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US09017064B2 Utilizing a diluent to lower combustion instabilities in a gas turbine engine 有权
利用稀释剂来降低燃气轮机的燃烧不稳定性

Utilizing a diluent to lower combustion instabilities in a gas turbine engine
Abstract:
A method of influencing combustion dynamics, including measuring a combustion dynamics parameter, and controlling a diluent flow (26) delivered to a fuel flow (32) upstream of a pilot burner fuel outlet (40) in response to the measured combustion dynamics parameter.
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