Dynamic analysis of the self-locking phenomenon in tape-spring hinges

被引：36
|
作者：
Hoffait, S. [1 ]
Bruls, O. [1 ]
Granville, D. [2 ]
Cugnon, F. [2 ]
Kerschen, G. [1 ]
机构：
[1] Univ Liege, Dept Aerosp & Mech Engn, B-4000 Liege, Belgium
[2] Samtech SA, B-4031 Liege, Belgium
来源：
ACTA ASTRONAUTICA | 2010年 / 66卷 / 7-8期
关键词：
Deployable structure; Tape-spring; Nonlinear dynamics; Buckling; Hysteresis; Self-locking; IMPROVED NUMERICAL DISSIPATION; STRUCTURAL DYNAMICS;
D O I：
10.1016/j.actaastro.2009.10.001
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper investigates the dynamic behaviour of tape-spring hinges that are commonly used in space deployable structures. During the deployment of an appendice (e.g. a solar panel or a beam), a tape-spring hinge allows the simultaneous achievement of the actuating, guiding and self-locking functions without friction elements. The proposed finite element model is able to capture buckling and hysteresis phenomena, which have a strong influence on the 3D motion of the system. A detailed analysis of those effects is developed, leading to a physical explanation of the crucial self-locking phenomenon. (C) 2009 Elsevier Ltd. All rights reserved.
引用
收藏
页码：1125 / 1132
页数：8
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