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    SEAL SUPPORT DISK AND ASSEMBLY
    3.
    发明公开
    SEAL SUPPORT DISK AND ASSEMBLY 审中-公开
    DICHTUNGSTRÄGERSCHEIBEUND ANORDNUNG

    公开(公告)号：EP2938836A4

    公开(公告)日：2016-02-17

    申请号：EP13867264

    申请日：2013-12-23

    申请人： UNITED TECHNOLOGIES CORP

    发明人： VO TUAN DAVID ,  SCOTT JONATHAN ARIEL

    IPC分类号： F01D11/02 ,  F01D11/00 ,  F01D25/24 ,  F02C7/28 ,  F16J15/08

    CPC分类号： F01D11/001 ,  F01D11/005 ,  F01D25/24 ,  F01D25/243 ,  F05D2240/59 ,  F16J15/0887

    摘要： An assembly for a gas turbine engine includes a first module, a second module interconnected with the first module, a first gas turbine component, and a seal assembly. The first gas turbine component includes a body extending generally radially between an inner mounting portion and an outer seal carrier portion. The inner mounting portion is fastened to the first module such that the first gas turbine component forms a boundary between a first annular cavity in the first module, and a second annular cavity in the second module. The seal assembly is mounted to the seal carrier portion of the first gas turbine component, and includes a flow diverter assembly having a flow diverter and a finger seal commonly fastened to a first axial side of the seal carrier portion.

    摘要翻译： 用于燃气涡轮发动机的组件包括第一模块，与第一模块互连的第二模块，第一燃气涡轮机部件和密封组件。 第一燃气涡轮机部件包括在内部安装部分和外部密封件载体部分之间大致径向延伸的主体。 内部安装部分紧固到第一模块，使得第一燃气涡轮机部件形成第一模块中的第一环形腔和第二模块中的第二环形空腔之间的边界。 密封组件安装到第一燃气涡轮机部件的密封承载部分，并且包括分流器组件，该分流器组件具有通常紧固到密封承载部分的第一轴向侧的分流器和指状密封件。

    TIE ROD CONNECTION FOR MID-TURBINE FRAME
    4.
    发明公开
    TIE ROD CONNECTION FOR MID-TURBINE FRAME 审中-公开
    ZUGSTANGENVERBINDUNGFÜREINEN MITTELTURBINENRAHMEN

    公开(公告)号：EP3111057A4

    公开(公告)日：2017-03-01

    申请号：EP15777050

    申请日：2015-01-21

    申请人： UNITED TECHNOLOGIES CORP

    发明人： VO TUAN DAVID ,  LEES ALAN

    IPC分类号： F01D25/28 ,  F01D9/06 ,  F01D25/16 ,  F01D25/24 ,  F02C7/20

    CPC分类号： F01D25/243 ,  F01D5/06 ,  F01D9/02 ,  F01D9/065 ,  F01D25/162 ,  F05D2220/32 ,  F05D2230/60 ,  F05D2250/312 ,  F05D2260/31

    摘要： A mid-turbine frame for use in a gas turbine engine comprises at least one vane extending between a vane inner platform and a vane outer platform, and an inner case radially inward of the inner platform. A plurality of tie rods extend from a platform radially inward of the inner case to a radially outer location which is secured by a mount member. The tie rods are secured in the inner case by a forward bolt, and at least one rear bolt, with the forward bolt extending along an axis which is non-parallel to a center axis of the inner case. A gas turbine engine and a method for assembling a mid-turbine frame are also disclosed.

    摘要翻译： 用于燃气涡轮发动机的中涡轮机框架包括在叶片内平台和叶片外平台之间延伸的至少一个叶片和内平台径向向内的内壳体。 多个拉杆从内壳的径向向内的平台延伸到由安装构件固定的径向外部位置。 拉杆通过前部螺栓固定在内部壳体中，并且至少一个后部螺栓，其中前部螺栓沿着不平行于内部壳体的中心轴线的轴线延伸。 还公开了一种燃气涡轮发动机和用于组装中涡轮机架的方法。

    FLOW DIVERTER ELEMENT AND ASSEMBLY
    6.
    发明公开
    FLOW DIVERTER ELEMENT AND ASSEMBLY 审中-公开
    流水头和布置

    公开(公告)号：EP2938868A4

    公开(公告)日：2016-01-06

    申请号：EP13869595

    申请日：2013-12-16

    申请人： UNITED TECHNOLOGIES CORP

    发明人： VO TUAN DAVID

    IPC分类号： F02C7/28 ,  F01D9/02 ,  F01D11/00 ,  F01D25/28

    CPC分类号： F01D11/08 ,  F01D9/02 ,  F01D11/001 ,  F01D11/005 ,  F02C7/28 ,  F05D2240/55 ,  F05D2260/6022

    摘要： An assembly for a gas turbine engine, comprises a fairing assembly extending generally axially through a portion of the gas turbine engine, a first component disposed radially inward of the fairing assembly, a second component disposed axially adjacent to the first component, a flow diverter, and a finger seal. The flow diverter includes a mounting portion securing the flow diverter to the first component, and an arm extending in an axial direction from the mounting portion toward the second component. The finger seal includes a fixed end secured between the flow diverter mounting portion and the first component.