Variable specific thrust turbofan engine

Power plants – Reaction motor – Interrelated reaction motors

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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.

REFERENCES:
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patent: 3867813 (1975-02-01), Leibach
patent: 4043121 (1977-08-01), Thomas et al.
patent: 4050242 (1977-09-01), Dusa
patent: 4055042 (1977-10-01), Colley
patent: 4080785 (1978-03-01), Koff
patent: 4288983 (1981-09-01), O'Rourke, Jr.
W. S. Willis, "Quiet Clean Short-Haul Experimental Engine (QCSEE) Final Report," Aug. 1979, pp. cover, 15, and 17.
General Electric Company, "Quite Clean Short-Haul Experimental Engine (QCSEE) UTW Fan Preliminary Design," Feb. 1975, pp: cover, 2 and 3.
General Electric Company, "Quiet Clean Short-Haul Experimental Engine (QCSEE) Preliminary Analyses and Design Report, vol. II" Oct. 1974, pp: cover, 465, 477, 478, 517, 522, and 523.
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.

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