发明授权
US07694521B2 Installation structure of pilot nozzle of combustor 有权
燃烧器引燃喷嘴安装结构

Installation structure of pilot nozzle of combustor
摘要:
Pilot fuel injected from fuel injection ports 21 of a pilot nozzle 2 bumps against an inner wall surface of a tapered portion of an inner circumference of a cone 41 of a pilot cone 4. At this time, the position where a pilot fuel from the fuel injection ports 21 hits is located in a range from a middle of the tapered portion of the inner circumference of a cone 41 to a downstream-side tip thereof.
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