Fan duct thrust reverser

Details Fan duct thrust reverser Fan duct thrust reverser

1975-12-22

1977-02-01

Blix, Trygve M.

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

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

244110B, 60226A, B64C 1506

Patent

active

040058220

ABSTRACT:
A thrust reverser arrangement for a fan-type jet propulsion engine comprising a split cowling surrounding the engine and forming a bypass duct with the engine outer wall. The rear portion of the split cowling is translatable rearward for forming a space between the cowling portions. A translatable sleeve having cascades through portions of its walls is interconnected with the rear portion of the cowling and translates therewith and fills the space between the cowling portions. Blocker doors are interconnected to the rear portion and are rotated into the bypass duct during the terminal rearward movement of the rear portion.

REFERENCES:
patent: 2950595 (1960-08-01), Laucher et al.
patent: 3497165 (1970-02-01), Sutton et al.
patent: 3503211 (1970-03-01), Medawar et al.
patent: 3612402 (1971-10-01), Timms et al.
patent: 3829020 (1974-08-01), Stearns
patent: 3941313 (1976-03-01), Jumelle

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