Bistable tape springs are ultrathin fiber-reinforced polymer composites, which could self-deploy through releasing stored strain energy. Strain energy relaxation is observed after long-term stowage of bistable tape springs due to viscoelastic effects and the tape springs might lose their self-deployment abilities. In order to mitigate the viscoelastic effects and thus ensure self-deployment, different tape springs were designed, manufactured, and tested. Deployment experiments show that a four-layer, [−45/0/90/45], plain weave glass fiber tape spring has a high capability to mitigate the strain energy relaxation effects to ensure self-deployment after long-term stowage in a coiled configuration. The two inner layers increase the deployment force and the outer layers are used to generate the bistability. The presented four-layer tape spring can self-deploy after more than six months of stowage at room temperature. A numerical model was used to assess the long-term stowage effects on the deployment capability of bistable tape springs. The experiments and modeling results show that the viscoelastic strain energy relaxation starts after only a few minutes after coiling. The relaxation shear stiffness decreases as the shear strain increases and is further reduced by strain energy relaxation when a constant shear strain is applied. The numerical model and experiments could be applied in design to predict the deployment force of other types of tape springs with viscoelastic and friction effects included.
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July 2017
Research-Article
Design and Analysis of Laminates for Self-Deployment of Viscoelastic Bistable Tape Springs After Long-Term Stowage
Huina Mao,
Huina Mao
Department of Aeronautical and
Vehicle Engineering,
KTH Royal Institute of Technology,
Stockholm 100 44, Sweden
e-mail: huina@kth.se
Vehicle Engineering,
KTH Royal Institute of Technology,
Stockholm 100 44, Sweden
e-mail: huina@kth.se
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Anton Shipsha,
Anton Shipsha
Department of Aeronautical and
Vehicle Engineering,
KTH Royal Institute of Technology,
Stockholm 100 44, Sweden
e-mail: shipsha@kth.se
Vehicle Engineering,
KTH Royal Institute of Technology,
Stockholm 100 44, Sweden
e-mail: shipsha@kth.se
Search for other works by this author on:
Gunnar Tibert
Gunnar Tibert
Department of Aeronautical and
Vehicle Engineering,
KTH Royal Institute of Technology,
Stockholm 100 44, Sweden
e-mail: tibert@kth.se
Vehicle Engineering,
KTH Royal Institute of Technology,
Stockholm 100 44, Sweden
e-mail: tibert@kth.se
Search for other works by this author on:
Huina Mao
Department of Aeronautical and
Vehicle Engineering,
KTH Royal Institute of Technology,
Stockholm 100 44, Sweden
e-mail: huina@kth.se
Vehicle Engineering,
KTH Royal Institute of Technology,
Stockholm 100 44, Sweden
e-mail: huina@kth.se
Anton Shipsha
Department of Aeronautical and
Vehicle Engineering,
KTH Royal Institute of Technology,
Stockholm 100 44, Sweden
e-mail: shipsha@kth.se
Vehicle Engineering,
KTH Royal Institute of Technology,
Stockholm 100 44, Sweden
e-mail: shipsha@kth.se
Gunnar Tibert
Department of Aeronautical and
Vehicle Engineering,
KTH Royal Institute of Technology,
Stockholm 100 44, Sweden
e-mail: tibert@kth.se
Vehicle Engineering,
KTH Royal Institute of Technology,
Stockholm 100 44, Sweden
e-mail: tibert@kth.se
1Corresponding author.
Manuscript received March 2, 2017; final manuscript received May 1, 2017; published online May 22, 2017. Assoc. Editor: Nick Aravas.
J. Appl. Mech. Jul 2017, 84(7): 071004 (10 pages)
Published Online: May 22, 2017
Article history
Received:
March 2, 2017
Revised:
May 1, 2017
Citation
Mao, H., Shipsha, A., and Tibert, G. (May 22, 2017). "Design and Analysis of Laminates for Self-Deployment of Viscoelastic Bistable Tape Springs After Long-Term Stowage." ASME. J. Appl. Mech. July 2017; 84(7): 071004. https://doi.org/10.1115/1.4036672
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