发明名称 Simplified spacecraft antenna reflector for stowage in confined envelopes
摘要 <p>A method for stowing a unitary flexible antenna reflector 10 in a confining envelope and deploying the reflector from the envelope. In a most general sense, the invention includes the steps of: a) applying a deforming force to diametrically opposed positions 16 and 18 near an edge of the reflector 10 to place the reflector in a deformed state; b) maintaining the reflector 10 in the deformed state until deployment; and c) releasing the reflector 10 from the deformed state. In a specific embodiment, the step of maintaining the reflector 10 in a deformed state includes the step of attaching a restraining element between the diametrically opposed positions on the edge of the reflector which is released on deployment. <IMAGE></p>
申请公布号 EP0534110(B1) 申请公布日期 1996.06.12
申请号 EP19920113600 申请日期 1992.08.10
申请人 HUGHES AIRCRAFT COMPANY 发明人 ROBINSON, STEPHEN A.
分类号 H01Q1/08;B64G1/22;H01Q1/28;H01Q15/16;H01Q15/20;(IPC1-7):H01Q15/16 主分类号 H01Q1/08
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