Combustion Nozzle with Floating Aft Plate
    1.
    发明申请
    Combustion Nozzle with Floating Aft Plate 有权
    燃烧喷嘴与浮动后板

    公开(公告)号:US20140338349A1

    公开(公告)日:2014-11-20

    申请号:US13662621

    申请日:2012-10-29

    CPC classification number: F23R3/04 F23R3/283 F23R3/286 F23R2900/03044

    Abstract: The present application provides a combustion nozzle for use with a gas turbine engine. The combustion nozzle may include a number of mixing tubes, an outer shell surrounding the mixing tubes, and a floating aft plate assembly. The floating plate assembly may enclose the outer shell. The mixing tubes may extend through the aft plate assembly.

    Abstract translation: 本申请提供了一种与燃气涡轮发动机一起使用的燃烧喷嘴。 燃烧喷嘴可以包括多个混合管,围绕混合管的外壳和浮动的后板组件。 浮板组件可以封闭外壳。 混合管可以延伸穿过后板组件。

    MULTI-PREMIXER FUEL NOZZLE SUPPORT SYSTEM
    2.
    发明申请
    MULTI-PREMIXER FUEL NOZZLE SUPPORT SYSTEM 失效
    多重燃料燃料喷嘴支持系统

    公开(公告)号:US20140000263A1

    公开(公告)日:2014-01-02

    申请号:US14015322

    申请日:2013-08-30

    CPC classification number: F23R3/10 F23R3/286

    Abstract: A system comprising a fuel nozzle. The fuel nozzle includes a mounting base and an inlet flow conditioner extending directly from the mounting base in a downstream direction. Moreover, the inlet flow conditioner structurally supports the fuel nozzle without a central support member extending directly from the mounting base inside the inlet flow conditioner.

    Abstract translation: 一种包括燃料喷嘴的系统。 燃料喷嘴包括安装基座和沿着下游方向从安装基座直接延伸的入口流动调节器。 此外,入口流动调节器结构地支撑燃料喷嘴,而没有直接从入口流动调节器内的安装基座延伸的中心支撑构件。

    Apparatus for mixing fuel in a gas turbine nozzle
    3.
    发明授权
    Apparatus for mixing fuel in a gas turbine nozzle 有权
    用于在燃气轮机喷嘴中混合燃料的装置

    公开(公告)号:US09500370B2

    公开(公告)日:2016-11-22

    申请号:US14136353

    申请日:2013-12-20

    Abstract: A fuel nozzle in a combustion turbine engine that includes: a fuel plenum defined between an circumferentially extending shroud and axially by a forward tube-sheet and an aft tube-sheet; and a mixing-tube that extends across the fuel plenum that defines a passageway connecting an inlet formed through the forward tube-sheet and an outlet formed through the aft tube-sheet, the mixing-tube comprising one or more fuel ports that fluidly communicate with the fuel plenum. The mixing-tube may include grooves on an outer surface, and be attached to the forward tube-sheet by a connection having a fail-safe leakage path.

    Abstract translation: 燃气涡轮发动机中的燃料喷嘴,其包括:在周向延伸的护罩之间限定的燃料增压室,并且由前管板和后管板轴向限定; 以及混合管,其延伸穿过所述燃料增压室,所述混合管限定连接通过所述前管板形成的入口的通道和通过所述后管板形成的出口,所述混合管包括一个或多个燃料端口,所述燃料端口与 燃料增压室。 混合管可以包括在外表面上的凹槽,并且通过具有故障安全泄漏路径的连接件附接到前管板。

    Combustion nozzle with floating aft plate
    4.
    发明授权
    Combustion nozzle with floating aft plate 有权
    燃烧喷嘴带浮板

    公开(公告)号:US09175855B2

    公开(公告)日:2015-11-03

    申请号:US13662621

    申请日:2012-10-29

    CPC classification number: F23R3/04 F23R3/283 F23R3/286 F23R2900/03044

    Abstract: The present application provides a combustion nozzle for use with a gas turbine engine. The combustion nozzle may include a number of mixing tubes, an outer shell surrounding the mixing tubes, and a floating aft plate assembly. The floating plate assembly may enclose the outer shell. The mixing tubes may extend through the aft plate assembly.

