发明名称 Self indexing latch system
摘要 A self-latching jaw assembly is illustrated which includes a pair of latching jaws (A) and (B) for latching a fitting of an associated structure such as the keel fitting (50) of a space telescope. The jaw assembly automatically locates the fitting received on a positioning pedestal (52) and latches it in its original location on the pedestal without need of precision alignment. The first jaw (A) is actuated and moved to the right whereupon a reciprocating plunger (62) will have been extended from the nose (64) of the jaw and will sense the hub (50b) of the spool (50a). A jaw position responsive switch (72) is then actuated to terminate the drive motor (E) of the jaw (A). The astronaut will then actuate the drive motor (F) of the jaw (B) and the jaw will move to the left whereupon standoff (82) will engage the face (64a) of the jaw (A) in a latching position. In the latching position, the noses (64) and (83) of the jaws (A) and (B) will be under the flanges of the spool (50a).
申请公布号 US4582289(A) 申请公布日期 1986.04.15
申请号 US19840580397 申请日期 1984.02.15
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 GIBSON, JOHN C.;CALVERT, JOHN A.;NESMITH, MALCOLM F.;CLOYD, RICHARD A.
分类号 B25B1/10;B25B1/18;B25B1/24;B64G1/66;F16B1/00;(IPC1-7):F16M13/00 主分类号 B25B1/10
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