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    LINER ASSEMBLY
    1.
    发明申请
    LINER ASSEMBLY 审中-公开
    内衬组件

    公开(公告)号：WO2014021973A2

    公开(公告)日：2014-02-06

    申请号：PCT/US2013/040232

    申请日：2013-05-09

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： TREAT, Christopher ,  STENMAN, Christina A. ,  DUELM, Shelton O. ,  SIMPSON, Alex J.

    IPC: F02K1/12 ,  F02K1/06 ,  F02C7/00

    CPC classification number: F02K1/1223 ,  F02K1/12 ,  F05D2300/6033 ,  F23R3/16

    Abstract: A liner assembly includes a plurality of flaps arranged about a central axis and operable to move relative to the central axis. Each of the plurality of flaps defines a forward end and an aft end, lateral sides, and an inner surface and an outer surface relative to the central axis. Each of the plurality of flaps has a thickness between the inner surface and the outer surface, and thickness varies in a lateral direction between the lateral sides.

    Abstract translation: 衬套组件包括围绕中心轴布置并可操作以相对于中心轴线移动的多个翼片。 多个翼片中的每一个限定了前端和后端，侧面以及相对于中心轴线的内表面和外表面。 多个翼片中的每一个在内表面和外表面之间具有厚度，并且厚度在横向方向之间在横向方向上变化。

    BLADE ELEMENT CROSS-TIES
    4.
    发明公开
    BLADE ELEMENT CROSS-TIES 审中-公开
    SCHAUFELELEMENT MIT QUERSTREBE

    公开(公告)号：EP2942484A1

    公开(公告)日：2015-11-11

    申请号：EP15166907.4

    申请日：2015-05-08

    Applicant: United Technologies Corporation

    Inventor： SNYDER, Daniel A. ,  THORNTON, Lane ,  SIMPSON, Alex J.

    IPC: F01D5/16 ,  F01D5/18

    Abstract: The invention concerns a blade element for a gas turbine engine and methods of manufacturing said blade elements.
    In one embodiment, a blade element 100 includes a first inner surface 108 of the blade element, wherein the first inner surface 108 is associated with a first outer blade surface 106 of the blade element, and a second inner surface 109 of the blade element, wherein the second inner surface 109 is associated with a second outer blade surface 107 of the blade element and wherein the second inner surface 109 is opposite from the first inner surface 108. The blade element 100 also includes a cross-tie 130 1 configured to connect the first inner surface 108 to the second inner surface 109, wherein the cross-tie 130 1 is positioned along a trailing edge 110 of the blade element 100 and the cross-tie 130 1 is configured to reduce vibration mode effects of the blade element 100.

    Abstract translation: 本发明涉及一种用于燃气涡轮发动机的叶片元件和制造所述叶片元件的方法。 在一个实施例中，叶片元件100包括叶片元件的第一内表面108，其中第一内表面108与叶片元件的第一外叶片表面106和叶片元件的第二内表面109相关联， 其中第二内表面109与叶片元件的第二外叶片表面107相关联，并且其中第二内表面109与第一内表面108相对。刀片元件100还包括跨接线130 1， 第一内表面108到第二内表面109，其中交叉连接130 1沿着叶片元件100的后缘110定位，并且交叉连接130 1被配置为减小叶片元件100的振动模式效应 。

    SPHERICAL JOINT ASSEMBLY WITH A SPHERICAL BEARING BETWEEN COLLARS
    6.
    发明公开
    SPHERICAL JOINT ASSEMBLY WITH A SPHERICAL BEARING BETWEEN COLLARS 审中-公开
    带球面支撑的球形接头组件

    公开(公告)号：EP3249248A1

    公开(公告)日：2017-11-29

    申请号：EP17172078.2

    申请日：2017-05-19

    Applicant: United Technologies Corporation

    Inventor： SIMPSON, Alex J. ,  KRYSTOWSKI, Edward A.

    IPC: F16C11/04

    CPC classification number: F16C11/0604 ,  F16C11/045 ,  F16C11/0695 ,  F16C2326/43 ,  F16C2360/23

    Abstract: A bearing joint assembly (10) includes a bearing sleeve (16), a first mount (24), a pair of second mounts (26A, 26B) and a fastener (18). The bearing sleeve (16) extends axially along a centerline (28) and includes a spherical bearing (42), a first collar (44) and a second collar (46). The spherical bearing (42) is axially between the first collar (44) and the second collar (46). An annular channel is formed by and extends axially between the spherical bearing (42) and the first collar (44). The first mount (24) is mounted on and slidably engages the spherical bearing (42). The bearing sleeve (16) is axially between the second mounts (26A, 26B). The fastener (18) projects through the bearing sleeve (16) and secures the bearing sleeve (16) to the second mounts (26A, 26B).

