发明申请
US20110005189A1 Active Control of Flame Holding and Flashback in Turbine Combustor Fuel Nozzle 审中-公开
涡轮燃烧器燃油喷嘴中火焰保持和闪回的主动控制

Active Control of Flame Holding and Flashback in Turbine Combustor Fuel Nozzle
摘要:
A system includes a turbine combustor fuel nozzle. The turbine combustor fuel nozzle includes a swirl vane. The turbine combustor fuel nozzle also includes an injection hole configured to inject fluid in a downstream region of the swirl vane. The injection of fluid in a downstream region of the swirl vane may be in response to detection of a condition indicative of a flame inside the turbine combustor fuel nozzle.
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