Fuel injector for a gas turbine engine combustion chamber
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United States of America Patent
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Dec 14, 2010
Issued Date -
N/A
app pub date -
Oct 5, 2007
filing date -
Oct 6, 2006
priority date (Note) -
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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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