发明名称 DUAL FUEL MIXER FOR GAS TURBINE COMBUSTER
摘要 A dual fuel mixer is disclosed having a mixing duct, a shroud surrounding the upstream end of the mixing duct having contained therein a gas fuel manifoldand a liquid fuel manifold in flow communication with a gas fuel supply and a liquid fuel supply, respectively, and control means, a set of inner and outer annular counter-rotating swirlers adjacent the upstream end of the mixing duct, where atleast the outer annular swirlers include hollow vanes with internal cavities and fuel passages, all of which are in fluid communication with the gas and liquid fuel manifolds to inject gas and liquid fuel into the air stream, and a hub separating the inner and outer annular swirlers to allow independent rotation thereof wherein high pressure air from a compressor is injected into the mixing duct through the swirlers to form an intense shear region and gas and/or liquid fuel is injected into the air stream from the outer annular swirler vanes so that the high pressure air and the fuel is uniformly mixed therein so as to produce minimal formation of pollutants whenthe fuel/air mixture is exhausted out the downstream end of the mixing duct into the combustor and ignited.
申请公布号 CA2155374(A1) 申请公布日期 1996.03.13
申请号 CA19952155374 申请日期 1995.08.03
申请人 GENERAL ELECTRIC COMPANY 发明人 JOSHI, NARENDRA D.;EKSTEDT, EDWARD E.
分类号 F01D9/06;F23C7/00;F23D17/00;F23R3/14;F23R3/28;F23R3/36;(IPC1-7):F02C7/22 主分类号 F01D9/06
代理机构 代理人
主权项
地址