Gas turbine engine power plant

Power plants – Reaction motor – Interrelated reaction motors

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Details

60229, 23926529, 244 123, 244 125, 244 23D, F02K 312

Patent

active

046793941

ABSTRACT:
A nozzle structure for a gas turbine power plant for a V.T.O.L. or S.T.O.L. type aircraft includes a main engine and at least one auxiliary engine; the efflux from the at least one auxiliary engine may be directed downwardly or alternatively horizontally through a convergent/divergent nozzle which may be closed off when the at least one auxiliary engine is inoperative.

REFERENCES:
patent: 2912189 (1959-11-01), Pouit
patent: 3161374 (1964-12-01), Allred et al.
patent: 3279191 (1966-10-01), Keenan et al.

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