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    FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE
    133.
    发明申请
    FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE 审中-公开
    用于齿轮式建筑燃气涡轮发动机的灵活支撑结构

    公开(公告)号：US20160053635A1

    公开(公告)日：2016-02-25

    申请号：US14859381

    申请日：2015-09-21

    Applicant: United Technologies Corporation

    Inventor： Michael E. McCune ,  Jason Husband

    IPC: F01D25/16 ,  F01D15/12 ,  F01D25/28

    CPC classification number: F02C7/36 ,  F01D5/06 ,  F01D9/02 ,  F01D15/12 ,  F01D25/16 ,  F01D25/164 ,  F01D25/28 ,  F02C7/32 ,  F02K3/06 ,  F04D19/02 ,  F04D25/045 ,  F04D29/053 ,  F04D29/056 ,  F04D29/321 ,  F04D29/325 ,  F05D2220/32 ,  F05D2240/60 ,  F05D2260/40311 ,  F05D2260/96 ,  Y02T50/671 ,  Y10T29/49321

    Abstract: A gas turbine engine according to an example of the present disclosure includes, among other things, a fan shaft configured to drive a fan, a support configured to support at least a portion of the fan shaft, the support defining a support transverse stiffness and a support lateral stiffness, a gear system coupled to the fan shaft, and a flexible support configured to at least partially support the gear system. The flexible support defines a flexible support transverse stiffness with respect to the support transverse stiffness and a flexible support lateral stiffness with respect to the support lateral stiffness. The input defines an input transverse stiffness with respect to the support transverse stiffness and an input lateral stiffness with respect to the support lateral stiffness.

    Abstract translation: 根据本公开的示例的燃气涡轮发动机尤其包括构造成驱动风扇的风扇轴，构造成支撑风扇轴的至少一部分的支撑件，支撑件限定支撑横向刚度和 支撑横向刚度，耦合到所述风扇轴的齿轮系统以及被配置为至少部分地支撑所述齿轮系统的柔性支撑件。 柔性支撑件相对于支撑横向刚度和相对于支撑横向刚度的柔性支撑横向刚度限定了柔性支撑横向刚度。 该输入定义了相对于支撑横向刚度的输入横向刚度和相对于支撑横向刚度的输入侧向刚度。

    Turbine engine gearbox
    135.
    发明授权
    Turbine engine gearbox 有权
    涡轮发动机变速箱

    公开(公告)号：US09222416B2

    公开(公告)日：2015-12-29

    申请号：US14470982

    申请日：2014-08-28

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Michael E. McCune

    IPC: F16H1/28 ,  F02C7/36 ,  F16H1/46 ,  F01D15/12 ,  F02K3/072 ,  F16H57/00

    CPC classification number: F02C7/36 ,  F01D15/12 ,  F02K3/04 ,  F02K3/072 ,  F05D2260/40311 ,  F16H1/28 ,  F16H1/46 ,  F16H57/0006 ,  Y02T50/671

    Abstract: A gas turbine engine comprises a fan, a compressor, a combustor, and a fan drive turbine rotor. The fan drive turbine drives the fan through a gear reduction. The gear reduction includes at least two double helical gears in meshed engagement. Each of the at least two double helical gears are disposed to rotate about respective axes, and each have a first plurality of gear teeth axially spaced from a second plurality of gear teeth by a spacer. Each of the first plurality of gear teeth has a first end facing the spacer and each of the second plurality of gear teeth has a first end facing the spacer. Each first end of the first plurality of gear teeth is circumferentially offset from each first end of the second plurality of gear teeth. A method is also disclosed.

