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 |
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代理人 |
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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 |