Gas turbine engine thrust reverser

Details Gas turbine engine thrust reverser Gas turbine engine thrust reverser

1986-08-12

1988-03-22

Casaregola, Louis J.

Power plants

Reaction motor

Interrelated reaction motors

23926531, F02K 302

Patent

active

047319917

ABSTRACT:
A ducted fan gas turbine engine is provided with a fan cowling member made up of a static portion and an axially translatable portion. A plurality of rails interconnect the first and second cowling member portions and carry a generally annular array of airflow deflector vanes. The deflector vanes are normally stowed in stacked relationship when the cowling portions are contiguous but are equally axially spaced apart to define a fan air flow thrust reverser when the second cowling portion has been translated to a position downstream of the first cowling portion.

REFERENCES:
patent: 3262270 (1966-07-01), Beavers
patent: 3262271 (1966-07-01), Beavers
patent: 3779010 (1973-12-01), Chamay et al.
patent: 4026105 (1977-05-01), James
patent: 4030290 (1977-06-01), Stachowiak
patent: 4030291 (1977-06-01), Sargisson

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