发明名称 |
Assembly and mounting of solar cells on space panels |
摘要 |
The present disclosure provides a method of fabricating a solar cell panel in an automated process by applying an adhesive pattern to a support, positioning a solar cell assembly over the pattern, and applying pressure to adhere the assembly to the support. |
申请公布号 |
US9608156(B2) |
申请公布日期 |
2017.03.28 |
申请号 |
US201514795461 |
申请日期 |
2015.07.09 |
申请人 |
SolAcro Technologies Corp. |
发明人 |
Clevenger Marvin B.;Richards Benjamin C.;Tourino Cory |
分类号 |
H01L21/00;H01L31/0725;H01L31/041;H01L31/0735;H01L31/048;H01L31/0304;H01L31/074;H01L31/18;H01L31/049 |
主分类号 |
H01L21/00 |
代理机构 |
|
代理人 |
|
主权项 |
1. A method of fabricating a solar cell array carrier comprising:
providing a support for mounting an array of solar cells; providing a pattern of a plurality of discrete predefined adhesive regions on a top surface of the support; positioning a single solar cell assembly of a plurality of solar cell assemblies over the top surface of each adhesive region; bonding each solar cell assembly of the plurality of solar cell assemblies to each region by application of pressure; and electrically connecting each solar cell assembly to an adjoining solar cell assembly subsequent to the bonding step to form at least a string of electrically interconnected solar cell assemblies, wherein electrically connecting each solar cell assembly to an adjoining solar cell assembly comprises: automatically positioning an interconnector using a pick and place process; and welding the placed interconnector using automatic parallel gap welding. |
地址 |
Albuquerque NM US |