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    GROUNDING SLEEVE
    2.
    发明申请
    GROUNDING SLEEVE 审中-公开
    接地套管

    公开(公告)号：WO2014150253A1

    公开(公告)日：2014-09-25

    申请号：PCT/US2014/022724

    申请日：2014-03-10

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： ANDERSON, Carney R. ,  DITOMASSO, John C.

    IPC: H01R4/66

    CPC classification number: B64D45/02 ,  F16B19/02 ,  F16B2001/0064 ,  H01R4/308 ,  H01R4/64 ,  H01R2201/26 ,  H02G13/40

    Abstract: A grounding sleeve for grounding an electrically insulated element disposed between two metal components includes an annular body extending between a first end and a second end. At least one window is formed in the annular body between the first end and the second end.

    Abstract translation: 用于将布置在两个金属部件之间的电绝缘元件接地的接地套筒包括在第一端和第二端之间延伸的环形体。 在第一端和第二端之间的环形体中形成至少一个窗口。

    GAS TURBINE ENGINE ROTOR SEAL
    3.
    发明申请
    GAS TURBINE ENGINE ROTOR SEAL 审中-公开
    气体涡轮发动机转子密封

    公开(公告)号：WO2014116330A2

    公开(公告)日：2014-07-31

    申请号：PCT/US2013/068923

    申请日：2013-11-07

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： AIELLO, Nicholas ,  ANDERSON, Carney R.

    IPC: F01D11/00 ,  F01D9/02 ,  F04D29/08 ,  F02C7/28

    CPC classification number: F01D11/001

    Abstract: A rotary seal for sealing a bladed rotor of a gas turbine engine to a stator thereof comprises a sealing element and a sealing element support comprising a radially outer edge portion on which the sealing element is fixed, a radially inner mounting portion adapted to be attached to a supported rotor hub, and a flexible, medial web portion extending between the radially outer edge portion and the radially inner mounting portion.

    Abstract translation: 用于将燃气涡轮发动机的叶片转子密封到其定子的旋转密封件包括密封元件和密封元件支撑件，所述密封元件和密封元件支撑件包括固定密封元件的径向外边缘部分，适于附接到 支撑的转子轮毂和在径向外边缘部分和径向内部安装部分之间延伸的柔性内侧腹板部分。

    GROUNDING SLEEVE
    5.
    发明公开
    GROUNDING SLEEVE 审中-公开
    接地套管

    公开(公告)号：EP2973869A1

    公开(公告)日：2016-01-20

    申请号：EP14769073.9

    申请日：2014-03-10

    Applicant: United Technologies Corporation

    Inventor： ANDERSON, Carney R. ,  DITOMASSO, John C.

    IPC: H01R4/66

    CPC classification number: B64D45/02 ,  F16B19/02 ,  F16B2001/0064 ,  H01R4/308 ,  H01R4/64 ,  H01R2201/26 ,  H02G13/40

    Abstract: A grounding sleeve for grounding an electrically insulated element disposed between two metal components includes an annular body extending between a first end and a second end. At least one window is formed in the annular body between the first end and the second end.

    Abstract translation: 用于使设置在两个金属部件之间的电绝缘元件接地的接地套管包括在第一端部和第二端部之间延伸的环形主体。 在第一端和第二端之间的环形主体中形成至少一个窗口。

    GAS TURBINE ENGINE AIRFOIL STRUCTURE
    8.
    发明公开
    GAS TURBINE ENGINE AIRFOIL STRUCTURE 有权
    GASTURBINENMOTORSCHAUFELBLATTSTRUKTUR

    公开(公告)号：EP2993300A1

    公开(公告)日：2016-03-09

    申请号：EP15183839.8

    申请日：2015-09-04

    Applicant: United Technologies Corporation

    Inventor： ANDERSON, Carney R. ,  GRAVES, William R.

    IPC: F01D5/14 ,  F01D21/04

    CPC classification number: F01D5/141 ,  F01D5/147 ,  F01D5/3007 ,  F01D21/045 ,  F05D2240/80 ,  F05D2260/94 ,  Y02T50/673

    Abstract: An airfoil structure (60) includes an airfoil (62) that has a leading edge (76) and a platform (64) that includes a first side (70) that is attached to the airfoil (62) and a second side (82) opposite the airfoil (62). The platform (64) includes a relief cut (80) on the second side (82) of the platform (64) axially aligned with the leading edge (76).

    Abstract translation: 翼型结构（60）包括具有前缘（76）和平台（64）的翼型件（62），该平台包括附接到翼型件（62）的第一侧面（70）和第二侧面（82） 与机翼相对（62）。 平台（64）包括在与前缘（76）轴向对准的平台（64）的第二侧（82）上的释放切口（80）。

    TOOL AND METHODS FOR AIRFOIL BONDING
    9.
    发明公开
    TOOL AND METHODS FOR AIRFOIL BONDING 审中-公开

    公开(公告)号：EP3572214A1

    公开(公告)日：2019-11-27

    申请号：EP19174762.5

    申请日：2019-05-15

    Applicant: United Technologies Corporation

    Inventor： ROBERTSON, Thomas J. Jr ,  ANDERSON, Carney R. ,  SCHUTTE, Peter T.

    IPC: B29C65/00 ,  F01D5/14 ,  F01D5/28

    Abstract: An airfoil bonding system (200) may comprise a mold tool (146) configured to support an airfoil assembly (100; 300) during a bonding process. The bonding process may include applying heat and pressure to the airfoil assembly (100; 300). A surface (148) of the mold tool (146) may complement a preselected airfoil parameter. The mold tool (146) may maintain the airfoil assembly (100; 300) in the preselected airfoil parameter during the application of heat and pressure to the airfoil assembly (100; 300).

    BLADED ROTOR DISK
    10.
    发明公开
    BLADED ROTOR DISK 审中-公开
    BESCHAUFELTE ROTORSCHEIBE

    公开(公告)号：EP3012404A1

    公开(公告)日：2016-04-27

    申请号：EP15190705.2

    申请日：2015-10-21

    Applicant: United Technologies Corporation

    Inventor： ANDERSON, Carney R.

    IPC: F01D5/02 ,  F01D5/10

    CPC classification number: F01D25/06 ,  F01D5/02 ,  F01D5/10 ,  F01D5/3007 ,  F05D2260/96

    Abstract: A rotor disk (200) includes a ring shaped rotor body (240) defining a radially inward opening. Rims (220) protrude radially outward from the rotor body (240), and outwardly facing rotor blade retention slots are defined between circumferentially adjacent rims (220). Each slot is operable to receive and retain a corresponding rotor blade, and each rim (220) of the rims includes an anti-vibratory feature (260). The anti-vibratory feature (260) includes a structure defining an isogrid pattern intruding into a surface of the rim (220).

    Abstract translation: 转子盘（200）包括限定径向向内开口的环形转子体（240）。 轮毂（220）从转子主体（240）径向向外突出，并且面向外的转子叶片保持槽限定在周向相邻的轮缘（220）之间。 每个槽可操作以接收和保持相应的转子叶片，并且轮缘的每个轮缘（220）包括防振特征（260）。 防振特征（260）包括限定侵入边缘（220）的表面的等网格图案的结构。

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