发明名称 CAPTIVE CABLE COIL AND ITS APPLICATION TO A REGULATOR FOR DEPLOYING A LENGTHENING PIECE OF A SPACE INSTRUMENT
摘要 So as to adjust the deployment of a lengthening piece of a space instrument, a captive cable coil (34) coupled to a centrifugal brake by a speed multiplier is used. The cable (40) is wound onto the coil (34) in the form of a single strand imprisoned in a roughly helical-shaped throat (38) formed, for example by machining, on the outer surface of the coil. One outer portion (42a) of the partition separating two adjacent spires of the throat is folded down onto the cable so as to prevent its volume from swelling. Fig. 2 SP 6158.69 GP
申请公布号 CA2042637(A1) 申请公布日期 1991.11.19
申请号 CA19912042637 申请日期 1991.05.15
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 HENRY, JEAN-PIERRE
分类号 B64G1/44;B64G1/22;B65H75/14;B65H75/18;B65H75/26;(IPC1-7):B64G1/66;B64G9/00 主分类号 B64G1/44
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