发明名称 |
Sheath-Based Rollable Lenticular-Shaped and Low-Stiction Composite Boom |
摘要 |
Various embodiments provide rollable and deployable composite booms that may be used in a wide range of applications both for space and terrestrial structural solutions. Various embodiment composite booms may be bistable, i.e. having a stable strain energy minimum in the coiled configuration as well as the in the deployed configuration. In various embodiments, a boom may be fabricated by aligning two independent tape-springs front-to-front encircled by a durable seamless polymer sleeve. The durable seamless polymer sleeve may allow the two tape-springs to slide past each other during the coiling/deployment process so as to reduce, e.g., minimize, shear and its derived problems. |
申请公布号 |
US2017058524(A1) |
申请公布日期 |
2017.03.02 |
申请号 |
US201615245515 |
申请日期 |
2016.08.24 |
申请人 |
U.S.A. as represented by the Administrator of the National Aeronautics and Space Administration |
发明人 |
Fernandez Juan M. |
分类号 |
E04C3/00;B29C65/48;B64G1/22 |
主分类号 |
E04C3/00 |
代理机构 |
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代理人 |
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主权项 |
1. A composite boom, comprising:
a polymer sleeve; a first tape-spring; and a second tape-spring, wherein:
the first and second tape-springs are encircled by the polymer sleeve without being structurally affixed together; andthe first and second tape-springs slide relative to one another inside the polymer sleeve during coiling and deployment of the bistable composite boom. |
地址 |
Washington DC US |