Gas turbine engine combustion chamber for optimizing the mixture

Details Gas turbine engine combustion chamber for optimizing the mixture Gas turbine engine combustion chamber for optimizing the mixture

1997-04-21

1999-08-10

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60748, F23R 306

Patent

active

059340673

ABSTRACT:
A gas turbine engine combustion chamber bounded by inner and outer annular walls extending around a longitudinal axis of the engine and connected by an end wall, through which extend a plurality of fuel injectors, each with an intake air swirler. The outer annular wall has a plurality of first orifices arranged in a common plane and spaced apart in a circumferential direction such that each first orifice is circumferentially associated with a fuel injector and is located on one side of a radius line extending from the longitudinal axis and passing through the axis of the associated fuel injector, and a plurality of second orifices in the inner annular wall arranged in a common plane and spaced apart in a circumferential direction such that each second orifice is circumferentially associated with a fuel injector and is located on an opposite side of the radius line from the first orifice associated with the same fuel injector.

REFERENCES:
patent: 2517015 (1950-08-01), Mock et al.
patent: 2807139 (1957-09-01), Jackson

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