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Space solar array architecture for ultra-high power applications

机译:适用于超高功率应用的太空太阳能阵列架构

摘要

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.
机译:公开了一种用于大功率应用的大面积,可部署的柔性毯状光伏太阳能阵列结构。该结构是提供高功率级别可扩展性的模块化可扩展太阳能阵列系统。该结构由重复的,类似的模块化可展开式太阳能阵列机翼组成,这些机翼以相反的方式并沿着刚性,坚固且有效包装的可展开主干结构的长度方向安装。可展开的太阳能电池阵列构建模块模块化“小翼”元件可以由滚动的或Z形折叠的柔性光伏毯配置组成,其结构展开是由纵向展开吊臂的弹性应变能驱动的。骨架结构由铰接的刚性可展开梁结构组成,该结构相对于航天器侧壁垂直展开并被闩锁。一旦铰接的骨架结构已经展开,被闩锁并形成刚性梁,就可以进行“小翼”的展开。

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