COMPONENT REPAIR ARRANGEMENT AND METHOD
    31.
    发明申请
    COMPONENT REPAIR ARRANGEMENT AND METHOD 审中-公开
    组件维修安排和方法

    公开(公告)号:US20140138358A1

    公开(公告)日:2014-05-22

    申请号:US13683125

    申请日:2012-11-21

    CPC classification number: B23P6/007 F01D5/005 F05D2230/233

    Abstract: A component repair arrangement includes a material depositing electrospark rod configured to deposit a material onto the component. Also included is a first routing hose for flowing a first shielding gas to a location proximate a tip of the material depositing electrospark rod, the first shielding gas removing a plurality of sparks generated proximate the tip.

    Abstract translation: 部件修理装置包括一种材料沉积电极棒,其被配置为将材料沉积到部件上。 还包括用于将第一保护气体流动到靠近沉积电极棒的材料的尖端的位置的第一布线软管,第一保护气体去除在尖端附近产生的多个火花。

    Coolant delivery via an independent cooling circuit

    公开(公告)号:US11454133B2

    公开(公告)日:2022-09-27

    申请号:US16663912

    申请日:2019-10-25

    Abstract: An embodiment of an independent cooling circuit for selectively delivering cooling fluid to a component of a gas turbine system includes: a plurality of independent circuits of cooling channels embedded within an exterior wall of the component, wherein the plurality of circuits of cooling channels are interwoven together; an impingement plate; and a plurality of feed tubes connecting the impingement plate to the exterior wall of the component and fluidly coupling each of the plurality of circuits of cooling channels to at least one supply of cooling fluid, wherein, in each of the plurality of circuits of cooling channels, the cooling fluid flows through the plurality of feed tubes into the circuit of cooling channels only in response to a formation of a breach in the exterior wall of the component that exposes at least one of the cooling channels of the circuit of cooling channels.

    Turbine airfoil with multiple walls and internal thermal barrier coating

    公开(公告)号:US10995621B2

    公开(公告)日:2021-05-04

    申请号:US16182113

    申请日:2018-11-06

    Abstract: An airfoil having a wall structure including a plurality of spaced walls for improved cooling and lifetime is disclosed. The airfoil and walls are made by additive manufacturing. The airfoil includes an exterior wall, an intermediate wall, and an interior wall each separated from adjacent walls by a plurality of standoff members; a plurality of outer cooling chambers defined between the exterior and intermediate walls, the chambers partitioned by an outer partition; a plurality of intermediate cooling chambers defined between the intermediate and interior walls, the chambers partitioned by an intermediate partition; a thermal barrier coating on each of the exterior wall and the intermediate wall; a first plurality of impingement openings through the intermediate wall; a second plurality of impingement openings through the interior wall; and a plurality of cooling passages through the exterior wall.

    COOLANT DELIVERY VIA AN INDEPENDENT COOLING CIRCUIT

    公开(公告)号:US20210123348A1

    公开(公告)日:2021-04-29

    申请号:US16663941

    申请日:2019-10-25

    Abstract: An embodiment of an independent cooling circuit for selectively delivering cooling fluid to a component of a gas turbine system includes: at least one coolant feed channel fluidly coupled to a supply of cooling fluid; and an interconnected circuit of cooling channels, including: an interconnected circuit of cooling channels embedded within an exterior wall of the component; an impingement plate; and a plurality of feed tubes connecting the impingement plate to the exterior wall of the component and fluidly coupling a supply of cooling fluid to the interconnected circuit of cooling channels; wherein the cooling fluid flows through the plurality of feed tubes into the interconnected circuit of cooling channels only in response to a formation of a breach in the exterior wall of the component that exposes at least one of the cooling channels.

    Combustor aft frame cooling
    37.
    发明授权

    公开(公告)号:US10830142B2

    公开(公告)日:2020-11-10

    申请号:US15289247

    申请日:2016-10-10

    Abstract: An aft frame for a duct of a combustor includes a rail or radial projection that extends circumferentially around the aft frame and that defines an outer surface of the aft frame. A preformed cover plate having an inner surface is attached to the outer surface of the aft frame. A plurality of micro-cooling channels is formed within at least one of the inner surface of the preformed cover plate and the outer surface of the aft frame. The preformed cover plate extends across the plurality of micro-cooling channels.

    HGP COMPONENT WITH EFFUSION COOLING ELEMENT HAVING COOLANT SWIRLING CHAMBER

    公开(公告)号:US20200300165A1

    公开(公告)日:2020-09-24

    申请号:US16360177

    申请日:2019-03-21

    Abstract: An effusion cooling element for the surface of a hot gas path (HGP) component is disclosed. The effusion cooling element includes a coolant swirling chamber embedded within the body of the HGP component. A coolant delivery passage is in the body and configured to deliver a coolant to the coolant swirling chamber. The coolant swirling chamber imparts a centrifugal force to the coolant. An effusion opening is in the HGP surface and in fluid communication with the coolant swirling chamber, the effusion opening having a smaller width than the coolant swirling chamber. The coolant exits the effusion opening over substantially all of 360° about the effusion opening, creating a coolant film on the HGP surface.

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