Recessed fuel injector positioning
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United States of America Patent
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Nov 14, 2017
Issued Date -
N/A
app pub date -
Nov 11, 2013
filing date -
Dec 11, 2012
priority date (Note) -
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Abstract
A combustion chamber for a gas turbine is provided. The combustion chamber has a pilot burner device, a fuel injector and an ignitor unit. The pilot burner device has a pilot body with a pilot surface which is facing an inner volume of the combustion chamber. The fuel injector has a fuel outlet for injecting a fuel into the inner volume. The ignitor unit is adapted for igniting the fuel inside the inner volume, wherein the ignitor unit is arranged at the pilot surface such that fuel which passes the ignitor unit is ignitable. The pilot body includes a recess, wherein the fuel outlet is arranged within the recess.
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