Linkage system for an aircraft turbojet engine

Details Linkage system for an aircraft turbojet engine Linkage system for an aircraft turbojet engine

1997-11-28

2000-03-07

Barefoot, Galen L.

Aeronautics and astronautics

Aircraft structure

Details

292 34, B64C 114

Patent

active

060329017

ABSTRACT:
A linkage system is disclosed for releasably latching a thrust reverser to an engine casing having a longitudinal axis, the linkage system having a seat on the thrust reverser and a movable latching member on the engine casing movable between an open position in which the latching member is displaced away from the seat, and a closed position in which the latching member is located adjacent to the seat so as to prevent displacement of the thrust reverser away from the engine casing.

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patent: 4555078 (1985-11-01), Grognard
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patent: 4679750 (1987-07-01), Burhans
patent: 4793643 (1988-12-01), Ahad et al.
patent: 5378029 (1995-01-01), Hoffeins
patent: 5775639 (1998-07-01), Fage

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