Supports – With condition responsive control means
Patent
1984-02-15
1986-04-15
Britts, Ramon S.
Supports
With condition responsive control means
2483164, F16M 1300
Patent
active
045822891
ABSTRACT:
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).
REFERENCES:
patent: 1337484 (1920-04-01), Ruoff
patent: 2727325 (1955-12-01), Jurinic
patent: 3050301 (1962-08-01), Palazzolo
patent: 3493233 (1970-02-01), Foufounis
patent: 3844177 (1974-10-01), Bourassa
patent: 4448406 (1984-05-01), Hallberg et al.
Calvert John A.
Cloyd Richard A.
Gibson John C.
Nesmith Malcolm F.
Beumer Joseph H.
Britts Ramon S.
Manning John R.
Ramirez Ramon O.
The United States of America as represented by the Administrator
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