Jet propulsion engines

Power plants – Reaction motor – Interrelated reaction motors

Patent

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Details

60269, 60 3918C, F02K 304

Patent

active

039409260

ABSTRACT:
A jet propulsion engine such as a gas turbine engine has an air compressor for supplying compressed air to the engine compressor stages. The air compressor is controllably and selectively driven by way of a disconnectable drive connection between the air compressor and a freely rotatable fan which is arranged in front of the air compressor and which in operation is rotated by the flow of intake air into the engine. A by-pass duct permits a part of the intake air to be by-passed around the air compressor and passed in variable proportions either to the engine compressor stages or directly out of a by-pass duct outlet.

REFERENCES:
patent: 2448824 (1948-09-01), Price
patent: 2565324 (1951-08-01), Ray
patent: 2930205 (1960-03-01), Walker
patent: 2952973 (1960-09-01), Hall et al.
patent: 2986218 (1961-05-01), Wagner et al.
patent: 3105661 (1963-10-01), Ferri
patent: 3587766 (1971-06-01), Slade
patent: 3609967 (1971-10-01), Waldmann
patent: 3719428 (1973-03-01), Dettmering

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