Power plants – Reaction motor – Interrelated reaction motors
Patent
1992-11-24
1993-11-16
Vrablik, John J.
Power plants
Reaction motor
Interrelated reaction motors
602263, F02K 302
Patent
active
052612279
ABSTRACT:
An aircraft turbofan engine and method of operation effect variable specific thrust. The engine includes a fan disposed in a fan casing and a booster compressor disposed in a first flow splitter and powered by a core engine. A second flow splitter is disposed inside the fan casing and defines fan outer and inner ducts. The booster compressor includes at least one stage of rotor blades each having a shroud and an integral rotor flade extending radially outwardly therefrom into the fan inner duct. The fan outer duct includes a variable area first exhaust nozzle disposed at an aft end of the fan casing and is positionable in a first position to permit shifting of a portion of the fan air from the outer duct to the inner duct for flow between the flades to vary specific thrust of the engine.
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General Electric Company, "Quite Clean Short-Haul Experimental Engine (QCSEE) Preliminary Analyses and Design Report, vol. I," Oct. 1974, pp: cover, 13, 14, 17, 19, 140, 143, 151, and 183.
General Electric Company
Squillaro Jerome C.
Vrablik John J.
Wicker W. J.
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