Gas turbine engine gas flow ducts

Details Gas turbine engine gas flow ducts Gas turbine engine gas flow ducts

1976-02-02

1977-10-11

Croyle, Carlton R.

Power plants

Reaction motor

Air passage bypasses combustion chamber

60269, 60271, 23926517, F02K 306, F02K 102

Patent

active

040528472

ABSTRACT:
A ducted fan gas turbine engine power plant has an augmenter air intake and a flow mixer for selectively mixing the augmenter air with the remaining engine flows.

REFERENCES:
patent: 3409228 (1968-11-01), Mehr
patent: 3579993 (1971-05-01), Tanner
patent: 3610533 (1971-10-01), Johnson et al.
patent: 3655009 (1972-04-01), Hilbig
patent: 3696617 (1972-10-01), Ellis
patent: 3806035 (1974-04-01), Calder

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