Thrust deflection

Details Thrust deflection Thrust deflection

1984-06-26

1986-10-21

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

With means controlling amount, shape or direction of...

23926519, 239503, 239512, 60230, B64C 938, F02K 162

Patent

active

046180940

ABSTRACT:
A gas turbine engine which is used for aircraft propulsion, is provided with a pair of thrust deflecting doors which, when deployed, deflect the exhaust gases onto some path other than axially of the engine, so as to spoil the thrust. The doors are waisted in profile. To prevent some of the exhaust gases from missing the doors, when deployed, and thus reducing their functional efficiency, plane flaps are provided on the jet pipe, which can be moved into the gas stream when the doors are deployed. The gas stream is thus constricted and so remains within the bounds of the deployed doors.

REFERENCES:
patent: 2972860 (1961-02-01), Moy
patent: 3984974 (1976-10-01), Medawar et al.
patent: 4052007 (1977-10-01), Willard
patent: 4147027 (1979-04-01), Greathouse

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