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    Connection for generator in a gas turbine engine
    1.
    发明授权
    Connection for generator in a gas turbine engine 有权
    燃气轮机发电机连接

    公开(公告)号：US09169780B2

    公开(公告)日：2015-10-27

    申请号：US13183848

    申请日：2011-07-15

    Applicant: Barry Barnett ,  Daniel Alecu ,  Andreas Eleftheriou

    Inventor： Barry Barnett ,  Daniel Alecu ,  Andreas Eleftheriou

    IPC: F02C7/06 ,  F02C7/32 ,  F02C7/36

    CPC classification number: F02C7/06 ,  F02C7/32 ,  F02C7/36 ,  F05D2260/202

    Abstract: A gas turbine engine having an electric generator includes a transmission shaft extending along a longitudinal axis of the engine and drivingly interconnecting a turbine shaft of the engine and a rotor shaft of the electric generator. The transmission shaft is engaged by splined mating connections with the turbine shaft and the rotor shaft. The transmission shaft has a shear neck defining a reduced radial wall thickness with respect to a remainder of the transmission shaft such as to provide a weakened region of the transmission shaft. An annular support structure, concentric with and surrounding the transmission shaft, is axially located between the shear neck and a forward end of the transmission shaft engaged to the turbine shaft, and includes a bearing operable to rotationally support the transmission shaft.

    Abstract translation: 具有发电机的燃气涡轮发动机包括：沿着发动机的纵轴延伸的传动轴，并将发动机的涡轮轴与发电机的转子轴驱动连接。 传动轴通过与涡轮轴和转子轴的花键配合连接接合。 传动轴具有剪切颈部，其相对于传动轴的其余部分限定径向壁厚度减小，以便提供传动轴的弱化区域。 与传动轴同心并且围绕传动轴的环形支撑结构轴向地位于剪切颈部和接合到涡轮轴的传动轴的前端之间，并且包括可操作以可旋转地支撑传动轴的轴承。

    Fan hub design
    2.
    发明授权
    Fan hub design 有权
    风扇轮毂设计

    公开(公告)号：US09169730B2

    公开(公告)日：2015-10-27

    申请号：US13297300

    申请日：2011-11-16

    Applicant: Barry Barnett

    Inventor： Barry Barnett

    IPC: F01D5/14 ,  F02K3/06

    CPC classification number: F01D5/30 ,  F01D5/02 ,  F01D5/14 ,  F02K3/06 ,  F05D2220/32 ,  F05D2240/20 ,  F05D2260/941

    Abstract: A fan rotor has a fan web and a plurality of circumferentially spaced-apart fan blades extending radially outwardly from an outer rim of the fan web. The outer rim is integrally connected to an inner rim through an axially facing web section. The web section has an inward concavature and extends aft of the center of gravity of the fan blades to shift the center of gravity of the hub rearwards while maintaining airfoil stress below critical levels. The rim section may have an inwardly projecting annular channel formed in a leading edge thereof and tuned to the 2M3ND mode of the fan hub.

    Abstract translation: 风扇转子具有风扇腹板和从风扇腹板的外缘径向向外延伸的多个周向间隔开的风扇叶片。 外缘通过轴向面对的腹板部分整体连接到内缘。 腹板部分具有向内的凹陷并且延伸到风扇叶片的重心的后方，以使桨毂的重心向后移动，同时保持翼型压力低于临界水平。 边缘部分可以具有形成在其前缘中的向内突出的环形通道并且被调谐到风扇轮毂的2M3ND模式。

    Foreign object damage resistant vane assembly
    4.
    发明授权
    Foreign object damage resistant vane assembly 有权
    异物损坏叶片组件

    公开(公告)号：US07494316B2

    公开(公告)日：2009-02-24

    申请号：US11468036

    申请日：2006-08-29

    Applicant: Barry Barnett ,  David Denis

    Inventor： Barry Barnett ,  David Denis

    IPC: F03B11/02

    CPC classification number: F01D9/042 ,  F02C7/05 ,  F05D2260/30

    Abstract: A vane including a root, a tip and an airfoil portion extending between the root and the tip, the vane also including a button portion interconnecting the airfoil portion and the root. The button portion protrudes beyond a profile of the airfoil a distance less than the root. The button portion includes leading and trailing ends free of sharp edges. The leading and trailing ends respectively protrude beyond leading and trailing edges of the airfoil portion.

