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US08011187B2 Fuel injection method and apparatus for a combustor 失效
燃料喷射方法和燃烧器装置

Fuel injection method and apparatus for a combustor
Abstract:
A combustor and injector system to inject a selected fuel into a combustor of a gas powered turbine. Generally, the injector is able to inject a selected fuel into a stream of an oxidizer to substantially mix the fuel with the oxidizer stream before any of the fuel in the fuel fan reaches an auto ignition temperature. Therefore the fuel may be substantially combusted at once and without any substantial hot spots.
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