Exhaust nozzle with reverser exhaust door mechanism

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle – With means controlling amount – shape or direction of...

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60230, 23926533, F02K 162, F02K 112

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active

050925253

ABSTRACT:
A convergent/divergent gas turbine engine exhaust nozzle having reverse thrust capability includes a door which blocks a reverse flow outlet port when the nozzle convergent flap is in any forward thrust operating mode. The door is coupled to the convergent nozzle flap such that it opens as the convergent nozzle flap moves to a reverse thrust position and the flap directs the exhaust gases through the reverser outlet. Coupling is accomplished by a cam track connected to the blocker door and a cam track connected to the convergent flap, with a cam follower interconnecting the two cam tracks. As the convergent flap is rotated, the cams and cam follower cause appropriate movement of the blocker door.

REFERENCES:
patent: 3655133 (1972-04-01), Medamar et al.
patent: 3831376 (1974-08-01), Moorehead
patent: 4074859 (1978-02-01), Lowman
patent: 4340178 (1982-07-01), Lawson
patent: 4463903 (1984-08-01), Nightengale
patent: 4502637 (1985-03-01), Nightingale

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