发明名称 Modular Self-Tracking Micro-Concentrator For Space Power
摘要 Technologies for a micro-concentrator modular array. The micro-concentrator modular array may include two or more micro-concentrator solar modules. One or more of the micro-concentrator solar modules may be removable from the micro-concentrator modular array. Micro-concentrator solar modules may be added to a micro-concentrator modular array. One or more of the micro-concentrator solar modules may be electrically and/or mechanically connected to other micro-concentrator solar modules. To facilitate an electrical connection, a conductive connector may be used to connect an electrical output of one micro-concentrator solar module with an electrical input of another micro-concentrator solar module.
申请公布号 US2015243822(A1) 申请公布日期 2015.08.27
申请号 US201414534261 申请日期 2014.11.06
申请人 The Boeing Company 发明人 Karam Nasser H.;Singer Scott B.;Krut Dimitri
分类号 H01L31/054;H01L31/05;H01L31/18;H02S50/10 主分类号 H01L31/054
代理机构 代理人
主权项 1. A micro-concentrator modular array (300), comprising: a plurality of micro-concentrator solar modules (10), each of the plurality of micro-concentrator solar modules (10) comprising a plurality of solar cells (22), wherein at least two of the plurality of micro-concentrator solar modules (10) comprises a connector pad (304) configured to facilitate a connection with an adjacent micro-concentrator solar module (10); and a connector (68) configured to removably engage connector pads (304) of two adjacent micro-concentrator solar modules (10) to connect the two adjacent micro-concentrator solar modules (10).
地址 Chicago IL US