Power plants – Reaction motor – Air passage bypasses combustion chamber
Patent
1974-05-07
1976-07-13
Husar, C. J.
Power plants
Reaction motor
Air passage bypasses combustion chamber
60269, 60 3941, 415 77, F02C 306, F02K 304
Patent
active
039686477
ABSTRACT:
A dual-flow or multiflow gas turbine power plant comprising a jet pipe, at east two separate flow-ducts each opening into the jet pipe, namely a first flow-ducts through which passes, in operation, a first gas flow and which contains a gas generator of the gas turbine type and an expansion-turbine located downstream of the gas generator, and a second flow-ducts through which passes, in operation, a second gas flow and a mixer device in which the first gas flow leaving the expansion turbine, and the second gas flow, are arranged to be mixed prior to entering the jet pipe, the plant further comprising a recompressor located downstream of the mixer device, in which the mixture of the two gas flows is arranged to be recompressed before entering the jet pipe.
REFERENCES:
patent: 2623356 (1952-12-01), Coanda
patent: 3368352 (1968-02-01), Hewson
patent: 3377804 (1968-04-01), Wright et al.
patent: 3677012 (1972-07-01), Batscha
Daniel William J.
Garrett Robert E.
Husar C. J.
Societe Nationale d'Etude et de Construction de Moteurs d'Aviati
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