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 代理人
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
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