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    FAN PLATFORM
    1.
    发明申请
    FAN PLATFORM 审中-公开
    风扇平台

    公开(公告)号：WO2015073096A3

    公开(公告)日：2015-07-09

    申请号：PCT/US2014052921

    申请日：2014-08-27

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： ROBERTSON THOMAS J

    IPC: F01D5/28

    CPC classification number: F01D5/282 ,  F01D5/02 ,  F01D5/147 ,  F01D11/008 ,  F05D2220/32 ,  F05D2220/36 ,  F05D2240/30 ,  F05D2240/80 ,  F05D2300/6034 ,  F05D2300/614 ,  Y02T50/672

    Abstract: A fan platform section (300) may include a flow path portion (310) with a plurality of composite plies. A first composite ply (830) in the plurality of composite plies may include directional fibers (835). The directional fibers may be configured to prevent twisting of the flow path section in response to a centripetal load. The fan platform section may include a second composite ply (820) in the plurality of composite plies. The second composite ply may include directional fibers (825). The directional fibers in the first composite ply may be orthogonal with respect to the directional fibers in the second composite ply.

    Abstract translation: 风机平台部分（300）可以包括具有多个复合层的流动路径部分（310）。 多个复合层片中的第一复合层片（830）可以包括定向纤维（835）。 定向光纤可被配置为响应于向心负载而防止流路部分扭曲。 风扇平台部分可以包括多个复合层中的第二复合层（820）。 第二复合层片可以包括定向纤维（825）。 第一复合层中的定向纤维可以相对于第二复合层中的定向纤维正交。

    AUXILIARY COMPONENT MOUNTS
    2.
    发明申请
    AUXILIARY COMPONENT MOUNTS 审中-公开
    辅助部件支架

    公开(公告)号：WO2014081500A3

    公开(公告)日：2014-08-21

    申请号：PCT/US2013059746

    申请日：2013-09-13

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： ROBERTSON THOMAS J ,  CLARKSON STEVEN ,  COSTA MARK W

    IPC: F16M13/00

    CPC classification number: F02C7/32 ,  F01D21/045 ,  F02C7/20 ,  F05D2220/32 ,  F05D2240/90 ,  F05D2260/30 ,  F05D2260/311

    Abstract: A mount for mounting a component to a gas turbine engine is disclosed. The mount may include a central portion that attaches to the component, and a flange circumscribing the central portion and extending to the gas turbine engine, the flange including a fusible region that breaks at a predetermined load. A method for protecting a component mounted to a gas turbine engine is also disclosed. The method may include attaching a mount to a casing of the gas turbine engine, the mount including a fusible region that breaks at a predetermined load. The method may further include attaching the component to the mount. The method may further include the fusible region breaking when the mount experiences the predetermined load, detaching the component from the casing of the gas turbine engine.

    Abstract translation: 公开了一种用于将部件安装到燃气涡轮发动机的支架。 所述安装件可以包括附接到所述部件的中央部分和限定所述中央部分并且延伸到所述燃气涡轮发动机的凸缘，所述凸缘包括在预定载荷下断裂的可熔区域。 还公开了一种用于保护安装到燃气涡轮发动机的部件的方法。 该方法可以包括将安装件附接到燃气涡轮发动机的壳体，安装件包括在预定负载下断裂的可熔区域。 该方法可以进一步包括将部件附接到安装件。 该方法可进一步包括当安装件经历预定负载时可熔区断裂，从燃气涡轮发动机的壳体分离该部件。

    RECIRCULATION SEAL FOR USE IN A GAS TURBINE ENGINE
    3.
    发明申请
    RECIRCULATION SEAL FOR USE IN A GAS TURBINE ENGINE 审中-公开
    在气体涡轮发动机中使用的再循环密封

    公开(公告)号：WO2015084460A3

    公开(公告)日：2015-08-20

    申请号：PCT/US2014056552

    申请日：2014-09-19

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： ROBERTSON THOMAS J ,  MCPHAIL JAMES J

    IPC: F02C7/28 ,  F01D11/00

    CPC classification number: F01D11/005 ,  F01D5/02 ,  F01D11/001 ,  F02C7/04 ,  F02C7/28 ,  F05D2220/32 ,  F05D2220/36 ,  F05D2240/24 ,  F05D2240/55 ,  F16J15/04

    Abstract: A recirculation seal for use within a gas turbine engine. The recirculation seal includes a first seal base, including a first seal base axis. The recirculation seal further includes a second seal base, including a second seal base axis The recirculation seal further includes a resilient bulb member coupled to the first seal base. The resilient bulb member includes an exterior bulb wall and an interior bulb wall, wherein the interior bulb wall defines an interior space.

    Abstract translation: 用于燃气涡轮发动机内的再循环密封。 再循环密封件包括第一密封基座，包括第一密封基座轴线。 再循环密封件还包括第二密封基座，包括第二密封基座轴线。再循环密封件还包括联接到第一密封基座的弹性球形部件。 弹性灯泡构件包括外部灯泡壁和内部灯泡壁，其中内部灯泡壁限定内部空间。

    AUXILIARY COMPONENT MOUNTS
    7.
    发明公开
    AUXILIARY COMPONENT MOUNTS 审中-公开
    辅助元件CARRIER

    公开(公告)号：EP2901067A4

    公开(公告)日：2016-05-25

    申请号：EP13856339

    申请日：2013-09-13

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： ROBERTSON THOMAS J ,  CLARKSON STEVEN ,  COSTA MARK W

    IPC: F16M13/00 ,  F01D21/04 ,  F02C7/32

    CPC classification number: F02C7/32 ,  F01D21/045 ,  F02C7/20 ,  F05D2220/32 ,  F05D2240/90 ,  F05D2260/30 ,  F05D2260/311

    Abstract: A mount for mounting a component to a gas turbine engine is disclosed. The mount may include a central portion that attaches to the component, and a flange circumscribing the central portion and extending to the gas turbine engine, the flange including a fusible region that breaks at a predetermined load. A method for protecting a component mounted to a gas turbine engine is also disclosed. The method may include attaching a mount to a casing of the gas turbine engine, the mount including a fusible region that breaks at a predetermined load. The method may further include attaching the component to the mount. The method may further include the fusible region breaking when the mount experiences the predetermined load, detaching the component from the casing of the gas turbine engine.

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