Research Progress on Thermally-induced Vibration of Large Deployable Space Structure

doi:10.12382/bgxb.2024.0636

Abstract

Abstract:

The thermally-induced vibration of large deployable space structureis one of thecitical issues in the development of China’s spacecraft with large-scale, high-precision and high-reliability. The research progress on thermally-induced vibration response are summarized in three aspects of the theoretical and numerical analysis, the experimental research, and the vibration suppression and structural optimization methods.The suggestions for the future research on thermally-induced vibration response of large deployable space structure are proposed corresponding to the development trend and demand of large-scale spacecraft technology in China.

Key words: large deployable space structure, thermally-induced vibration, thermal analysis, vibration suppression

CLC Number:

TN98

LUO Cheng, FAN Chao, BI Yanqiang, SU Xinming, LIN Guiping. Research Progress on Thermally-induced Vibration of Large Deployable Space Structure[J]. Acta Armamentarii, 2024, 45(S1): 231-241.

Figures/Tables 5

Fig.1 Deployable space antenna structure composed of thin-walled tubes

Fig.2 Thermal flutter criterion

Fig.3 Experimental system for thermally-induced vibration

Fig.4 Experimental results of thermally-induced vibration

Fig.5 Thermally-induced vibration experiment of space truss structure

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