    Abstract translation: 燃气涡轮发动机包括风扇，压缩机，燃烧器和风扇驱动涡轮机转子。 风扇驱动涡轮驱动风扇通过齿轮减速。 齿轮减速包括至少两个啮合啮合的双斜齿轮。 所述至少两个双螺旋齿轮中的每一个设置成围绕相应的轴线旋转，并且每个具有通过间隔件与第二多个齿轮齿轴向间隔开的第一多个齿轮齿。 第一多个齿轮齿中的每一个具有面向间隔件的第一端，并且第二多个齿轮齿中的每一个具有面向间隔件的第一端。 第一多个齿轮齿的每个第一端从第二多个齿轮齿的每个第一端周向地偏移。 还公开了一种方法。

    GAS TURBINE ENGINE WITH DISTRIBUTED FANS WITH DRIVE CONTROL
    136.
    发明申请
    GAS TURBINE ENGINE WITH DISTRIBUTED FANS WITH DRIVE CONTROL 审中-公开
    具有驱动控制的分布式风扇的气体涡轮发动机

    公开(公告)号：US20150361880A1

    公开(公告)日：2015-12-17

    申请号：US14600487

    申请日：2015-01-20

    Applicant: United Technologies Corporation

    Inventor： Gabriel L. Suciu ,  Wesley K. Lord ,  Jesse M. Chandler ,  Michael Winter ,  Michael E. McCune ,  William G. Sheridan

    IPC: F02C3/10 ,  F01D15/10

    CPC classification number: F02C3/10 ,  B64D27/12 ,  B64D35/04 ,  F02C3/107 ,  F02K3/00 ,  F02K3/077

    Abstract: A gas turbine engine comprises a plurality of fan rotors. A gas generator comprises at least one compressor rotor, at least one gas generator turbine rotor, a combustion section, and a fan drive turbine downstream of at least one gas generator turbine rotor. A shaft is configured to be driven by the fan drive turbine. The shaft engages gears to drive the plurality of fan rotors. A system controls the amount of power supplied to the plurality of fan rotors. A method of operating a gas turbine engine is also disclosed.

    Abstract translation: 燃气涡轮发动机包括多个风扇转子。 气体发生器包括至少一个压缩机转子，至少一个气体发生器涡轮机转子，燃烧部分和在至少一个气体发生器涡轮机转子下游的风扇驱动涡轮机。 轴构造成由风扇驱动涡轮机驱动。 轴接合齿轮以驱动多个风扇转子。 系统控制提供给多个风扇转子的功率量。 还公开了一种操作燃气涡轮发动机的方法。

    Uninterruptible oil supply in planetary system
    138.
    发明授权
    Uninterruptible oil supply in planetary system 有权
    行星系统不间断供油

    公开(公告)号：US08968141B2

    公开(公告)日：2015-03-03

    申请号：US13947158

    申请日：2013-07-22

    Applicant: United Technologies Corporation

    Inventor： Loc Quang Duong ,  Lawrence E. Portlock ,  Michael E. McCune

    IPC: F16H57/04 ,  F16H57/08

    CPC classification number: F16H57/042 ,  F16H57/045 ,  F16H57/0471 ,  F16H57/0479 ,  F16H57/0482 ,  F16H57/082

    Abstract: A planetary carrier includes a journal bearing for supporting a planetary gear. The journal bearing receives lubricant to produce a lubricant film to support gear loads. A torque frame is attached to the carrier housing to transmit torque and to prevent twisting of the carrier housing. The torque frame includes several lubricant communication passages to provide lubricant to each of the separate journal bearings. Each of the lubricant communication passages includes an accumulator for storing lubricant during normal operation. The accumulator stores a desired amount of lubricant to provide lubricant to the adjacent journal bearing for the interim period between primary system stoppage and reestablishment of lubricant flow by a secondary system.

    Abstract translation: 行星架包括用于支撑行星齿轮的轴颈轴承。 轴颈轴承接收润滑剂以产生润滑剂膜以支撑齿轮负载。 扭矩框架附接到承载壳体以传递扭矩并且防止承载壳体的扭转。 扭矩框架包括若干润滑剂连通通道，以向每个单独的轴颈轴承提供润滑剂。 每个润滑剂连通通道包括用于在正常操作期间储存润滑剂的储液器。 蓄能器存储所需量的润滑剂，以在主系统停止和辅助系统重新建立润滑剂流动之间的临时期间向邻近的轴颈轴承提供润滑剂。

    PLANETARY GEAR SYSTEM ARRANGEMENT WITH AUXILIARY OIL SYSTEM
    139.
    发明申请
    PLANETARY GEAR SYSTEM ARRANGEMENT WITH AUXILIARY OIL SYSTEM 审中-公开
    辅助油系统布置与辅助油系统

