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    GEARED ARCHITECTURE CARRIER TORQUE FRAME ASSEMBLY
    1.
    发明申请
    GEARED ARCHITECTURE CARRIER TORQUE FRAME ASSEMBLY 审中-公开
    齿轮架构承载架扭矩组件

    公开(公告)号：WO2014028089A3

    公开(公告)日：2014-04-24

    申请号：PCT/US2013042808

    申请日：2013-05-28

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： PESCOSOLIDO ALESSIO ,  MULDOON MARC J ,  COFFIN JAMES B

    IPC: F02C7/36 ,  F01D15/12 ,  F16H57/04

    CPC classification number: F01D15/12 ,  F05D2260/31 ,  F05D2260/40311 ,  F16H57/025 ,  F16H57/082 ,  Y02T50/671 ,  Y10T29/49229

    Abstract: A fan drive gear system for a gas turbine engine includes a carrier supporting circumferentially arranged gears within gear mount sections spaced circumferentially about a periphery. A shelf is disposed between each of the gear mounting sections. A torque frame is attached to the carrier and includes circumferentially arranged finger sections. Each of the finger sections includes first and second ends that are spaced apart to receive the shelf. A pin extends through openings in the shelf and first and second ends to secure the torque frame to the carrier.

    Abstract translation: 用于燃气涡轮发动机的风扇驱动齿轮系统包括支撑围绕周边间隔开的齿轮安装部分内的周向布置的齿轮的托架。 在每个齿轮安装部之间设置有搁板。 扭矩框架附接到载体并且包括周向布置的指状部分。 每个指状部分包括间隔开以接收搁板的第一端和第二端。 销延伸穿过搁板和第一和第二端的开口，以将扭矩框固定到托架上。

    INSEPARABLE MACHINED LUBRICANT MANIFOLD
    3.
    发明申请
    INSEPARABLE MACHINED LUBRICANT MANIFOLD 审中-公开
    不可分割的机器润滑剂歧管

    公开(公告)号：WO2015047514A2

    公开(公告)日：2015-04-02

    申请号：PCT/US2014045335

    申请日：2014-07-03

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： OTTO JOHN R ,  BAKER STEPHANIE M ,  COFFIN JAMES B

    IPC: F16H57/04

    CPC classification number: F16H57/0424 ,  F01D25/18 ,  F02C7/06 ,  F02K3/06 ,  F04D29/063 ,  F05D2220/36 ,  F05D2230/60 ,  F05D2240/30 ,  F05D2260/36 ,  F05D2260/40311 ,  F05D2260/98

    Abstract: A lubricant manifold for gear system of a turbofan engine includes a base plate defining an inlet, an outlet and a plurality of open channels. The open channels define a portion of a corresponding plurality of lubricant passages. A cover plate is attached to the base plate to complete the formation of the plurality of lubricant passages. An interlocking interface between the base plate and the cover plate secures the cover plate to the base plate.

    Abstract translation: 用于涡扇发动机的齿轮系统的润滑剂歧管包括限定入口，出口和多个开放通道的基板。 开放通道限定了相应的多个润滑剂通道的一部分。 盖板连接到基板上以完成多个润滑剂通道的形成。 底板和盖板之间的互锁界面将盖板固定到底板上。

    TURBOFAN ENGINE ASSEMBLY METHODS
    4.
    发明申请
    TURBOFAN ENGINE ASSEMBLY METHODS 审中-公开
    涡轮发动机组装方法

    公开(公告)号：WO2014197080A3

    公开(公告)日：2015-03-05

    申请号：PCT/US2014027512

    申请日：2014-03-14

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： COFFIN JAMES B ,  PESCOSOLIDO ALESSIO

    IPC: F02C7/20 ,  F01D25/16 ,  F01D25/28 ,  F02C7/06

    CPC classification number: F01D25/16 ,  F01D25/28 ,  F02C7/36 ,  F02K3/06 ,  F05D2230/60 ,  F05D2230/68 ,  F05D2240/55 ,  F05D2260/40311

    Abstract: A method for assembling a turbofan engine (20) comprises coupling a bearing assembly (176) and a shaft (420) as a unit to a bearing support (453). A transmission (46) and the fan shaft (132) are installed to a front frame assembly (172). The bearing assembly and shaft are installed as a unit so that the shaft engages a central gear (52) of the transmission and the bearing support engages the front frame assembly.

