Jet engine provided with a thrust reverser

Details Jet engine provided with a thrust reverser Jet engine provided with a thrust reverser

1990-08-24

1993-03-09

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Processes

Of discharge modification of flow varying

23926529, 23926537, 244110B, F02K 110, F02K 112

Patent

active

051920239

ABSTRACT:
A jet engine for an aircraft has a thrust reverser including one or more doors which define at least a part of the throat of the engine's nozzle. The engine further includes a latch mechanism for retaining the doors in a stowed position. The doors may be deployed for reversal of engine thrust, but are also capable while stowed of being pivoted in a limited way to change the cross-section area of the throat of the nozzle.

REFERENCES:
patent: 2481330 (1949-09-01), Neal
patent: 2735264 (1956-02-01), Jewett
patent: 4093122 (1978-06-01), Linderman
patent: 4194692 (1980-03-01), Dickenson
patent: 4605169 (1986-08-01), Mayers
patent: 4641782 (1987-02-01), Woodward
patent: 4819876 (1989-04-01), Thayer
patent: 4966327 (1990-10-01), Fage et al.

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