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    STATOR VANE PLATFORM WITH FLANGES
    13.
    发明申请
    STATOR VANE PLATFORM WITH FLANGES 审中-公开
    带法兰的定子瓦平台

    公开(公告)号：US20160069199A1

    公开(公告)日：2016-03-10

    申请号：US14783965

    申请日：2014-04-11

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Shelton O. Duelm ,  Kevin L. Rugg

    IPC: F01D9/04 ,  F01D25/24

    CPC classification number: F01D9/042 ,  F01D25/246 ,  Y02T50/672 ,  Y02T50/673

    Abstract: Disclosed is a gas turbine engine that includes a plurality of stator vanes. Each of the stator vanes includes an airfoil section and a platform provided at an end of the airfoil section. The platforms are provided with flanges on opposed ends thereof, and the flanges are fastened to corresponding flanges of an adjacent one of the plurality of stator vanes.

    Abstract translation: 公开了一种包括多个定子叶片的燃气涡轮发动机。 每个定子叶片包括翼型部分和设置在翼型部分的端部处的平台。 平台在其相对的两端设置有凸缘，并且凸缘被紧固到多个定子叶片中相邻的一个定子叶片的对应凸缘。

    GAS TURBINE ENGINE ATTACHMENT STRUCTURE AND METHOD THEREFOR
    14.
    发明申请
    GAS TURBINE ENGINE ATTACHMENT STRUCTURE AND METHOD THEREFOR 审中-公开
    燃气涡轮发动机附件结构及其方法

    公开(公告)号：US20160003104A1

    公开(公告)日：2016-01-07

    申请号：US14768857

    申请日：2014-01-28

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： David J. Sander ,  Shelton O. Duelm

    IPC: F01D25/26 ,  F01D9/04

    CPC classification number: F01D25/26 ,  F01D9/041 ,  F01D25/162 ,  F01D25/246 ,  F02C7/20 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2230/642 ,  F05D2230/644 ,  F05D2240/12 ,  F05D2240/14 ,  Y02T50/672 ,  Y02T50/673

    Abstract: An attachment structure for a gas turbine engine includes a frame that has a first annular case. A second annular case extends around the frame. The first annular case and the second annular case include a plurality of interlocks. Each of the interlocks includes a first member mounted on one of the first annular case or the second annular case and a corresponding second member mounted on the other of the first annular case or the second case. The first member is received in the second member such that the plurality of interlocks restricts relative circumferential and axial movement between the first annular case and the second annular case.

    Abstract translation: 用于燃气涡轮发动机的附接结构包括具有第一环形壳体的框架。 第二环形壳体围绕框架延伸。 第一环形壳体和第二环形壳体包括多个互锁。 每个互锁件包括安装在第一环形壳体或第二环形壳体中的一个上的第一构件和安装在第一环形壳体或第二壳体中的另一个上的对应的第二构件。 第一构件被容纳在第二构件中，使得多个互锁件限制第一环形壳体和第二环形壳体之间的相对周向和轴向运动。

    MANUFACTURE OF FULL RING STRUT VANE PACK
    15.
    发明申请
    MANUFACTURE OF FULL RING STRUT VANE PACK 审中-公开
    全系列风箱包装的制造

    公开(公告)号：US20140255174A1

    公开(公告)日：2014-09-11

    申请号：US13723941

    申请日：2012-12-21

    Applicant: United Technologies Corporation

    Inventor： Shelton O. Duelm ,  Michael G. McCaffrey

    IPC: F01D5/28 ,  F01D9/04

    Abstract: A vane assembly for a gas turbine engine is disclosed and includes a plurality of individual vane segments forming an annular ring. Each of the plurality of vane segments is formed of a ceramic matrix composite including at least one airfoil extending between an inner platform and an outer platform. An outer wrap is disposed about an outer periphery of the annular ring and over an interface between outer platforms of adjacent ones of the plurality of vane segments.

    Abstract translation: 公开了一种用于燃气涡轮发动机的叶片组件，并且包括形成环形环的多个单独叶片段。 多个叶片段中的每一个由包括在内平台和外平台之间延伸的至少一个翼型的陶瓷基复合材料形成。 围绕环形圈的外周并且在多个叶片段中的相邻叶片段的外平台之间的界面上设置外包裹物。

    Gas turbine engine attachment structure and method therefor
    16.
    发明授权
    Gas turbine engine attachment structure and method therefor 有权

    公开(公告)号：US10151218B2

    公开(公告)日：2018-12-11

    申请号：US14768857

    申请日：2014-01-28

    Applicant: United Technologies Corporation

    Inventor： David J. Sander ,  Shelton O. Duelm

    IPC: F01D25/26 ,  F01D9/04 ,  F01D25/24 ,  F02C7/20 ,  F01D25/16

    Abstract: An attachment structure for a gas turbine engine includes a frame that has a first annular case. A second annular case extends around the frame. The first annular case and the second annular case include a plurality of interlocks. Each of the interlocks includes a first member mounted on one of the first annular case or the second annular case and a corresponding second member mounted on the other of the first annular case or the second case. The first member is received in the second member such that the plurality of interlocks restricts relative circumferential and axial movement between the first annular case and the second annular case.

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