发明名称 FUEL VAPORIZER FOR A TURBINE ENGINE COMBUSTOR
摘要 An assembly is provided for a turbine engine. The assembly includes a fuel injector and a fuel vaporizer. A nozzle of the fuel injector is adapted to direct fuel to impinge against the fuel vaporizer. The fuel vaporizer is adapted to substantially vaporize the impinging fuel.
申请公布号 US2016209041(A1) 申请公布日期 2016.07.21
申请号 US201415023580 申请日期 2014.10.06
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Twelves, Jr. Wendell V.;Williams Alexander W.;Kironn Lexia;Butcher Evan;Schirtzinger Gary A.;Ott Joseph
分类号 F23R3/30;F02C7/22 主分类号 F23R3/30
代理机构 代理人
主权项 1. An assembly for a turbine engine, the assembly comprising: a fuel injector including a nozzle; and a fuel vaporizer; the nozzle adapted to direct fuel to impinge against the fuel vaporizer; and the fuel vaporizer adapted to substantially vaporize the impinging fuel.
地址 Hartford, CT US