VALVE INCLUDING MULTILAYER WEAR PLATE
    1.
    发明申请
    VALVE INCLUDING MULTILAYER WEAR PLATE 有权
    阀门包括多层磨损板

    公开(公告)号:US20160084395A1

    公开(公告)日:2016-03-24

    申请号:US14949388

    申请日:2015-11-23

    IPC分类号: F16K25/00 F16K1/22

    摘要: A valve is provided and includes a component including a surface and a wear plate including a surface disposed in sliding engagement with the surface of the component. The surface of the wear plate includes a corrosion resistant substrate, a secondary layer disposed on a surface of the corrosion resistant substrate, a noble metal layer disposed on a surface of the secondary layer and a tertiary layer disposed on a surface of the noble metal layer.

    摘要翻译: 提供阀,并且包括包括表面的部件和耐磨板,所述耐磨板包括与所述部件的表面滑动配合的表面。 耐磨板的表面包括耐腐蚀基材,设置在耐腐蚀基材的表面上的二次层,设置在二次层的表面上的贵金属层和设置在贵金属层的表面上的第三层 。

    FIRST STAGE TURBINE NOZZLE WITH EROSION COATING SURFACE FINISH

    公开(公告)号:US20200024719A1

    公开(公告)日:2020-01-23

    申请号:US16239889

    申请日:2019-01-04

    摘要: A first stage turbine nozzle includes a first stage hub portion extending axially along a central axis, a first stage disk portion attached to the first stage hub portion and centered on the central axis, and a plurality of first stage vanes positioned radially around and attached to the first stage disk portion. Each vane extends a vane height H away from the first stage disk portion and each vane has a first end positioned at a diameter D away from the central axis. The first stage turbine nozzle also includes a plurality of first stage throats defined between radially adjacent first stage vanes. Each first stage throat has a throat width W between radially adjacent first stage vanes. The first stage turbine nozzle also includes a coating on a sidewall of each first stage vane, wherein a surface roughness of the sidewall is between 125 and 200 microinches Ra.

    First stage turbine nozzle with erosion coating surface finish

    公开(公告)号:US10214804B2

    公开(公告)日:2019-02-26

    申请号:US14584499

    申请日:2014-12-29

    摘要: A first stage turbine nozzle includes a first stage hub portion extending axially along a central axis, a first stage disk portion attached to the first stage hub portion and centered on the central axis, and a plurality of first stage vanes positioned radially around and attached to the first stage disk portion. Each vane extends a vane height H away from the first stage disk portion and each vane has a first end positioned at a diameter D away from the central axis. The first stage turbine nozzle also includes a plurality of first stage throats defined between radially adjacent first stage vanes. Each first stage throat has a throat width W between radially adjacent first stage vanes. The first stage turbine nozzle also includes a coating on a sidewall of each first stage vane.

    Valve including multilayer wear plate
    8.
    发明授权
    Valve including multilayer wear plate 有权
    阀门包括多层耐磨板

    公开(公告)号:US09470328B2

    公开(公告)日:2016-10-18

    申请号:US14949388

    申请日:2015-11-23

    IPC分类号: F16K25/00 F16K1/22 F16K1/226

    摘要: A valve is provided and includes a component including a surface and a wear plate including a surface disposed in sliding engagement with the surface of the component. The surface of the wear plate includes a corrosion resistant substrate, a secondary layer disposed on a surface of the corrosion resistant substrate, a noble metal layer disposed on a surface of the secondary layer and a tertiary layer disposed on a surface of the noble metal layer.

    摘要翻译: 提供阀,并且包括包括表面的部件和耐磨板,所述耐磨板包括与所述部件的表面滑动配合的表面。 耐磨板的表面包括耐腐蚀基材,设置在耐腐蚀基材的表面上的二次层,设置在二次层的表面上的贵金属层和设置在贵金属层的表面上的第三层 。

    SECOND STAGE TURBINE NOZZLE WITH EROSION COATING SURFACE FINISH
    10.
    发明申请
    SECOND STAGE TURBINE NOZZLE WITH EROSION COATING SURFACE FINISH 审中-公开
    第二级涡轮喷嘴与腐蚀涂层表面处理

    公开(公告)号:US20160186585A1

    公开(公告)日:2016-06-30

    申请号:US14584486

    申请日:2014-12-29

    摘要: A second stage turbine nozzle includes a second stage disk portion having a central axis, and a plurality of second stage vanes positioned radially around and attached to the second stage disk portion. Each second stage vane extends a vane height H away from the second stage disk portion and each second stage vane has a first end positioned at a diameter D away from the central axis. The second stage turbine nozzle also includes a plurality of second stage throats defined between radially adjacent second stage vanes. Each second stage throat has a throat width W between radially adjacent second stage vanes. The second stage turbine nozzle also includes a coating on a sidewall of each second stage vane, wherein a surface roughness of the sidewall is between 125 and 200.

    摘要翻译: 第二级涡轮喷嘴包括具有中心轴线的第二级盘部分和径向地围绕并连接到第二级盘部分的多个第二级叶片。 每个第二级叶片将叶片高度H从第二级盘片部分延伸出来,并且每个第二级叶片具有位于离中心轴线的直径D的第一端。 第二级涡轮喷嘴还包括限定在径向相邻的第二级叶片之间的多个第二级喉道。 每个第二级喉部在径向相邻的第二级叶片之间具有喉部宽度W. 第二级涡轮喷嘴还包括在每个第二级叶片的侧壁上的涂层,其中侧壁的表面粗糙度在125和200之间。