    Abstract translation: 本申请提供了一种与燃气涡轮发动机一起使用的燃烧喷嘴。 燃烧喷嘴可以包括多个混合管,围绕混合管的外壳和浮动的后板组件。 浮板组件可以封闭外壳。 混合管可以延伸穿过后板组件。

    APPARATUS FOR MIXING FUEL IN A GAS TURBINE NOZZLE
    5.
    发明申请
    APPARATUS FOR MIXING FUEL IN A GAS TURBINE NOZZLE 有权
    在燃气涡轮喷嘴中混合燃料的装置

    公开(公告)号:US20150176841A1

    公开(公告)日:2015-06-25

    申请号:US14136353

    申请日:2013-12-20

    Abstract: A fuel nozzle in a combustion turbine engine that includes: a fuel plenum defined between an circumferentially extending shroud and axially by a forward tube-sheet and an aft tube-sheet; and a mixing-tube that extends across the fuel plenum that defines a passageway connecting an inlet formed through the forward tube-sheet and an outlet formed through the aft tube-sheet, the mixing-tube comprising one or more fuel ports that fluidly communicate with the fuel plenum. The mixing-tube may include grooves on an outer surface, and be attached to the forward tube-sheet by a connection having a fail-safe leakage path.

    Abstract translation: 燃气涡轮发动机中的燃料喷嘴,其包括:在周向延伸的护罩之间限定的燃料增压室,并且由前管板和后管板轴向限定; 以及混合管,其延伸穿过所述燃料增压室,所述混合管限定连接通过所述前管板形成的入口的通道和通过所述后管板形成的出口,所述混合管包括一个或多个燃料端口,所述燃料端口与 燃料增压室。 混合管可以包括在外表面上的凹槽,并且通过具有故障安全泄漏路径的连接件附接到前管板。

    TUBE ASSEMBLY FOR USE IN FUEL INJECTION ASSEMBLIES AND METHODS OF ASSEMBLING SAME
    6.
    发明申请
    TUBE ASSEMBLY FOR USE IN FUEL INJECTION ASSEMBLIES AND METHODS OF ASSEMBLING SAME 审中-公开
    用于燃油喷射装置的管组件及其组装方法

    公开(公告)号:US20140251483A1

    公开(公告)日:2014-09-11

    申请号:US13788812

    申请日:2013-03-07

    CPC classification number: F02C7/222 Y10T29/49826

    Abstract: A tube assembly for use in a fuel injection assembly of a turbine engine is provided. The tube assembly includes a housing, and a plurality of tube assembly units positioned adjacent to one another within the housing such that each tube assembly extends along a longitudinal axis of the housing. Each tube assembly unit includes a tube, and a plurality of flanges extending radially outward from each tube, wherein flanges of adjacent tube assembly units form at least a portion of at least one wall within the housing.

    Abstract translation: 提供了一种用于涡轮发动机的燃料喷射组件的管组件。 管组件包括壳体和多个管组件单元,其在壳体内彼此相邻设置,使得每个管组件沿着壳体的纵向轴线延伸。 每个管组件单元包括管和从每个管径向向外延伸的多个凸缘,其中相邻管组件单元的凸缘形成壳体内的至少一个壁的至少一部分。

    Multi-premixer fuel nozzle support system
    7.
    发明授权
    Multi-premixer fuel nozzle support system 失效
    多预混合燃料喷嘴支撑系统

    公开(公告)号:US08769956B2

    公开(公告)日:2014-07-08

    申请号:US14015322

    申请日:2013-08-30

    CPC classification number: F23R3/10 F23R3/286

    Abstract: A system comprising a fuel nozzle. The fuel nozzle includes a mounting base and an inlet flow conditioner extending directly from the mounting base in a downstream direction. Moreover, the inlet flow conditioner structurally supports the fuel nozzle without a central support member extending directly from the mounting base inside the inlet flow conditioner.

    Abstract translation: 一种包括燃料喷嘴的系统。 燃料喷嘴包括安装基座和沿着下游方向从安装基座直接延伸的入口流动调节器。 此外,入口流动调节器结构地支撑燃料喷嘴,而没有直接从入口流动调节器内的安装基座延伸的中心支撑构件。

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