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    GAS TURBINE SEAL ASSEMBLY AND SEAL SUPPORT
    22.
    发明申请
    GAS TURBINE SEAL ASSEMBLY AND SEAL SUPPORT 审中-公开
    气体涡轮密封组件和密封支撑

    公开(公告)号：WO2014105803A1

    公开(公告)日：2014-07-03

    申请号：PCT/US2013/077442

    申请日：2013-12-23

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： CHUONG, Conway ,  BUDNICK, Matthew

    IPC: F01D11/02 ,  F01D25/24 ,  F02C7/28

    CPC classification number: F01D11/001 ,  F01D11/003 ,  F01D11/005 ,  F01D25/162 ,  F01D25/24 ,  F01D25/246 ,  F02C7/28 ,  F05D2240/55

    Abstract: A gas turbine engine assembly includes a second module connected axially to a first module along a joint, and an annular cavity defined between the first module and the second module. The seal assembly is disposed proximate the cavity, and includes a seal support ring, a first finger seal, and a second finger seal. The support ring has a backing portion secured to a radial wall of to the first module, and a first seal land extending axially into the cavity away from the first module. The first finger seal has a free end adapted to contact an inner side of the first seal land. The second finger seal is adapted to seal a radially outer portion of the annular cavity

    Abstract translation: 燃气涡轮发动机组件包括沿着接头轴向连接到第一模块的第二模块和限定在第一模块和第二模块之间的环形空腔。 密封组件设置在空腔附近，并且包括密封支撑环，第一指状密封件和第二手指密封件。 所述支撑环具有固定到所述第一模块的径向壁的背衬部分和从所述第一模块轴向延伸到所述腔体中的第一密封区域。 第一指状密封件具有适于接触第一密封区域的内侧的自由端。 第二指状密封件适于密封环形空腔的径向外部部分

    MULTI-PURPOSE GAS TURBINE SEAL SUPPORT AND ASSEMBLY
    23.
    发明申请
    MULTI-PURPOSE GAS TURBINE SEAL SUPPORT AND ASSEMBLY 审中-公开
    多用途气体涡轮机密封支撑和组件

    公开(公告)号：WO2014105780A1

    公开(公告)日：2014-07-03

    申请号：PCT/US2013/077397

    申请日：2013-12-23

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： VO, Tuan, David ,  CHUONG, Conway ,  BUDNICK, Matthew ,  SCOTT, Jonathan, Ariel

    IPC: F01D11/02 ,  F01D25/24 ,  F02C7/28

    CPC classification number: F01D11/02 ,  F01D9/065 ,  F01D11/001 ,  F01D11/122 ,  F01D25/162 ,  F01D25/28 ,  F02C7/28

    Abstract: A gas turbine engine assembly includes a first module, a second module rotatable about a center line of the gas turbine engine and fluidly coupled with the first module, and a multi-purpose seal support. The multi-purpose seal support includes an aft end secured to the first module, and a forward end disposed proximate the second module. The forward end has a discourager portion, a seal portion, and a meshing portion.

    Abstract translation: 燃气涡轮发动机组件包括第一模块，可围绕燃气涡轮发动机的中心线旋转并与第一模块流体连接的第二模块，以及多用途密封支撑件。 多用途密封件支撑件包括固定到第一模块的后端和靠近第二模块设置的前端。 前端具有罢工部分，密封部分和啮合部分。

    MOUNT WITH DEFLECTABLE TABS
    24.
    发明申请
    MOUNT WITH DEFLECTABLE TABS 审中-公开
    安装可拆卸的餐具

    公开(公告)号：WO2014105657A1

    公开(公告)日：2014-07-03

    申请号：PCT/US2013/076760

    申请日：2013-12-19

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： BUDNICK, Matthew

    IPC: F02C7/20 ,  F01D25/28

    CPC classification number: F02C7/20 ,  F01D9/041 ,  F01D11/005 ,  F01D25/162 ,  F01D25/243 ,  F02C7/24 ,  F05D2260/941 ,  Y10T29/49828

    Abstract: An assembly for a gas turbine engine includes a first component, a second component, and a first mount. The first mount includes an annular body that is connected to the first component and a plurality of circumferentially spaced tabs extending from the body. The tabs are connected to the second component and are deflectable to allow the second component to move relative to the first component.

    Abstract translation: 用于燃气涡轮发动机的组件包括第一部件，第二部件和第一安装件。 第一安装件包括连接到第一部件的环形主体和从主体延伸的多个周向间隔的突出部。 突片连接到第二部件并且可偏转以允许第二部件相对于第一部件移动。

    HEAT SHIELD FOR A CASING
    26.
    发明申请
    HEAT SHIELD FOR A CASING 审中-公开
    热风箱

    公开(公告)号：WO2014105602A1

    公开(公告)日：2014-07-03

    申请号：PCT/US2013/076385

    申请日：2013-12-19

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： BUDNICK, Matthew

    IPC: F02C7/24 ,  F02C7/20 ,  F01D25/24

    CPC classification number: F01D25/145 ,  F01D9/065 ,  F01D25/162 ,  F01D25/24 ,  F01D25/28 ,  F02C7/12 ,  F02C7/28 ,  F05D2220/32 ,  F05D2260/231 ,  Y02T50/675 ,  Y10T29/49321

    Abstract: A gas turbine engine includes a casing, a fairing, and a heat shield. The fairing is annularly shaped and disposed adjacent the casing. The heat shield is connected to the casing and includes a first portion and a second portion. The first portion is generally cylindrically shaped and extends between the fairing and the casing and the second portion extends generally radially away from the casing and the first portion toward the fairing.

    Abstract translation: 燃气涡轮发动机包括壳体，整流罩和隔热罩。 整流罩是环形的并且设置在壳体附近。 隔热罩连接到壳体并且包括第一部分和第二部分。 第一部分通常是圆柱形的并且在整流罩和壳体之间延伸，并且第二部分大致径向延伸远离壳体，第一部分朝向整流罩延伸。

    REDUCED MISALIGNMENT GEAR SYSTEM
    28.
    发明公开
    REDUCED MISALIGNMENT GEAR SYSTEM 审中-公开
    具有减少平行不对传输系统

    公开(公告)号：EP3036411A1

    公开(公告)日：2016-06-29

    申请号：EP14838303.7

    申请日：2014-08-13

    Applicant: United Technologies Corporation

    Inventor： BUDNICK, Matthew ,  CHUONG, Conway

    IPC: F01D25/18

    CPC classification number: F01D25/18 ,  F01D25/16 ,  F02C7/06 ,  F02C7/36 ,  F05D2260/40311 ,  F16H1/28 ,  F16H57/043 ,  F16H57/0471 ,  F16H57/0479 ,  F16H57/0486 ,  Y02T50/671

    Abstract: A lubrication system for a fan drive planetary gear system according to an exemplary aspect of the present disclosure includes, among other things, a stationary first bearing configured to receive a lubricant from a lubricant input, the stationary first bearing is located adjacent a fan drive shaft. A second bearing is configured to rotate with the fan drive shaft, the first bearing engages the second bearing and is configured to transfer the lubricant from the first bearing to the second bearing and into at least one fluid passage in the fan drive shaft. A conduit fluidly connects the at least one passage in the fan drive shaft with at least one component on the fan drive gear system.

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