Gas turbine engine with bypass diverter means

Details Gas turbine engine with bypass diverter means Gas turbine engine with bypass diverter means

1987-07-29

1989-07-11

Stout, Donald E.

Power plants

Reaction motor

Interrelated reaction motors

602263, 244 6, 244207, F02K 304

Patent

active

048459399

ABSTRACT:
A gas turbine engine for a compound helicopter comprises a core gas generator, an upstream fan, and a power turbine. Bypass air is selectively directable to either augmentor wings, or to a second power turbine which is mechanically coupled to the first power turbine.

REFERENCES:
patent: 3332644 (1967-07-01), Whittley
patent: 3938328 (1976-02-01), Klees
patent: 4054030 (1977-10-01), Pedersen
patent: 4326686 (1982-04-01), Runge

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