This invention relates to an apparatus and method for increasing the reactivity of a fuel/air mixture (40) prior to homogenous combustion of the mixture. More specifically, this invention is a pilot for a gas turbine combustor which utilizes the heat of combustion within the pilot to increase the reactivity of a portion of the fuel/air mixture (42, 43) utilized by the pilot.
申请公布号
WO9964788(A1)
申请公布日期
1999.12.16
申请号
WO1999US12599
申请日期
1999.06.07
申请人
PRECISION COMBUSTION, INC.
发明人
ETEMAD, SHAHROKH;KARIM, MD., HASAN, UL;PFEFFERLE, WILLIAM, C.