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    Turbine engine variable area vane with feather seal
    182.
    发明授权
    Turbine engine variable area vane with feather seal 有权

    公开(公告)号：US09909435B2

    公开(公告)日：2018-03-06

    申请号：US14789573

    申请日：2015-07-01

    Applicant: United Technologies Corporation

    Inventor： Tracy A. Propheter-Hinckley

    IPC: F01D11/00 ,  F01D17/16 ,  F01D9/04

    CPC classification number: F01D9/041 ,  F01D11/001 ,  F01D11/003 ,  F01D17/162 ,  F05D2220/30 ,  F05D2240/12 ,  F05D2240/55

    Abstract: An apparatus for sealing a gap between a stator vane platform including a seal slot, and a rotatable stator vane including a shaft connected to a vane end. The apparatus includes a substantially flat, semi-annular seal body, a first tab and a second tab. The seal body extends circumferentially between a first body end and a second body end, and radially between a radial inner body side and a radial outer body side. The inner body side wraps partially around the shaft, and the outer body side mates with the seal slot. The first tab extends axially from the first body end, and the second tab extends axially from the second body end. The first tab and the second tab engage the vane end and cause the seal body to move within the seal slot during rotation of the stator vane.

    Self-cooled orifice structure
    183.
    发明授权
    Self-cooled orifice structure 有权

    公开(公告)号：US09851105B2

    公开(公告)日：2017-12-26

    申请号：US14790970

    申请日：2015-07-02

    Applicant: United Technologies Corporation

    Inventor： Tracy A. Propheter-Hinckley ,  Dominic J. Mongillo ,  Joel H. Wagner ,  Mark F. Zelesky ,  Stanislav Kostka ,  Timothy S. Snyder

    IPC: F23R3/06 ,  F23R3/00

    CPC classification number: F23R3/06 ,  F23R3/002 ,  F23R3/005 ,  F23R2900/00019 ,  F23R2900/03042 ,  F23R2900/03044 ,  Y02T50/675

    Abstract: A self-cooled orifice structure that may be for a combustor of a gas turbine engine, and may further be a dilution hole structure, includes a hot side panel, a cold side panel spaced from the hot side panel, and a continuous inner wall extending between the hot and cold side panels and defining an orifice having a centerline and communicating axially through the hot and cold side panels. A plurality of end walls of the structure are in a cooling cavity that is defined in-part by the hot and cold side panels and the inner wall. Each end wall extends between and are engaged to the hot and cold side panels and are circumferentially spaced from the next adjacent end wall. A plurality of inlet apertures extend through the cold side panel and are in fluid communication with the cavity, and each one of the plurality of inlet apertures are proximate to a first side of a respective one of the plurality of end walls. A plurality of outlet apertures extend through the hot side panel and are in fluid communication with the cavity, and each one of the plurality of outlet apertures are associated with an opposite second side of a respective one of the plurality of end walls.

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