发明名称 Niederhalte- und Auslösevorrichtung für entfaltbare Satellitenkomponenten
摘要 The invention relates to a hold-down and triggering device (1) for holding a hold-down pin (6) in a positive fit and triggering said pin which is used for components of a satellite which are to be folded out. Said device comprises a housing (2) having a sleeve (3) that is arranged therein. The sleeve is formed by at least two sleeve components (3a, 3b) which are wound with a bandage (29) consisting of optionally conglutinated fibres. The sleeve components are preferably prestressed against the housing (2). At least one triggering element (30) comprising a cutting edge (37) is arranged at the housing (2). The cutting edge (37) is moved in direction towards the bandage (29) by means of a control setting in order to cut said bandage (29).
申请公布号 DE19856446(A1) 申请公布日期 2000.06.21
申请号 DE19981056446 申请日期 1998.12.08
申请人 DAIMLERCHRYSLER AG 发明人 PFEFFERKORN, DIETER
分类号 B64G1/22;B64G1/44;B64G1/64;(IPC1-7):B64G1/42 主分类号 B64G1/22
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