    公开(公告)号：US20140369818A1

    公开(公告)日：2014-12-18

    申请号：US14474869

    申请日：2014-09-02

    Applicant: United Technologies Corporation

    Inventor： Michael E. McCune ,  William G. Sheridan ,  Lawrence E. Portlock

    IPC: F02C7/06 ,  F01D25/18 ,  F02C7/36 ,  F01D25/16

    CPC classification number: F01N3/208 ,  F01D25/16 ,  F01D25/18 ,  F01N3/2066 ,  F01N11/00 ,  F01N2610/01 ,  F01N2610/02 ,  F01N2610/1406 ,  F01N2610/142 ,  F01N2610/148 ,  F01N2900/1814 ,  F02C3/10 ,  F02C7/06 ,  F02C7/10 ,  F02C7/36 ,  F02K3/06 ,  F05D2260/40311 ,  F16N7/34 ,  Y02T10/24 ,  Y02T50/671 ,  Y10T29/4932 ,  Y10T137/0324 ,  Y10T137/7297

    Abstract: A gas turbine engine includes a fan, a speed reduction device driving the fan and a lubrication system for lubricating components across a rotation gap. The lubrication system includes a lubricant input. A stationary first bearing receives lubricant from the lubricant input and has a first race in which lubricant flows and a second race. A second bearing for rotation is within the first bearing including a first opening in registration with the first race such that lubricant may flow from the first race through the first opening into a first conduit. There is a rotating carrier for supporting at least one planetary gear. The second bearing extends from the rotating carrier about an axis. A first spray bar is disposed on the carrier. The second bearing has a second opening in registration with the second race and a second conduit for passing lubricant to the spray bar.

    Abstract translation: 燃气涡轮发动机包括风扇，驱动风扇的减速装置和用于沿旋转间隙润滑部件的润滑系统。 润滑系统包括润滑油输入。 固定的第一轴承从润滑剂输入端接收润滑剂并且具有其中润滑剂流动的第一种族和第二种族。 用于旋转的第二轴承在第一轴承内，包括与第一座圈对准的第一开口，使得润滑剂可以从第一座圈通过第一开口流入第一管道。 存在用于支撑至少一个行星齿轮的旋转载体。 第二轴承围绕轴线从旋转载体延伸。 第一喷杆设置在载体上。 第二轴承具有与第二座圈对准的第二开口和用于将润滑剂传送到喷杆的第二导管。

    Journal pin oil supply for gear system
    140.
    发明授权
    Journal pin oil supply for gear system 有权
    齿轮系统的针脚供油

    公开(公告)号：US08894529B2

    公开(公告)日：2014-11-25

    申请号：US14204031

    申请日：2014-03-11

    Applicant: United Technologies Corporation

    Inventor： Michael E. McCune

    IPC: F16H1/48 ,  F16H57/04 ,  F16C33/02 ,  F02C7/32 ,  F16H57/08

    CPC classification number: F16H57/043 ,  F02C7/32 ,  F05D2260/40311 ,  F16C33/02 ,  F16H57/0479 ,  F16H2057/085 ,  Y02T50/671 ,  Y10T29/49464

    Abstract: An example journal pin includes a generally cylindrical body disposed on an axis having a supply passage. A first chamber and a second chamber are disposed in the generally cylindrical body and are in fluid communication with the supply passage. A recess on an outer diameter of the cylindrical body is in fluid communication with the first chamber and the second chamber. The first chamber and second chamber are each radially outward of the supply passage and including an outlet to the recess. The first chamber and second chamber each have a first section radially inward of a second section. A cross sectional area of the second section is greater than a cross sectional area of the corresponding first section.

    Abstract translation: 示例轴颈销包括设置在具有供给通道的轴线上的大致圆柱形的主体。 第一腔室和第二腔室设置在大致圆柱形的本体中并且与供应通道流体连通。 圆筒体的外径上的凹部与第一腔室和第二腔室流体连通。 第一腔室和第二腔室各自在供应通道的径向外侧并且包括到凹部的出口。 第一室和第二室各自具有第二部分的径向内侧的第一部分。 第二部分的横截面面积大于对应的第一部分的横截面面积。

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