Combustion apparatus for a gas turbine engine

Power plants – Combustion products used as motive fluid – Combustion products generator

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239406, F02C 722

Patent

active

041552202

ABSTRACT:
Combustion apparatus for a gas turbine engine for directing combustion air to enter the combustor adjacent the fuel oil nozzle in a vigorous swirling pattern to thoroughly mix with the atomized fuel to eliminate fuel rich, smoke producing pockets from the combustion zone. The apparatus includes air inlet ports directing one portion of the combustion air in an axially directed swirling motion, another portion of the air in a tangentially directed swirling motion with other portions of the air directed to cool and clean the nozzle and cool the wall of the combustor.

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