STATOR VANE MISTAKE PROOFING
    1.
    发明申请
    STATOR VANE MISTAKE PROOFING 审中-公开
    定期风扇失误检测

    公开(公告)号:WO2014028093A3

    公开(公告)日:2014-04-24

    申请号:PCT/US2013043083

    申请日:2013-05-29

    Abstract: An assembly for use in a gas turbine engine includes an inner diameter (ID) shroud having a plurality of ID slots and an outer diameter (OD) shroud having a plurality of OD slots. The OD shroud is positioned radially outward from the ID shroud. A first stator airfoil extends from the ID shroud to the OD shroud. The first stator airfoil is positioned at least partially in one of the ID slots and is positioned at least partially in one of the OD slots. A first end of the first stator airfoil has one of a raised tab and an indented notch.

    Abstract translation: 用于燃气涡轮发动机的组件包括具有多个ID槽的内径(ID)护罩和具有多个OD槽的外径(OD)罩。 OD护罩从ID护罩径向向外定位。 第一定子翼型件从ID护罩延伸到OD护罩。 第一定子翼型件至少部分地定位在ID槽中的一个中,并且至少部分地定位在其中一个OD槽中。 第一定子翼型件的第一端具有凸起凸片和凹口中的一个。

    STATOR VANE MISTAKE PROOFING
    3.
    发明专利

    公开(公告)号:SG11201405882SA

    公开(公告)日:2014-10-30

    申请号:SG11201405882S

    申请日:2013-05-29

    Abstract: An assembly for use in a gas turbine engine includes an inner diameter (ID) shroud having a plurality of ID slots and an outer diameter (OD) shroud having a plurality of OD slots. The OD shroud is positioned radially outward from the ID shroud. A first stator airfoil extends from the ID shroud to the OD shroud. The first stator airfoil is positioned at least partially in one of the ID slots and is positioned at least partially in one of the OD slots. A first end of the first stator airfoil has one of a raised tab and an indented notch.

    ASSEMBLY FIXTURE FOR A STATOR VANE ASSEMBLY
    5.
    发明公开
    ASSEMBLY FIXTURE FOR A STATOR VANE ASSEMBLY 有权
    MONTAGEARMATURFÜRLEITSCHAUFELANORDNUNG

    公开(公告)号:EP2859189A4

    公开(公告)日:2016-08-24

    申请号:EP13796412

    申请日:2013-05-08

    CPC classification number: F01D9/042 F01D25/285

    Abstract: A disclosed fixture for assembling a stator vane assembly for a gas turbine engine includes an outer locating ring including a plurality of outer locating pins defining a position for each of a plurality of vanes relative to an outer fairing and an inner locating ring including a plurality of inner locating rings defining a position of each of the plurality of vanes relative to an inner fairing. A clamp section includes a clamp portion and a clamp pin that define an angular orientation of each of the plurality of vanes relative to each of the inner and outer fairings, and an inner locating section supporting a plurality of radial locating pins defining a radial position of each of the plurality of vanes relative to the inner and outer fairings.

    Abstract translation: 公开的用于组装用于燃气涡轮发动机的定子叶片组件的固定装置包括外定位环,该外定位环包括多个外定位销,所述多个外定位销限定了相对于外整流装置的多个叶片中的每一个的位置,以及包括多个 内定位环限定多个叶片中的每一个相对于内部整流罩的位置。 夹具部分包括夹紧部分和夹紧销,所述夹紧部分和夹紧销限定所述多个叶片中的每一个相对于所述内部和外部整流罩中的每一个的角度取向,以及内部定位部分,其支撑多个径向定位销,所述径向定位销限定 多个叶片中的每一个相对于内部和外部整流罩。

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