Augmentor burner

Power plants – Reaction motor – Liquid oxidizer

Patent

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Details

60740, 60 39826, F02K 310

Patent

active

053850157

ABSTRACT:
The fuel spray bars and a compressor air bar is disposed in the cavities of the extended vanes of the turbine exhaust case to flow a fuel/air mixture perpendicular to the gas path and the pilot burner encased in the tail cone ejects a hot stream of combustion products adjacent the fuel air mixture to ignite the mixture and the ejected compressor air serves to create a recirculation zone adjacent the apertures of the spray bars to sustain combustion during the actuation of the augmentor.

REFERENCES:
patent: 2862359 (1958-12-01), Spears
patent: 2867085 (1959-01-01), Saboe
patent: 2914912 (1959-12-01), Woll
patent: 2929203 (1960-03-01), Henning et al.
patent: 2979899 (1961-04-01), Salmon

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