Thrust reverser/exhaust nozzle assembly for a gas turbine engine

Details Thrust reverser/exhaust nozzle assembly for a gas turbine engine Thrust reverser/exhaust nozzle assembly for a gas turbine engine

1984-05-16

1986-05-27

Peters, Jr., Joseph F.

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

60230, 23926541, B64C 1500

Patent

active

045910979

ABSTRACT:
An improved thrust reverser/exhaust nozzle assembly has a plurality of blocker devices located in the divergent section of the exhaust nozzle and a plurality of deflector devices located in the convergent section of the nozzle. The blocker and deflector devices are linked together such that they move simultaneously and maintain a substantially constant engine flowrate during transitions of the engine between forward and reverse thrust conditions.

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patent: 3739582 (1973-06-01), Maison
patent: 3973731 (1976-08-01), Thayer
patent: 4375276 (1983-03-01), Konarski
patent: 4382551 (1983-05-01), Thayer
patent: 4502637 (1985-03-01), Nightingale

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