EFFUSION PLATE USING ADDITIVE MANUFACTURING METHODS
    31.
    发明申请
    EFFUSION PLATE USING ADDITIVE MANUFACTURING METHODS 有权
    使用添加剂制造方法的冲击板

    公开(公告)号:US20140202163A1

    公开(公告)日:2014-07-24

    申请号:US13748568

    申请日:2013-01-23

    Abstract: Additive manufacturing techniques may be utilized to construct effusion plates. Such additive manufacturing techniques may include defining a configuration for an effusion plate having one or more internal cooling channels. The manufacturing techniques may further include depositing a powder into a chamber, applying an energy source to the deposited powder, and consolidating the powder into a cross-sectional shape corresponding to the defined configuration. Such methods may be implemented to construct an effusion plate having one or more channels with a curved cross-sectional geometry.

    Abstract translation: 可以使用添加剂制造技术来构造渗出板。 这种添加剂制造技术可以包括限定具有一个或多个内部冷却通道的渗出板的构造。 制造技术可以进一步包括将粉末沉积到室中,向沉积的粉末施加能量源,并将粉末固结成对应于限定构型的横截面形状。 可以实施这样的方法来构造具有弯曲横截面几何形状的具有一个或多个通道的渗出板。

    Premixer With Fuel Tubes Having Chevron Outlets
    32.
    发明申请
    Premixer With Fuel Tubes Having Chevron Outlets 审中-公开
    具有燃料管的预混合器具有雪佛龙出口

    公开(公告)号:US20140144152A1

    公开(公告)日:2014-05-29

    申请号:US13684891

    申请日:2012-11-26

    CPC classification number: F02C7/22 F23D14/48 F23D14/62 F23R3/286

    Abstract: A premixer includes an air tube formed in a burner tube defining a longitudinal axis, and a coaxially disposed fuel tube with a turbulence enhancing chevron outlet. The fuel tube may include an exterior tube and an interior tube with the interior tube, the exterior tube or both having chevron outlets. The chevron outlets may be tapered and notched.

    Abstract translation: 预混合器包括形成在限定纵向轴线的燃烧器管中的空气管和具有湍流增强人字纹出口的同轴布置的燃料管。 燃料管可以包括外管和具有内管,外管或两者都具有人字形出口的内管。 人字形出口可以是锥形和凹口。

    TORCH IGNITER FOR A COMBUSTOR
    33.
    发明申请

    公开(公告)号:US20230045965A1

    公开(公告)日:2023-02-16

    申请号:US17975110

    申请日:2022-10-27

    Abstract: An igniter for a combustor of a turbomachine includes a fuel inlet in fluid communication with a mixing plenum. The mixing plenum is positioned upstream of a mixing channel. An air inlet is in fluid communication with the mixing plenum and an ignition source is in operative communication with the mixing channel. The igniter may include a mounting flange configured for coupling the igniter to the combustor. The ignition source may be positioned proximate to a downstream end of the mixing channel and upstream of the mounting flange. The mixing channel may define a venturi shape. The venturi shape includes a converging section between an upstream end of the mixing channel and a venturi throat.

    Dual-fuel fuel nozzle with gas and liquid fuel capability

    公开(公告)号:US10663171B2

    公开(公告)日:2020-05-26

    申请号:US15626435

    申请日:2017-06-19

    Abstract: The present disclosure is directed to a dual-fuel fuel nozzle that includes a center body having a tube shape and a gas fuel plenum defined within the center body. The duel-fuel fuel nozzle also includes a ring manifold defining a liquid fuel plenum disposed within the center body. The duel-fuel fuel nozzle further includes a plurality of radially oriented fuel injectors in fluid communication with the liquid fuel plenum. Additionally, the duel-fuel fuel nozzle includes an inner fuel tube extending axially within the center body. A portion of the inner fuel tube extends helically about an axial centerline of the center body. The inner fuel tube is in fluid communication with an axially oriented fuel injector. Furthermore, the duel-fuel fuel nozzle includes first fuel tube extending helically around a portion of the inner fuel tube within the center body. The first fuel tube is fluidly coupled to the fuel plenum.

    NOZZLE ASSEMBLY FOR A DUAL-FUEL FUEL NOZZLE
    36.
    发明申请

    公开(公告)号:US20180363912A1

    公开(公告)日:2018-12-20

    申请号:US15626461

    申请日:2017-06-19

    Abstract: The present disclosure is directed to a nozzle assembly including a header manifold and a ring manifold, which defines a liquid fuel plenum, spaced from the header manifold. An outer sleeve connects to the ring manifold, and a nozzle body connects to the outer sleeve. The ring manifold, the outer sleeve, and the nozzle body define a fluid chamber. An inner fuel tube extends from the header manifold to the nozzle body. A portion of the inner fuel tube extends helically about an axial centerline of the nozzle assembly between the ring manifold and the nozzle body. A first fuel tube extends helically around a portion of the inner fuel tube. The first fuel tube fluidly couples the liquid fuel plenum to the header manifold. A second fuel tube extends helically around a portion of the inner fuel tube and fluidly couples the liquid fuel plenum to the header manifold.

    AERODYNAMIC FASTENING OF TURBOMACHINE FUEL INJECTORS

    公开(公告)号:US20180363909A1

    公开(公告)日:2018-12-20

    申请号:US15626783

    申请日:2017-06-19

    Abstract: A premixing fuel nozzle assembly for a turbomachine is disclosed as having at least one fuel injector with an outer jacket having a first end and a second end and a threaded surface disposed therebetween. The first end has a cylindrical sealing surface and the second end has at least one wrenching pocket. An annular hub is disclosed as having an aperture with a first end and a second end and a threaded surface disposed therebetween, wherein the aperture is configured to at least partially house the fuel injector therein and the annular hub further has a conical seat about the first end. The fuel injector cylindrical sealing surface swages inward to form a hermetic seal when contacting the annular hub conical seat as the fuel injector is threaded into the aperture.

    System for reducing combustion dynamics and NOx in a combustor
    39.
    发明授权
    System for reducing combustion dynamics and NOx in a combustor 有权
    用于减少燃烧器中的燃烧动力学和NOx的系统

    公开(公告)号:US09353950B2

    公开(公告)日:2016-05-31

    申请号:US13709320

    申请日:2012-12-10

    Abstract: A combustor includes an end cap that extends radially across at least a portion of the combustor. The end cap includes an upstream surface axially separated from a downstream surface. A plurality of tubes extend from the upstream surface through the downstream surface of the end cap to provide fluid communication through the end cap. Each tube in a first set of the plurality of tubes has an inlet proximate to the upstream surface and an outlet downstream from the downstream surface. Each outlet has a first portion that extends a different axial distance from the inlet than a second portion.

    Abstract translation: 燃烧器包括沿着燃烧器的至少一部分径向延伸的端盖。 端盖包括从下游表面轴向分离的上游表面。 多个管从上游表面延伸通过端盖的下游表面以提供通过端盖的流体连通。 多个管的第一组中的每个管具有靠近上游表面的入口和从下游表面下游的出口。 每个出口具有第一部分,该第一部分与第二部分相比延伸与入口不同的轴向距离。

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