    Abstract translation: 叶片包括根部，尖端和在根部和尖端之间延伸的翼型部分，叶片还包括将翼型部分和根部相互连接的按钮部分。 按钮部分突出超过翼型的轮廓，其距离小于根部。 按钮部分包括没有锋利边缘的前端和后端。 前端和尾端分别突出超过翼型部分的前缘和后缘。

    COUPLING ELEMENT FOR TORQUE TRANSMISSION IN A GAS TURBINE ENGINE
    7.
    发明申请
    COUPLING ELEMENT FOR TORQUE TRANSMISSION IN A GAS TURBINE ENGINE 有权
    燃气轮机发动机扭矩传递的耦合元件

    公开(公告)号：US20140116061A1

    公开(公告)日：2014-05-01

    申请号：US13660039

    申请日：2012-10-25

    Applicant: Barry BARNETT ,  Phillipe BONNIERE ,  Daniel ALECU

    Inventor： Barry BARNETT ,  Phillipe BONNIERE ,  Daniel ALECU

    IPC: F16D3/80 ,  F02C7/12

    CPC classification number: F16D1/101 ,  F01D5/026 ,  F05D2260/20 ,  F16D2001/103 ,  Y02T50/675 ,  Y10T403/25 ,  Y10T464/10

    Abstract: A gas turbine engine having a coupling element for coupling a first shaft to a second shaft, the second shaft being substantially axially aligned with the first shaft, the coupling element provided with an exterior surface that engages an opposing interior surface of the first shaft and an interior surface that engages an opposing exterior surface of the second shaft to facilitate torque transfer between the first shaft and the second shaft when rotated together, wherein the coupling element and at least one of the first and second shafts cooperate to define at least one fluid passageway therebetween.

    Abstract translation: 一种燃气涡轮发动机，其具有用于将第一轴联接到第二轴的联接元件，所述第二轴与所述第一轴基本上轴向对齐，所述联接元件设置有与所述第一轴的相对的内表面接合的外表面， 内表面，其接合所述第二轴的相对的外表面，以便当一起旋转时促进在所述第一轴和所述第二轴之间的扭矩传递，其中所述联接元件和所述第一和第二轴中的至少一个协作以限定至少一个流体通道 之间。

    Blade fixing design for protecting against low speed rotation induced wear
    8.
    发明授权
    Blade fixing design for protecting against low speed rotation induced wear 有权
    刀片固定设计，用于防止低速旋转引起的磨损

    公开(公告)号：US08708656B2

    公开(公告)日：2014-04-29

    申请号：US12786902

    申请日：2010-05-25

    Applicant: Barry Barnett ,  Philippe Bonniere

    Inventor： Barry Barnett ,  Philippe Bonniere

    IPC: F01D5/30

    CPC classification number: F01D5/3007 ,  F05D2260/30

    Abstract: The blade dovetails and associated dovetail slots of a gas turbine engine rotor assembly are shaped so that during windmilling the high stress regions of the blade dovetails are shielded from rubbing against the disk and vice versa. Bumper surfaces are provided in low stress regions of the dovetail assembly such that the windmilling contact points between the blade dovetails and the disk are in non-critical areas of the dovetail assembly.

    Abstract translation: 燃气涡轮发动机转子组件的叶片燕尾榫和相关联的燕尾槽成形为使得在风车期间，叶片燕尾榫的高应力区域被遮蔽而不与盘摩擦，反之亦然。 缓冲表面设置在燕尾组件的低应力区域中，使得叶片燕尾榫和盘之间的风向接触点位于燕尾组件的非关键区域。

    SUPPORT FOR ELECTRIC MACHINE IN A TURBINE ENGINE
    10.
    发明申请
    SUPPORT FOR ELECTRIC MACHINE IN A TURBINE ENGINE 有权
    涡轮发动机电机支持

    公开(公告)号：US20130133336A1

    公开(公告)日：2013-05-30

    申请号：US13304960

    申请日：2011-11-28

    Applicant: Barry Barnett ,  David Denis

    Inventor： Barry Barnett ,  David Denis

    IPC: F02C6/00 ,  F16M13/02 ,  B23P11/00

    CPC classification number: F01D25/164 ,  F01D15/10 ,  F01D25/04 ,  F02C7/20 ,  F02C7/32 ,  F05D2220/76 ,  Y02T50/671 ,  Y10T29/49009

    Abstract: Devices and methods for supporting an accessory (32) in a gas turbine engine (10) are disclosed. The accessory (32) may have an interface (36) for coupling to a shaft (24) of the gas turbine engine (10). The device may comprise a first support (38) configured to support a first portion (34) of the accessory (32) proximal the interface (36) and a second support (40) configured to support a second portion (35) of the accessory (32) distal from the interface (36). The second support (40) may be configured to provide a lower resistance to relative displacement between the accessory (32) and structure (42) of the engine (10) than does the first support (34).

    Abstract translation: 公开了一种在燃气涡轮发动机（10）中支撑附件（32）的装置和方法。 附件（32）可以具有用于联接到燃气涡轮发动机（10）的轴（24）的接口（36）。 该装置可以包括构造成支撑靠近接口（36）的附件（32）的第一部分（34）的第一支撑件（38）和构造成支撑附件的第二部分（35）的第二支撑件（40） （32）远离界面（36）。 第二支撑件（40）可以构造成比第一支撑件（34）提供对发动机（10）的附件（32）和结构（42）之间的相对位移的较低阻力。

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