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

    公开(公告)号:US20130319011A1

    公开(公告)日:2013-12-05

    申请号:US13488754

    申请日:2012-06-05

    摘要: 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.

    摘要翻译: 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。

    Gas turbine engine geared architecture axial retention arrangement
    2.
    发明授权
    Gas turbine engine geared architecture axial retention arrangement 有权
    燃气轮机发动机齿轮架构轴向保持装置

    公开(公告)号:US08790075B2

    公开(公告)日:2014-07-29

    申请号:US13435353

    申请日:2012-03-30

    摘要: 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.

    摘要翻译: 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。

    Geared architecture carrier torque frame assembly
    3.
    发明授权
    Geared architecture carrier torque frame assembly 有权
    齿轮架架式扭矩架总成

    公开(公告)号:US09267389B2

    公开(公告)日:2016-02-23

    申请号:US13488754

    申请日:2012-06-05

    IPC分类号: F01D15/12

    摘要: 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.

    摘要翻译: 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。

    GAS TURBINE ENGINE GEARED ARCHITECTURE AXIAL RETENTION ARRANGEMENT
    4.
    发明申请
    GAS TURBINE ENGINE GEARED ARCHITECTURE AXIAL RETENTION ARRANGEMENT 有权
    气体涡轮发动机齿轮架构轴承保持装置

    公开(公告)号:US20130259657A1

    公开(公告)日:2013-10-03

    申请号:US13435353

    申请日:2012-03-30

    IPC分类号: F02C7/36 B23P6/00 F01D15/12

    摘要: 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.

    摘要翻译: 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。

    Gas turbine engine geared architecture axial retention arrangement
    5.
    发明授权
    Gas turbine engine geared architecture axial retention arrangement 有权
    燃气轮机发动机齿轮架构轴向保持装置

    公开(公告)号:US08517670B1

    公开(公告)日:2013-08-27

    申请号:US13557491

    申请日:2012-07-25

    摘要: 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.

    摘要翻译: 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。

    JOURNAL BEARING WITH SINGLE UNIT JUMPER TUBE AND FILTER
    7.
    发明申请
    JOURNAL BEARING WITH SINGLE UNIT JUMPER TUBE AND FILTER 有权
    JOURNAL轴承与单个单元弯管和过滤器

    公开(公告)号:US20100317478A1

    公开(公告)日:2010-12-16

    申请号:US12627117

    申请日:2009-11-30

    IPC分类号: F16H57/04 F16C33/10

    摘要: A journal bearing includes a central body having first passageway and a filter module. The central body extends axially and is adapted to be supported at each outer end. The first passageway extends generally axially through a portion of the central body. The filter module is disposed in the first passageway and is configured to trap debris from a lubricant fluid flowing therethrough. In one embodiment, the filter module is adapted to be inserted and removed from the first passageway as a single unit, thereby allowing the filter module to be connected and disconnected from fluid communication with a lubricant manifold positioned adjacent the journal bearing.

    摘要翻译: 轴颈轴承包括具有第一通道和过滤器模块的中心体。 中心体轴向延伸并适于在每个外端被支撑。 第一通道大致轴向延伸穿过中心体的一部分。 过滤器模块设置在第一通道中,并且被配置为从流过其中的润滑剂流体捕获碎屑。 在一个实施例中,过滤器模块适于作为单个单元从第一通道插入和移除,从而允许过滤器模块与位于轴颈轴承附近的润滑剂歧管的流体连通和断开。

    COUPLING SYSTEM FOR A STAR GEAR TRAIN IN A GAS TURBINE ENGINE
    8.
    发明申请
    COUPLING SYSTEM FOR A STAR GEAR TRAIN IN A GAS TURBINE ENGINE 有权
    气动涡轮发动机中的星形齿轮的耦合系统

    公开(公告)号:US20130178327A1

    公开(公告)日:2013-07-11

    申请号:US13605732

    申请日:2012-09-06

    IPC分类号: F16H1/28

    摘要: A star gear train for use in a gas turbine engine includes a sun gear, a ring gear, a plurality of star gears and a coupling system. The sun gear is rotatable by a shaft. The ring gear is secured to a ring gear shaft. Each of the plurality of star gears is rotatably mounted in a star carrier and meshes with the sun gear and the ring gear. The coupling system comprises a sun gear flexible coupling, a carrier flexible coupling and a deflection limiter. The sun gear flexible coupling connects the sun gear to the shaft. The carrier flexible coupling connects the carrier to a non-rotating mechanical ground. The deflection limiter is connected to the star carrier to limit excessive radial and circumferential displacement of the star gear train.

