Thrust reverser for a jet engine, more especially for equipping

Details Thrust reverser for a jet engine, more especially for equipping Thrust reverser for a jet engine, more especially for equipping

1981-07-01

1983-10-18

Barefoot, Galen L.

Aeronautics and astronautics

Retarding and restraining devices

Friction brakes

23926527, 23926519, 602262, B64C 1500, F02K 306

Patent

active

044101520

ABSTRACT:
The engine is of the type having a central body surrounded by a casing defining therebetween a duct for the passage of the flux. The casing comprises a fixed upstream section extended downstream by means in which are housed jacks; a downstream section movable axially to which are fixed the rods of the jacks; and an intermediate section formed of swinging doors mounted between the beams and hinged thereto by lateral pivots, each door being coupled to the mobile downstream section by means of a hinged link so that the movement of the downstream section causes the doors to swing. This type of reverser is designed more especially for turbo-fan engines having a lateral nacelle configuration in which the whole of the flux flows in the annular duct between the central body and the casing.

REFERENCES:
patent: 3050937 (1962-08-01), James et al.
patent: 3097484 (1963-07-01), Andre et al.
patent: 3279182 (1966-10-01), Helmintoller
patent: 3492821 (1970-02-01), Monaghan et al.
patent: 3599874 (1971-08-01), Horn
patent: 3601992 (1971-08-01), Maison
patent: 3605411 (1971-09-01), Maison et al.
patent: 3665709 (1972-05-01), Medawar et al.
patent: 3684183 (1972-08-01), Baerresen
patent: 4073440 (1978-02-01), Hapke

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