Lobe mixer for gas turbine engine

Details Lobe mixer for gas turbine engine Lobe mixer for gas turbine engine

1980-09-26

1983-08-30

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

With addition of secondary fluid upstream of outlet

60262, 60271, 181220, F02K 126

Patent

active

044012691

ABSTRACT:
The lobe mixer of a gas turbine engine is modified by judiciously extending chutes axially and radially inwardly toward the engine centerline permitting the use of a smaller cooperating centerbody while improving on engine performance and noise suppression.

REFERENCES:
patent: 4066214 (1978-01-01), Johnson
patent: 4149375 (1979-04-01), Wynosky et al.

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