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    • 2. 发明授权
    • Space solar array architecture for ultra-high power applications
    • 太阳能阵列架构适用于超大功率应用
    • US09120583B1
    • 2015-09-01
    • US13447166
    • 2012-04-14
    • Brian R SpenceSteven F WhitePeter Sorenson
    • Brian R SpenceSteven F WhitePeter Sorenson
    • B64G1/22B64G1/44
    • B64G1/443B64G1/222B64G1/44H02S30/20
    • A large area, deployable flexible blanket photovoltaic solar array architecture for high power applications is disclosed. The structure is a modularized and scalable solar array system that provides high power level scalability. The structure is comprised of repeating, similar modular deployable roll-out solar array wings mounted in an opposing manner and along the length of a rigid, strong and efficiently packaged deployable backbone structure. The deployable roll-out solar array building block modular “winglet” elements can be comprised of either a rolled or z-folded flexible photovoltaic blanket configuration, and their structural deployment is motivated by the elastic strain energy of longitudinal roll-out booms. The backbone structure is comprised of a stiff deployable beam structure articulated that is deployed perpendicular with respect to the spacecraft sidewall and latched out. Deployment of the “winglets” can be conducted once the articulated backbone structure has been deployed, is latched, and forms a rigid beam.
    • 公开了用于大功率应用的大面积可部署的柔性毯式光伏太阳能阵列架构。 该结构是一个模块化和可扩展的太阳能阵列系统,提供高功率水平的可扩展性。 该结构由重复的相似的模块化展开式推出的太阳能阵列翼片组成,它们以相对的方式安装,并沿着刚性,强力和有效地封装的可部署骨架结构的长度。 可部署的推出式太阳能阵列构件块模块化“小翼”元件可以由轧制或z折叠的柔性光伏电池组件构成,并且其结构部署由纵向推出臂的弹性应变能量驱动。 骨架结构包括一个铰接的刚性可展开的梁结构,该梁结构相对于航天器侧壁垂直展开并锁定。 一旦关节骨干结构已经部署,被锁定并形成刚性梁,就可以进行“小翼”的部署。