Abstract
Based on Timoshenko and Gere buckling theories and classic Euler beam buckling theory, two different theoretical models are established to analyze the stability of deployment status for the multi-layer equal tape-spring hinge. Twelve different single-layer and double-layer equal tape-spring hinges are tested. The relative errors of the folded peak moment between theoretical results and experimental results are no more than 7.73%, the average relative errors are no more than 4.93%, and the standard deviation is no more than 4.97%, which demonstrates the accuracy of the nonlinear mechanical model for the multi-layer equal tape-spring hinge. Parametric study shows that the greater section radius, central angle, thickness or layer number is, the greater the folded peak moment is. However, longitudinal length has a negative correlation with the folded peak moment.
| Original language | English |
|---|---|
| Pages (from-to) | 275-281 |
| Number of pages | 7 |
| Journal | Yuhang Xuebao/Journal of Astronautics |
| Volume | 37 |
| Issue number | 3 |
| DOIs | |
| State | Published - 30 Mar 2016 |
Keywords
- Buckling
- Experimental research
- Hyperelastic hinges
- Triangular prism deployment mast
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