Dynamic analysis and optimization of double-layer tape-spring hinge

YANG Hui, LIU Rong-qiang, WANG Yan, GUO Hong-wei, TAO Jian-guo

Journal of Vibration and Shock ›› 2016, Vol. 35 ›› Issue (9) : 20-27.

PDF(1985 KB)
PDF(1985 KB)
Journal of Vibration and Shock ›› 2016, Vol. 35 ›› Issue (9) : 20-27.

Dynamic analysis and optimization of double-layer tape-spring hinge

  • YANG Hui, LIU Rong-qiang, WANG Yan, GUO Hong-wei, TAO Jian-guo
Author information +
History +

Abstract

 Flexible tape-spring hinges can be folded elastically and are able to self-deploy by releasing stored strain energy with fewer component parts and slight weights. Deploying dynamics behaviors of double-layer tape-spring (DLTS) hinge was optimized for reducing deployment shock angle. A deploying experiment is set up to verify the validation of the numerical models for the double-layer tape-spring hinge. The deployment shock angle and locked time are set as objectives, the thickness of outer and inner layer tape-spring on outer bending direction of the DLTS hinge are set as design variables. The modified non-dominated sorting genetic algorithm is employed to achieve the optimal design of the DLTS hinge. The finite element models for the non-equal thickness optimal design based on numerical method are established and validated the optimization results with relative errors no more than 5.008 %. Compared deployment behaviors between the non-equal thickness optimal design and equal thickness configuration for the DLTS hinge, the deployment shock angle and locked time for the former configuration are reduced by 52.154 % and 29.104 % respectively. The parameter study shows that the deployment shock angle is more sensitive to the outer layer thickness of tape-spring, and the locked time is first decreased and then increased with the thickness greater.
 

Key words

deployment shock / double-layer tape-spring hinge / dynamic analysis / optimization

Cite this article

Download Citations
YANG Hui, LIU Rong-qiang, WANG Yan, GUO Hong-wei, TAO Jian-guo. Dynamic analysis and optimization of double-layer tape-spring hinge[J]. Journal of Vibration and Shock, 2016, 35(9): 20-27

References

[1] LANE S A, MURPHEY T W, ZATMAN M. Overview of the innovative space-based radar antenna technology program [J]. Journal of Spacecraft and Rockets, 2011, 48(1): 135-145.
[2] ANON. Hughes graphite antennas installed on Mast-2 craft. Space News, Nov. 1994.
[3] ADAMS D S, MOBREM M. Lenticular jointed antenna deployment anomaly and resolution onboard the Mars Express Spacecraft [J]. Journal of Spacecraft and Rockets, 2009, 46(2): 403-410.
[4] SEFFEN K A, PELLEGRINO S. Deployment dynamics of tape springs [J]. Proceedings of the Royal Society of London, Series A: Mathematical and Physical Sciences, 1999, 455(1983): 1003-1048.
[5] SOYKASAP O. Deployment analysis of a self-deployable composite boom [J]. Composite Structures, 2009, 89: 374-381.
[6] YAO X F, MA Y J, YIN Y J, et al. Design theory and dynaimic mechanical characterization of the deployable composite tube hinge [J]. Science China: Physics, Mechanics and Astronomy, 2011, 54(4): 633-639.
[7] MALLIKARACHCHI H M Y C, PELLEGRINO S. Deployment dynamics of ultrathin composite booms with tape-spring hinges [J]. Journal of Spacecraft and Rockets, 2014, 51(2): 604-613.
[8] YANG H, LIU R Q, WANG Y, et al. Experiment and multiobjective optimization design of tape-spring hinge [EB/OL]. Structural and Multidisciplinary Optimization, 2014. The final publication is available at http://www. link.springer.com/article/10.1007/s00158-014-1205-9.
[9] YANG H, DENG Z Q, LIU R Q, et al. Optimizing the quasi-static folding and deploying of thin-walled tube flexure hinges with double slots [J]. Chinese Journal of Mechanical Engineering, 2014, 27(2): 279-286.
[10] MALLIKARACHCHI H M Y C, PELLEGRINO S. Quasi-static folding and deployment of ultrathin composite tape-spring hinges [J]. Journal of Spacecraft and Rockets, 2011, 48(1): 187–198.
[11] HOU S J, LIU T Y, DONG D, et al. Factor screening and multivariable crashworthiness optimization for vehicle side impact by factorial design [J]. Structural and Multidisciplinary Optimization, 2014, 49:147-167.
[12] LI M, DENG Z Q, GUO H W, et al. Crashworthiness analysis on alternative square honeycomb structure under axial loading [J]. Chinese Journal of Mechanical Engineering, 2013, 26(4): 784-792.
[13] Deb K, Pratap A, Agarwal S, Meyarivan T. A fast and elitist multiobjective genetic algorithm: NSGA-II [J]. IEEE Transactions on Evolutionary Computation, 2002, 6(2): 182–97.
 
 
PDF(1985 KB)

781

Accesses

0

Citation

Detail

Sections
Recommended

/