Thrust reverser for a long duct fan engine

Aeronautics and astronautics – Retarding and restraining devices – Friction brakes

Patent

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Details

60226A, B64C 2568, B64F 102

Patent

active

042782201

ABSTRACT:
A bypass duct outer cowl includes a fixed cascade disposed between axially spaced fixed cowl portions and a translatable cowl sleeve and blocker doors movably disposed on the respective radially outer and inner sides of the cascade. Actuation and linkage structure located entirely within the outer cowl provides for selectively moving the cowl sleeve rearwardly and rotating the blocker doors to a position across the bypass duct to cause the fan airflow to pass through the cascade in a thrust-reversing manner.

REFERENCES:
patent: 3262268 (1966-07-01), Beavers
patent: 3280561 (1966-10-01), Kutney
patent: 3347467 (1967-10-01), Carl et al.
patent: 3511055 (1970-05-01), Timms
patent: 3608314 (1971-09-01), Colley
patent: 3691771 (1972-09-01), Colley
patent: 3779010 (1973-12-01), Chamay et al.
patent: 3820719 (1974-06-01), Clark
patent: 4030291 (1977-06-01), Sargisson

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