    Abstract translation: 轴承接头组件（10）包括轴承套筒（16），第一安装件（24），一对第二安装件（26A，26B）和紧固件（18）。 轴承套筒（16）沿着中心线（28）轴向延伸并且包括球面轴承（42），第一套环（44）和第二套环（46）。 球形轴承（42）轴向位于第一套环（44）和第二套环（46）之间。 环形通道由球形轴承（42）和第一套环（44）之间形成并轴向延伸。 第一安装件（24）安装在球面轴承（42）上并且可滑动地接合球面轴承（42）。 轴承套筒（16）轴向位于第二安装件（26A，26B）之间。 紧固件18穿过轴承套筒16并将轴承套筒16固定在第二安装座26A，26B上。

    SPHERICAL BEARING SLEEVE CONFIGURED WITH ONE OR MORE DISCRETE COLLARS
    7.
    发明公开
    SPHERICAL BEARING SLEEVE CONFIGURED WITH ONE OR MORE DISCRETE COLLARS 审中-公开
    配有一个或多个离散套圈的球面轴套

    公开(公告)号：EP3249249A1

    公开(公告)日：2017-11-29

    申请号：EP17172292.9

    申请日：2017-05-22

    Applicant: United Technologies Corporation

    Inventor： SIMPSON, Alex J. ,  KRYSTOWSKI, Edward A.

    IPC: F16C11/04

    CPC classification number: F16C11/0604 ,  F16C11/045 ,  F16C11/0695 ,  F16C2326/43 ,  F16C2360/23

    Abstract: A bearing joint assembly (10) may include a bearing sleeve (16), a first collar (18), a first mount (28), a pair of second mounts (30A,30B) and a fastener (22), which projects through the bearing sleeve (16) and secures the bearing sleeve (16) to the second mounts (30A,30B). The bearing sleeve (16) extends axially along a centerline (32) and includes a spherical bearing. The first collar (18) is configured with the bearing sleeve (16). A first annular channel is formed by and extends axially between the spherical bearing and the first collar (18). The first mount (28) is mounted on and slidably engages the spherical bearing. The spherical bearing and the first collar (18) are axially between the second mounts (30A,30B).

    Abstract translation: 轴承接头组件（10）可以包括轴承套筒（16），第一套环（18），第一安装座（28），一对第二安装座（30A，30B）和紧固件（22） 轴承套筒（16）并将轴承套筒（16）固定到第二安装座（30A，30B）。 轴承套筒（16）沿中心线（32）轴向延伸并包括球面轴承。 第一套环（18）配置有轴承套筒（16）。 第一环形通道由球面轴承和第一套环（18）形成并轴向延伸。 第一安装件（28）安装在球面轴承上并可滑动地接合球面轴承。 球面轴承和第一轴环（18）轴向位于第二安装座（30A，30B）之间。

    ENHANCED DURABILITY DRIVE LINK FOR HIGH LOAD MISALIGNMENT
    8.
    发明公开
    ENHANCED DURABILITY DRIVE LINK FOR HIGH LOAD MISALIGNMENT 审中-公开
    增强的耐久性驱动链路实现高负载误差

    公开(公告)号：EP3228885A1

    公开(公告)日：2017-10-11

    申请号：EP17155049.4

    申请日：2017-02-07

    Applicant: United Technologies Corporation

    Inventor： ALHOLM, Hannes A. ,  CZAPSKI, Jr. Joseph J. ,  JLIDI, Bessem ,  SIMPSON, Alex J.

    IPC: F16C23/04 ,  B64D27/26 ,  B64C15/00 ,  F02K1/00

    CPC classification number: F02K1/1292 ,  B23P15/003 ,  B64C15/00 ,  F02K1/15 ,  F05D2260/40 ,  F16C23/043 ,  F16C23/045 ,  F16C2360/23

    Abstract: A drive link assembly (100) includes a case (106) having a spherically formed inner ring (107). A clevis (130) is affixed to a surface of the case such that the inner ring is disposed horizontally between a first end and a second end of the clevis. A spacer (110, 112, 114, 116) having a spherical inset portion is positioned on the surface horizontally between the clevis and the spherically formed inner ring, such that the spherical inset portion is aligned with the spherically formed inner ring. A spherical bearing (118) is seated within the spherically formed inner ring. A rod (108) is affixed to an outer surface of the spherical bearing.

    Abstract translation: 驱动连杆组件（100）包括具有球形内环（107）的壳体（106）。 U形夹（130）固定到外壳的表面，使得内环水平地布置在U形夹的第一端和第二端之间。 具有球形嵌入部分的间隔件（110,112,114,116）在水平表面上定位在U形夹和球形内环之间，使得球形嵌入部分与球形内环对齐。 球形轴承（118）位于球形内环内。 杆（108）被固定到球形轴承的外表面。

    LINKAGE ASSEMBLY
    10.
    发明公开
    LINKAGE ASSEMBLY 审中-公开

    公开(公告)号：EP3657034A1

    公开(公告)日：2020-05-27

    申请号：EP19214994.6

    申请日：2018-07-06

    Applicant: United Technologies Corporation

    Inventor： SIMPSON, Alex J. ,  KNOWLTON, Robert T.

    IPC: F16C11/06 ,  B64D33/04 ,  F02K1/12 ,  F16C11/02 ,  F16C11/04

    Abstract: Disclosed is a linkage assembly for a gas turbine engine (20) having a link (102a-102d) having a first end (104a), a second end (104b), and a rod (106) extending therebetween, the first end having a first sliding bearing (108) disposed within a first sliding bearing housing (107), a fastener (118) comprising a first flange (126a) and a second flange (126b), a pin (120) extending between the first flange and the second flange, wherein the first sliding bearing is pivotally connected to the pin; and a biasing member (136a, 136b) secured between the first flange and the sliding bearing housing, the biasing member contacting the sliding bearing housing and biasing the link against rotation about a center axis for the rod of the link.

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