Turbofan engine with flexible, variable area nozzle

Power plants – Reaction motor – Interrelated reaction motors

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Details

60271, F02K 110, F02K 306

Patent

active

039674436

ABSTRACT:
A fluid flow duct of a gas turbine engine, the duct being defined between a fan cowl and a centerbody and there being provided movable flexible members attached to the centerbody, each member being movable within the duct by fluid pressure between a first concave position and a second convex position for varying the cross-sectional flow area of the duct.

REFERENCES:
patent: 2623352 (1952-12-01), Sedille et al.
patent: 2629569 (1953-02-01), Andrews
patent: 3258913 (1966-07-01), Moorehead
patent: 3279192 (1966-10-01), Hull et al.
patent: 3380663 (1968-04-01), Jumelle
patent: 3729934 (1973-05-01), Denning et al.
patent: 3756026 (1973-09-01), Timms et al.

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