conducted. A 3-dof trilinear dynamic model is proposed, based on the study of the stiffness characteristics of the connection structure and considering contact nonlinearities. The connection surface is simplified as two axial trilinear springs and a lateral linear spring. The motion of the system can be divided into nine regions by the turning point of the trilinear springs. So that the motion of the system in each region can be completely resolved, the dynamic characteristics of the 3-dof trilinear system under impulse load and simple harmonic load are studied by means of semi-numerical analytical method. It is found that the response frequency of the system remains unchanged under a small impulse load, and the response can be obtained by approximate analytical expressions. When the impulse load is large, the response frequency is fluctuant, which reflects the sensitivity of the nonlinear system to the magnitude of impulse load. Under the simple harmonic excitation of bending moment, the response frequency curve of the system presents good single peak characteristics when the excitation amplitude is small. When the amplitude is large, the peak frequency of the system shifts, and the phenomenon of multi-peak resonance is shown in a certain range.

源语言英语
期刊论文编号648
期刊Aerospace
9
11
DOI
出版状态已出版 - 11月 2022

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