发明名称 GAS TURBINE FUEL SYSTEM FOR LOW DYNAMICS
摘要 A combustor is provided and includes a center body having a tubular inner wall, a cartridge disposed within the tubular inner wall to define an outer annular space between an outer surface thereof and the tubular inner wall and an inner annular space having an open end and a closed end opposite the open end and an insert disposed within the outer annular space to envelop the cartridge proximate to the open end, the insert including a body having a tubular forward portion and a partially tubular aft portion, the partially tubular aft portion thereby forming a recessed track having a longitudinal axis substantially aligned with a longitudinal axis of the outer annular space.
申请公布号 US2012180486(A1) 申请公布日期 2012.07.19
申请号 US201113008115 申请日期 2011.01.18
申请人 KIM KWANWOO;PARSANIA NISHANT GOVINDBHAI;SHARMA DHEERAJ;GENERAL ELECTRIC COMPANY 发明人 KIM KWANWOO;PARSANIA NISHANT GOVINDBHAI;SHARMA DHEERAJ
分类号 F02C7/24;F02C7/22 主分类号 F02C7/24
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