发明名称 Satellite solar generator panel deployment device
摘要 The device allows a pair of solar generator panels (2,3) which are hinged together to be opened out from a folded position into a deployed position via an operating cable (13) passed around a cable disc (11) coupled to the hinge axis (4). The cable disc is separated from the hinge axis after deployment of the solar generator panels by rotation of one of the panels (3) about the hinge axis, to allow rotation of this panel via an electric setting motor fitted to the hinge axis for tracking the position of the sun.
申请公布号 DE19610297(C1) 申请公布日期 1997.01.23
申请号 DE1996110297 申请日期 1996.03.15
申请人 DAIMLER-BENZ AEROSPACE AKTIENGESELLSCHAFT, 80804 MUENCHEN, DE 发明人 STICH, WALTER, DIPL.-ING., 83714 MIESBACH, DE;STOECKLE, AXEL, DIPL.-ING., 81739 MUENCHEN, DE
分类号 B64G1/22;B64G1/44;(IPC1-7):B64G1/44;F16H19/00;H01L31/045 主分类号 B64G1/22
代理机构 代理人
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