发明名称 Simplified spacecraft antenna reflector for stowage in confined envelopes
摘要 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.
申请公布号 US5574472(A) 申请公布日期 1996.11.12
申请号 US19950491331 申请日期 1995.06.30
申请人 HUGHES ELECTRONICS 发明人 ROBINSON, STEPHEN A.
分类号 H01Q1/08;B64G1/22;H01Q1/28;H01Q15/16;H01Q15/20;(IPC1-7):H01Q15/20 主分类号 H01Q1/08
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