公开(公告)号：WO2015112215A2

公开(公告)日：2015-07-30

申请号：PCT/US2014063419

申请日：2014-10-31

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FRISH JOHN D ,  WILLIAMS ALEXANDER W ,  BRADSHAW SEAN D

IPC: F02C7/22 ,  F02C7/14 ,  F02C7/18 ,  F23R3/28

CPC classification number: F02C7/14 ,  F02C7/222 ,  F05D2220/32 ,  F05D2260/231 ,  F23R3/283 ,  Y02T50/675

Abstract: 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.

Abstract translation: 用于燃气涡轮发动机的燃料喷射器系统的冷却系统具有热交换器，用于冷却扩散器壳体空气的一部分，然后将冷却的扩散器壳体空气穿过围绕位于至少扩散器壳体增压室中的燃料喷射器管道的套筒 以最小化管道中的燃料加热速率。 通过最小化喷射器导管内的燃料温度，由此消除或减少焦化积聚。

公开(公告)号：EP3033508A4

公开(公告)日：2017-04-19

申请号：EP14836084

申请日：2014-08-14

Applicant: UNITED TECHNOLOGIES CORP

Inventor： KIRONN LEXIA ,  COFFEY ROGER O ,  TWELVES WENDELL V ,  SCHIRTZINGER GARY A ,  OTT JOE ,  BUTCHER EVAN ,  FRISH JOHN D

IPC: F02C7/12 ,  F02C7/14 ,  F02C7/22 ,  F23R3/28

CPC classification number: F23R3/283 ,  F02C7/14 ,  F02C7/18 ,  F02C7/222 ,  F05D2240/35 ,  F05D2260/213 ,  F23K5/14 ,  F23K2301/20 ,  F23R3/20 ,  Y02T50/675

Abstract: A fuel injector is provided for a gas turbine engine. The fuel injector includes a fuel conduit and a cooling fluid circuit through a strut. A gas turbine engine is provided that includes a multiple of fuel injectors in communication with a combustor and a cooling system in communication with each of the multiple of fuel injectors.

Abstract translation: 燃气喷射器设置用于燃气涡轮发动机。 燃料喷射器包括通过支柱的燃料管道和冷却流体回路。 提供了一种燃气涡轮发动机，其包括与燃烧器连通的多个燃料喷射器和与多个燃料喷射器中的每一个连通的冷却系统。

公开(公告)号：EP3066321A4

公开(公告)日：2016-11-23

申请号：EP14879428

申请日：2014-10-31

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FRISH JOHN D ,  WILLIAMS ALEXANDER W ,  BRADSHAW SEAN D

IPC: F02C7/22 ,  F02C7/14 ,  F02C7/18 ,  F23R3/28

CPC classification number: F02C7/14 ,  F02C7/222 ,  F05D2220/32 ,  F05D2260/231 ,  F23R3/283 ,  Y02T50/675

Abstract: 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.

公开(公告)号：EP3055536A4

公开(公告)日：2016-11-09

申请号：EP14852242

申请日：2014-10-06

Applicant: UNITED TECHNOLOGIES CORP

Inventor： FRISH JOHN D

IPC: F02C7/22 ,  F02C3/14 ,  F02C7/18 ,  F23R3/28

CPC classification number: F23R3/283 ,  F02C7/18 ,  F02C7/222 ,  F05D2220/32 ,  F05D2260/20

Abstract: An assembly is provided for a turbine engine. The assembly includes a cooling tube through which a flow path extends. The assembly also includes a fuel injector, which includes a stem connected to a tip. The stem is arranged within the cooling tube. The tip extends from the cooling tube to a nozzle. The cooling tube is adapted to direct cooling air through the flow path.

Abstract translation: 提供了一种用于涡轮发动机的组件。 该组件包括一个流道延伸通过的冷却管。 组件还包括燃料喷射器，其包括连接到尖端的杆。 阀杆布置在冷却管内。 尖端从冷却管延伸到喷嘴。 冷却管适于引导冷却空气通过流路。