Combuster and operating method for gas-or liquid-fuelled turbine

Details Combuster and operating method for gas-or liquid-fuelled turbine Combuster and operating method for gas-or liquid-fuelled turbine

1996-02-21

1998-07-28

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

60737, 60752, F02C 718, F23R 304

Patent

active

057848769

ABSTRACT:
In a combustor for a gas turbine, combustor 1 utilizes at least 50% of the air supplied thereto by a compressor to mix with the fuel to form a lean mixture, the remainder of the air is utilized for impingement cooling and the spent impingement cooling air is injected as radial jets into a post-primary combustion zone 17 through perforations 6.

REFERENCES:
patent: 4008568 (1977-02-01), Spears et al.
patent: 4205524 (1980-06-01), Schirmer
patent: 4567730 (1986-02-01), Scott

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