发明名称 Docking system
摘要 A convex forward surface of a forward-biased probe head of a first portion of a docking system engages a central concave conical surface of a second portion of the docking system. A first linear actuator moves a flexible docking cable assembly relative to a support structure through bores therein and through the probe head. An aftward retraction of the docking cable assembly causes a linearly-actuated cam element thereof to rotate a rotary cam follower pivoted from the support structure, which engages an aft edge portion of the probe head, forcing the probe head forward. A plurality of distal coupling elements operatively coupled to the support structure around a central axis thereof engage with and become releasably captured by a corresponding socket and associated capture mechanism of a mating second portion of the docking system, and rigidized when the probe head is forced against the central concave conical surface.
申请公布号 US7861974(B2) 申请公布日期 2011.01.04
申请号 US20090406955 申请日期 2009.03.18
申请人 MICHIGAN AEROSPACE CORPORATION 发明人 HAYS ANTHONY BECKMAN;RITTER GREG ALAN;TCHORYK, JR. PETER;PAVLICH JANE CAMILE;WASSICK GREGORY JOSEPH
分类号 B64G1/64 主分类号 B64G1/64
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