Fuel and air mixing parts for a turbine combustion chamber

Details Fuel and air mixing parts for a turbine combustion chamber Fuel and air mixing parts for a turbine combustion chamber

1995-03-14

1997-01-07

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combustion products generator

60752, F02C 700

Patent

active

055905307

ABSTRACT:
An annular combustion chamber for a gas turbine engine is provided with a plurality of fuel injection nozzles at its upstream end to direct swirled flows of fuel and air into the chamber. Ports in the combustion chamber walls direct air into the combustion chamber to oppose the swirling fuel and air flows from the fuel injection nozzles to achieve better fuel and air mixing.

REFERENCES:
patent: 3134229 (1964-05-01), Johnson
patent: 3643430 (1972-02-01), Emory, Jr. et al.
patent: 3811278 (1974-05-01), Taylor et al.
patent: 3874169 (1975-01-01), Andersson
patent: 4301657 (1981-11-01), Penny

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