COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE AND METHOD OF MAKING SAME
    6.
    发明申请
    COMBUSTOR ASSEMBLY FOR A GAS TURBINE ENGINE AND METHOD OF MAKING SAME 有权
    用于气体涡轮发动机的燃烧器组件及其制造方法

    公开(公告)号:US20170009996A1

    公开(公告)日:2017-01-12

    申请号:US14793000

    申请日:2015-07-07

    Abstract: A combustor can assembly includes a plurality of combustor cans spaced circumferentially about a gas turbine engine. Each combustor can is coupled in flow communication with at least one fuel manifold via a respective can fuel line. The combustor can assembly also includes a first interconnecting fuel line that includes a first end and a second end. The first end is coupled in flow communication with the can fuel line of a first combustor can, and the second end is coupled in flow communication with the can fuel line of a second combustor can that is not circumferentially adjacent to the first combustor can. The combustor can assembly further includes a first control device operatively coupled to the can fuel line of the first combustor can. The first control device is operable to change a dynamic operational characteristic of the first and second combustor cans independently of other combustor cans.

    Abstract translation: 燃烧器罐组件包括围绕燃气涡轮发动机周向间隔开的多个燃烧器罐。 每个燃烧器罐可以经由相应的罐燃料管线与至少一个燃料歧管流动连通地联接。 燃烧室组件还包括包括第一端和第二端的第一互连燃料管线。 第一端与第一燃烧器罐的罐燃料管线流动连通地联接,并且第二端部与第二燃烧器罐的罐燃料管线流动连通,第二燃烧器罐体不能在周向上邻近第一燃烧器罐。 燃烧室组件还包括可操作地连接到第一燃烧器罐的罐燃料管线的第一控制装置。 第一控制装置可操作以独立于其它燃烧器罐改变第一和第二燃烧器罐的动态操作特性。

    Simple cycle gas turbomachine system having a fuel conditioning system
    7.
    发明授权
    Simple cycle gas turbomachine system having a fuel conditioning system 有权
    具有燃料调节系统的简单循环气体涡轮机系统

    公开(公告)号:US09422868B2

    公开(公告)日:2016-08-23

    申请号:US13859388

    申请日:2013-04-09

    CPC classification number: F02C7/224

    Abstract: A simple cycle gas turbomachine includes a compressor portion, and a turbine portion having an outlet. At least one combustor is fluidically connected to the compressor portion and the turbine portion. An exhaust member includes an inlet, fluidically connected to the outlet of the turbine portion, a first outlet and a second outlet. A fuel conditioning system includes a heat exchange member provided with a first circuit having an exhaust gas inlet fluidically connected to the second outlet of the exhaust member and an exhaust gas inlet, a second circuit having an inlet fluidically connected to a source of fuel and an outlet fluidically connected to the at least one combustor. A conditioned fluid conduit is fluidically connected between a source of conditioned fluid and one of the combustor assembly and the first outlet of the exhaust member.

    Abstract translation: 简单的循环气体涡轮机包括压缩机部分和具有出口的涡轮机部分。 至少一个燃烧器流体地连接到压缩机部分和涡轮机部分。 排气构件包括流体连接到涡轮部分的出口的入口,第一出口和第二出口。 燃料调节系统包括具有第一回路的热交换构件,该第一回路具有与排气构件的第二出口流体连接的排气入口和排气入口,第二回路具有与燃料源流体连接的入口和 出口流体连接到至少一个燃烧器。 调节流体导管流体地连接在调节流体源和燃烧器组件之一和排气构件的第一出口之间。

    SIMPLE CYCLE GAS TURBOMACHINE SYSTEM HAVING A FUEL CONDITIONING SYSTEM
    9.
    发明申请
    SIMPLE CYCLE GAS TURBOMACHINE SYSTEM HAVING A FUEL CONDITIONING SYSTEM 有权
    具有燃油调节系统的简单循环气体涡轮机系统

    公开(公告)号:US20140298816A1

    公开(公告)日:2014-10-09

    申请号:US13859388

    申请日:2013-04-09

    CPC classification number: F02C7/224

    Abstract: A simple cycle gas turbomachine includes a compressor portion, and a turbine portion having an outlet. At least one combustor is fluidically connected to the compressor portion and the turbine portion. An exhaust member includes an inlet, fluidically connected to the outlet of the turbine portion, a first outlet and a second outlet. A fuel conditioning system includes a heat exchange member provided with a first circuit having an exhaust gas inlet fluidically connected to the second outlet of the exhaust member and an exhaust gas inlet, a second circuit having an inlet fluidically connected to a source of fuel and an outlet fluidically connected to the at least one combustor. A conditioned fluid conduit is fluidically connected between a source of conditioned fluid and one of the combustor assembly and the first outlet of the exhaust member.

    Abstract translation: 简单的循环气体涡轮机包括压缩机部分和具有出口的涡轮机部分。 至少一个燃烧器流体地连接到压缩机部分和涡轮机部分。 排气构件包括流体连接到涡轮部分的出口的入口,第一出口和第二出口。 燃料调节系统包括具有第一回路的热交换构件,该第一回路具有与排气构件的第二出口流体连接的排气入口和排气入口,第二回路具有与燃料源流体连接的入口和 出口流体连接到至少一个燃烧器。 调节流体导管流体地连接在调节流体源和燃烧器组件之一和排气构件的第一出口之间。

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