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
EP3055620(A1)
申请公布日期
2016.08.17
申请号
EP20140852174
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
