Combustor for gas turbine engine

Details Combustor for gas turbine engine Combustor for gas turbine engine

1993-04-22

1995-07-11

Thorpe, Timothy S.

Power plants

Combustion products used as motive fluid

Combustion products generator

60748, 239404, 239472, F23R 314

Patent

active

054310199

ABSTRACT:
An air blast fuel nozzle includes a unitary structure which introduces not only axially swirling primary airflow into the primary zone of the combustor chamber, but also introduces radial inflow, coswirling, primary airflow into the premixing chamber immediately upstream of the primary zone of the combustor.

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patent: 4754600 (1988-07-01), Barbier et al.
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Lefebvre, Arthur H. Gas Turbine Combustion. New York, N.Y.: McGraw-Hill, 1983. pp. 413-422.

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