发明名称 Reflector surface adjustment structure
摘要 Rear and forward reflector shells or dishes (36,38) are independently supported on a dynamically rigid truss structure (12) by means of separate studs extending from the forward nodes of the truss to the two shells. Forward node (22) carries adjustable rear shell stud (52) and independently carries adjustable forward shell stud (80). Both of the studs have flat portions oriented normal to the radius of the shell so that radial shell expansion due to temperature and temperature differential minimize shell distortion.
申请公布号 US4845510(A) 申请公布日期 1989.07.04
申请号 US19870083489 申请日期 1987.08.10
申请人 HUGHES AIRCRAFT COMPANY 发明人 CHANG, STANLEY S.;YBARRA-ROJAS, AMILCAR B.;BAU, HUI
分类号 H01Q15/14;H01Q3/20;H01Q15/16 主分类号 H01Q15/14
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