Turbojet engine thrust reverser with asymmetrical doors

Details Turbojet engine thrust reverser with asymmetrical doors Turbojet engine thrust reverser with asymmetrical doors

1996-07-08

1998-03-17

Freay, Charles G.

Power plants

Reaction motor

With thrust direction modifying means

602262, 23926527, F02K 100

Patent

active

057273804

ABSTRACT:
A thrust reverser is disclosed for a turbofan-type turbojet engine having a cowling bounding a gas flow duct in which the thrust reverser has a plurality of thrust reverser doors each pivotally attached to the cowling so as to be movable between a forward thrust position and a reverse thrust position which redirects the gases passing through the gas flow duct outwardly from the cowling to produce a reverse thrust. At least one of the plurality of thrust reverser doors having a width, measured in a generally circumferential direction around the cowling, less than a corresponding width of at least one of the other thrust reverser doors.

REFERENCES:
patent: 3097484 (1963-07-01), Andre et al.
patent: 3279182 (1966-10-01), Helmintoller
patent: 3605411 (1971-09-01), Maison et al.
patent: 3640468 (1972-02-01), Searle et al.
patent: 4410152 (1983-10-01), Kennedy et al.
patent: 4462207 (1984-07-01), Hitchcock
patent: 4894985 (1990-01-01), Dubois et al.
patent: 5230213 (1993-07-01), Lawson
patent: 5284015 (1994-02-01), Carimali et al.
patent: 5297387 (1994-03-01), Carimali et al.

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