Combined guide vane and mixer for a gas turbine engine

Details Combined guide vane and mixer for a gas turbine engine Combined guide vane and mixer for a gas turbine engine

1976-02-20

1977-09-06

Croyle, Carlton R.

Power plants

Reaction motor

Air passage bypasses combustion chamber

F02K 306

Patent

active

040459578

ABSTRACT:
The multi-lobed mixer downstream of the turbine of a gas turbine engine is constructed to include the exit guide vanes for the turbine carried on the inner diameter of the mixer so as to prevent diffusing with a consequential reduction of pressure losses and engine weight.

REFERENCES:
patent: 3048376 (1962-08-01), Howald et al.
patent: 3377804 (1968-04-01), Wright et al.
patent: 3385064 (1968-05-01), Wilde et al.
patent: 3673802 (1972-07-01), Krebs et al.

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