|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/3936 ; ; 60/3937 ; ; 60/737|
|발명자 / 주소|
|인용정보||피인용 횟수 : 89 인용 특허 : 41|
A generally annular combustor system has a chamber with an annular chamber portion and a plurality of can-like chamber portions protruding from the annular chamber portion. An external fuel/air premixer is associated with each can chamber portion to provide a mixture with a desired (generally lean) fuel/air ratio tangentially through the can sidewall. A first portion of the total compressed air flows to the premixers, a second portion enters the combustion chamber through ports which, for can chamber volumes sufficient for complete combustion, can be loc...
A combustor for combusting fuel and compressed air to produce combustion gases, for use in a gas turbine having a compressor and a turbine mounted spaced apart on a common shaft, the combustor comprising: a chamber having an annular chamber portion with an axis, a radially outer surface, and an exit for delivery of combustion gases, and at least one can chamber portion protruding from said radially outer surface and flow connected to said annual chamber portion, and a fuel/air inlet for admitting the fuel and the compressed air for combustion into said c...