发明名称 CASING MANIFOLD FOR HIGH PRESSURE AIR DELIVERY TO FUEL NOZZLE PILOT SYSTEM
摘要 PROBLEM TO BE SOLVED: To provide a pilot manifold system for a combustor of a gas turbine engine.SOLUTION: The pilot manifold system may include a casing with a casing manifold, an end cover connected to the casing and having an end cover passage in communication with the casing manifold, and a fuel nozzle mounted on the vicinity of the end cover. The fuel nozzle may include a pilot system in communication with the end cover passage.
申请公布号 JP2015094582(A) 申请公布日期 2015.05.18
申请号 JP20140225675 申请日期 2014.11.06
申请人 GENERAL ELECTRIC CO <GE> 发明人 ROMIG BRYAN WESLEY;BRANDON TAYLOR OVERBY
分类号 F23R3/10;F02C7/22;F23R3/20;F23R3/28;F23R3/30 主分类号 F23R3/10
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