    Abstract translation: 一种用于组装涡轮风扇发动机（20）的方法包括将轴承组件（176）和作为单元的轴（420）联接到轴承支撑件（453）。 变速器（46）和风扇轴（132）安装到前框架组件（172）上。 轴承组件和轴被安装为单元，使得轴接合变速器的中心齿轮（52）并且轴承支撑件接合前框架组件。

    TURBOMACHINE GEARED ARCHITECTURE SUPPORT ASSEMBLY
    5.
    发明申请
    TURBOMACHINE GEARED ARCHITECTURE SUPPORT ASSEMBLY 审中-公开
    涡轮机齿轮结构支撑组件

    公开(公告)号：WO2014025427A2

    公开(公告)日：2014-02-13

    申请号：PCT/US2013040536

    申请日：2013-05-10

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： HUSBAND JASON ,  COFFIN JAMES B

    CPC classification number: F02C3/107 ,  F02C7/36 ,  F02K3/06 ,  F04D25/028 ,  F05D2260/40311 ,  F05D2260/90 ,  Y10T29/49826

    Abstract: An example turbomachine geared architecture support assembly includes a compliant member configured to hold a geared architecture within a turbomachine. The compliant member has a compliant section that permits rotation of the geared architecture relative to a fixed portion of the turbomachine. A stop limits rotation of the geared architecture relative to the fixed portion of the turbomachine.

    Abstract translation: 示例涡轮机齿轮传动架构支撑组件包括被配置为将齿轮架构保持在涡轮机内的顺应性构件。 柔性构件具有允许齿轮架构相对于涡轮机械的固定部分旋转的柔性部分。 停止限制齿轮架构相对于涡轮机的固定部分的旋转。

    GAS TURBINE ENGINE GEARED ARCHITECTURE AXIAL RETENTION ARRANGEMENT
    6.
    发明申请
    GAS TURBINE ENGINE GEARED ARCHITECTURE AXIAL RETENTION ARRANGEMENT 审中-公开
    气体涡轮发动机齿轮架构轴承保持装置

    公开(公告)号：WO2014007881A2

    公开(公告)日：2014-01-09

    申请号：PCT/US2013033795

    申请日：2013-03-26

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： COFFIN JAMES B ,  PESCOSOLIDO ALESSIO

    IPC: F02C7/36 ,  B23P6/00 ,  F01D15/12

    CPC classification number: F02C7/20 ,  B64D27/26 ,  B64D2027/266 ,  F01D21/045 ,  F01D25/16 ,  F02C7/36 ,  F05D2220/36 ,  F05D2260/40311 ,  Y10T29/49318

    Abstract: A support assembly for a geared architecture includes an engine static structure. A flex support is secured to the engine static structure and includes a bellow. A support structure is operatively secured to the flex support. A geared architecture is mounted to the support structure. First members are removably secured to one of the engine static structure and the flex support and second members are removably secured to the support structure. The first and second members are circumferentially aligned with one another and spaced apart from one another during a normal operating condition. The first and second members are configured to be engageable with one another during an extreme event to limit axial movement of the geared architecture relative to the engine static structure.

    Abstract translation: 用于齿轮架构的支撑组件包括发动机静态结构。 柔性支撑件固定在发动机静态结构上，并包括一个波纹管。 支撑结构可操作地固定到柔性支撑件上。 齿轮架构安装在支撑结构上。 第一构件可移除地固定到发动机静态结构和柔性支撑件之一，并且第二构件可移除地固定到支撑结构。 第一和第二构件在正常操作条件下彼此周向对准并且彼此间隔开。 第一和第二构件被配置为在极端事件期间可彼此接合以限制齿轮架构相对于发动机静态结构的轴向移动。

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