Turbine engines

Details Turbine engines Turbine engines

1974-07-10

1976-05-11

Blix, Trygve M.

Aeronautics and astronautics

Aircraft power plants

60262, B64D 2716

Patent

active

039557820

ABSTRACT:
A gas turbine turbojet engine for a supersonic aircraft which fits into a nacelle having a substantially square cross-section. Air flow passing between the square section of the nacelle and the circular section of the engine is compressed by an auxiliary compressor driven by a compressor of the turbojet. The auxiliary compressor is housed within a diameter not greater than the maximum diameter of the turbojet, thus enhancing the engine performance particularly at take-off.

REFERENCES:
patent: 2663517 (1953-12-01), Price
patent: 3161019 (1964-12-01), Keenan et al.
patent: 3186661 (1965-06-01), Denning et al.
patent: 3673802 (1972-07-01), Krebs et al.
patent: 3854286 (1974-12-01), Klees

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