Fuel injector for a gas turbine engine combustion chamber

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

Reexamination Certificate

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Details

C060S742000

Reexamination Certificate

active

07849693

ABSTRACT:
A fuel injector for a gas turbine engine combustion chamber is disclosed. The fuel injector includes a first fuel supply line for running at idle speed, a second, main, fuel supply line for running at speeds up to full throttle, and first and second injection orifices with which the two fuel supply lines respectively communicate. The injection orifices are arranged in a ring and the first orifices occupy a sector of the ring.

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