Dual-purpose ejector for aircraft load jettisoning mechanism

Details Dual-purpose ejector for aircraft load jettisoning mechanism Dual-purpose ejector for aircraft load jettisoning mechanism

1976-11-08

1978-07-25

Blix, Trygve M.

Aeronautics and astronautics

Aircraft structure

Passenger or cargo loading or discharging

89 15B, 89 15G, 294 83AB, B64D 102

Patent

active

041025202

ABSTRACT:
An ejector serves for suspending under aircraft loads which have suspension rings or saddle members, both of known kind. The ejector includes a carrier device which has, for each load suspension point, a first pivoted hook which can coact with a saddle member, a fastener disposed adjacent to the first hook, and a detachable device removably mounted in the fastener, the detachable device having a housing for receiving the upper part of a suspension ring, a second hook pivotable about a horizontal pin and serving, in a closed position, to lock the suspension ring in the housing, and a spring urging the second hook against the first hook so that the second hook follows opening and closing movements of the first hook and is itself thereby moved into opening and closing positions.

REFERENCES:
patent: 3503576 (1970-03-01), Savarieau
patent: 3854680 (1974-12-01), Hasquenoph et al.
patent: 3954233 (1976-05-01), Hasquenoph et al.
patent: 3967528 (1976-07-01), Baker

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