Fuel injection system

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

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60746, F02C 722

Patent

active

048173894

ABSTRACT:
A gas turbine engine combustor has a plurality of circumferentially fuel injectors. Two lower nozzles are pilot nozzles and are of the fuel pressure atomized type, and the majority of nozzles are of the air atomized type. A pressurizing valve maintains high fuel pressure to the pilot nozzles at all operating conditions. The fuel/air ratio for the pilot nozzles is optimized facilitating start up and increased stability during transient conditions.

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patent: 4711085 (1987-12-01), Lyons

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