发明申请
US20050120717A1 Fuel injection method and apparatus for a combustor 有权
燃料喷射方法和燃烧器装置

Fuel injection method and apparatus for a combustor
摘要:
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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