发明名称 LAUNCH LOCK ASSEMBLIES WITH REDUCED PRELOAD AND SPACECRAFT ISOLATION SYSTEMS INCLUDING THE SAME
摘要 Launch lock assemblies with reduced preload are provided. The launch lock assembly comprises first and second mount pieces, a releasable clamp device, and a pair of retracting assemblies. Each retracting assembly comprises a pair of toothed members having interacting toothed surfaces. The releasable clamp device normally maintains the first and second mount pieces in clamped engagement. When the releasable clamp device is actuated, the first and second mount pieces are released from clamped engagement and one toothed member of each retracting assembly moves in an opposite direction relative to the other one toothed member of the other retracting assembly to define an axial gap on each side of the first mount piece.
申请公布号 US2014084113(A1) 申请公布日期 2014.03.27
申请号 US201213626843 申请日期 2012.09.25
申请人 HONEYWELL INTERNATIONAL INC. 发明人 BARBER TIM DANIEL;YOUNG KEN;HINDLE TIMOTHY
分类号 B64G1/66 主分类号 B64G1/66
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