FITTING FOR MID-TURBINE FRAME OF GAS TURBINE ENGINE
    1.
    发明申请
    FITTING FOR MID-TURBINE FRAME OF GAS TURBINE ENGINE 有权
    燃气轮机发动机中涡轮机配件

    公开(公告)号:US20160312660A1

    公开(公告)日:2016-10-27

    申请号:US14696615

    申请日:2015-04-27

    CPC classification number: F01D25/28 F01D25/12 F01D25/14 F02C7/18 Y02T50/675

    Abstract: A fitting according to an exemplary aspect of the present disclosure includes, among other things, a main body portion having a first axial end and a second axial end opposite the first axial end, an inlet provided at the first axial end, and an outlet adjacent the second axial end. The outlet includes a plurality of circumferentially spaced-apart slots formed through the main body portion, and each slot has an area within a range of 0.52 and 0.59 square inches.

    Abstract translation: 根据本公开的示例性方面的配件包括主体部分,其具有第一轴向端部和与第一轴向端部相对的第二轴向端部,设置在第一轴向端部处的入口和邻近的出口 第二个轴向端。 出口包括穿过主体部分形成的多个周向间隔开的槽,并且每个槽具有在0.52和0.59平方英寸的范围内的面积。

    SUPPORT RING WITH THERMAL HEAT SHIELD FOR CASE FLANGE

    公开(公告)号:US20190353043A1

    公开(公告)日:2019-11-21

    申请号:US15982714

    申请日:2018-05-17

    Abstract: A heat shield vane support may have a structure including at least one of a cylindrical and a frustoconical portion with an outboard diameter and an inboard diameter extending about an axis and extending axially between a forward face and an aft face and may comprise a flange extending circumferentially about the aft face radially inward from the inboard diameter, a plurality of anti-rotation features distributed circumferentially about the inboard diameter extending radially inward from the inboard diameter and extending axially with respect to the cylindrical structure between a forward edge and an aft edge defining a length L, and a plurality of teeth distributed circumferentially about the forward face and extending axially from the forward face.

    Support ring with thermal heat shield for case flange

    公开(公告)号:US10808558B2

    公开(公告)日:2020-10-20

    申请号:US15982714

    申请日:2018-05-17

    Abstract: A heat shield vane support may have a structure including at least one of a cylindrical and a frustoconical portion with an outboard diameter and an inboard diameter extending about an axis and extending axially between a forward face and an aft face and may comprise a flange extending circumferentially about the aft face radially inward from the inboard diameter, a plurality of anti-rotation features distributed circumferentially about the inboard diameter extending radially inward from the inboard diameter and extending axially with respect to the cylindrical structure between a forward edge and an aft edge defining a length L, and a plurality of teeth distributed circumferentially about the forward face and extending axially from the forward face.

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