首页>
外国专利>
Combustor for gas- or liquid-fueled turbine
Combustor for gas- or liquid-fueled turbine
展开▼
机译:燃气或液体燃气涡轮机的燃烧器
展开▼
页面导航
摘要
著录项
相似文献
摘要
The combustor has three injection stages to supply fuel or a fuel/air mixture progressively to a pre-chamber or a main combustion chamber wherein the third injection stage comprises an elongated passage with an arrangement for introducing fuel into the passage. Preferably the passage extends alongside the combustion chamber and/or another passage for cooling air.
展开▼