    摘要翻译: 用于燃气涡轮发动机的星形齿轮系包括太阳齿轮,齿圈,多个星形齿轮和联接系统。 太阳齿轮通过轴可旋转。 齿圈固定在齿圈轴上。 多个星形齿轮中的每一个可旋转地安装在星形载体中并与太阳轮和环形齿轮啮合。 耦合系统包括太阳齿轮柔性联轴器,托架柔性联轴器和偏转限制器。 太阳齿轮柔性联轴器将太阳齿轮连接到轴。 载体柔性联轴器将载体连接到非旋转机械接地。 偏转限制器连接到星形载体以限制星形齿轮系的过大的径向和周向位移。

    FLEXIBLE SHAFT FOR GAS TURBINE ENGINE
    9.
    发明申请
    FLEXIBLE SHAFT FOR GAS TURBINE ENGINE 有权
    气动涡轮发动机柔性轴

    公开(公告)号:US20100150702A1

    公开(公告)日:2010-06-17

    申请号:US12710863

    申请日:2010-02-23

    IPC分类号: F16C1/00 F04D29/08 F04D29/043

    摘要: A shaft for a gas turbine engine is provided that includes a first shaft section, a second shaft section, a first flexible linkage, and a second flexible linkage. The first shaft section extends between a forward axial end and an aft axial end along a first axial centerline. The second shaft section extends between a forward axial end and an aft axial end along a second axial centerline. The first flexible linkage includes a bridge section connected between a first diaphragm and a second diaphragm. The first diaphragm is connected to the aft axial end of the first shaft section. The second diaphragm is connected to the forward axial end of the second shaft section. The second flexible linkage includes a diaphragm and a hub. The second flexible linkage diaphragm cantilevers radially outwardly from an inner radial end to an outer radial end, and is connected to the aft axial end of the second shaft section. The hub is connected to the outer radial end of the second flexible linkage diaphragm, and includes an engine shaft coupling connected to the hub.

    摘要翻译: 提供了一种用于燃气涡轮发动机的轴,其包括第一轴部分,第二轴部分,第一柔性连杆机构和第二柔性连杆机构。 第一轴部段沿着第一轴向中心线在前轴向端部和后轴向端部之间延伸。 第二轴部段沿着第二轴向中心线在前轴向端部和后轴向端部之间延伸。 第一柔性联动装置包括连接在第一膜片和第二膜片之间的桥接部分。 第一隔膜连接到第一轴段的后轴向端。 第二隔膜连接到第二轴段的前轴向端。 第二柔性联动装置包括隔膜和轮毂。 第二柔性连接隔膜从内径向端部径向向外延伸到外径向端部,并且连接到第二轴部的后轴向端部。 轮毂连接到第二柔性连接隔膜的外径向端,并且包括连接到轮毂的发动机轴联轴器。

    Coupling system for a star gear train in a gas turbine engine
    10.
    发明授权
    Coupling system for a star gear train in a gas turbine engine 有权
    燃气涡轮发动机中星形齿轮系的联接系统

    公开(公告)号:US08585539B2

    公开(公告)日:2013-11-19

    申请号:US13605732

    申请日:2012-09-06

    IPC分类号: F16H57/08

    摘要: A star gear train for use in a gas turbine engine includes a sun gear, a ring gear, a plurality of star gears and a coupling system. The sun gear is rotatable by a shaft. The ring gear is secured to a ring gear shaft. Each of the plurality of star gears is rotatably mounted in a star carrier and meshes with the sun gear and the ring gear. The coupling system comprises a sun gear flexible coupling, a carrier flexible coupling and a deflection limiter. The sun gear flexible coupling connects the sun gear to the shaft. The carrier flexible coupling connects the carrier to a non-rotating mechanical ground. The deflection limiter is connected to the star carrier to limit excessive radial and circumferential displacement of the star gear train.

    摘要翻译: 用于燃气涡轮发动机的星形齿轮系包括太阳齿轮,齿圈,多个星形齿轮和联接系统。 太阳齿轮通过轴可旋转。 齿圈固定在齿圈轴上。 多个星形齿轮中的每一个可旋转地安装在星形载体中并与太阳轮和环形齿轮啮合。 耦合系统包括太阳齿轮柔性联轴器,托架柔性联轴器和偏转限制器。 太阳齿轮柔性联轴器将太阳齿轮连接到轴。 载体柔性联轴器将载体连接到非旋转机械接地。 偏转限制器连接到星形载体以限制星形齿轮系的过大的径向和周向位移。