发明名称 COOLED FUEL INJECTOR SYSTEM FOR A GAS TURBINE ENGINE
摘要 A cooling system for a fuel injector system of a gas turbine engine has a heat exchanger for cooling a portion of diffuser case air and then routing the cooled diffuser case air through a sleeve that surrounds a fuel injector conduit located in at least the diffuser case plenum for minimizing fuel heat-up rates in the conduit. By minimizing fuel temperatures within the injector conduit, coking accumulation is thereby eliminated or reduced.
申请公布号 WO2015112215(A3) 申请公布日期 2015.10.08
申请号 WO2014US63419 申请日期 2014.10.31
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 FRISH, JOHN D.;WILLIAMS, ALEXANDER W.;BRADSHAW, SEAN D.
分类号 F02C7/22;F02C7/14;F02C7/18;F23R3/28 主分类号 F02C7/22
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