Thrust reversal device for air-craft turbojets

Details Thrust reversal device for air-craft turbojets Thrust reversal device for air-craft turbojets

1982-05-25

1984-12-04

Love, John J.

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

602262, 244110B, F02K 162

Patent

active

044859708

ABSTRACT:
The invention relates to thrust reversal devices for jet aircraft turboreactors and particularly for a turbo-fan type engine.
The casing E surrounding the engine structure D comprises an intermediate section S3 formed by doors P4 pivoting about an axis 17-17' extending along a chord of passage CA so that the rear part of the door is short, which provides considerable clearance for the doors which may open up to 90.degree., as well as an action of flux F1 flowing in the passage promoting opening of the doors. A jack 21 coupled to each of the doors acts between the fixed structure of the casing and the internal part of the door.

REFERENCES:
patent: 3279182 (1966-10-01), Helmintoller
patent: 3475913 (1969-11-01), Mortlock et al.
patent: 3531049 (1970-09-01), Hom
patent: 3601992 (1970-08-01), Maison
patent: 3647141 (1972-03-01), Murday
patent: 3699682 (1972-10-01), Kleckner
patent: 3764096 (1973-10-01), Wright
patent: 4052007 (1977-10-01), Willard

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