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    COMPUTER-IMPLEMENTED METHOD, APPARATUS, AND COMPUTER PROGRAM PRODUCT FOR SECURING NODE PORT ACCESS IN A SWITCHED-FABRIC STORAGE AREA NETWORK
    1.
    发明申请
    COMPUTER-IMPLEMENTED METHOD, APPARATUS, AND COMPUTER PROGRAM PRODUCT FOR SECURING NODE PORT ACCESS IN A SWITCHED-FABRIC STORAGE AREA NETWORK 有权
    计算机实现的方法，装置和计算机程序产品，用于在开关式织物储存区域网络中保护节点端口访问

    公开(公告)号：US20070239989A1

    公开(公告)日：2007-10-11

    申请号：US11277653

    申请日：2006-03-28

    申请人： Barry Barnett ,  Daniel Eisenhauer ,  Matthew Landt

    发明人： Barry Barnett ,  Daniel Eisenhauer ,  Matthew Landt

    IPC分类号： H04L9/00

    CPC分类号： H04L67/1097 ,  H04L63/101

    摘要： A computer-implemented method, apparatus, and computer program product are disclosed for securing node port access in a switched-fabric storage area network. Permitted combinations of fabric port identifiers and node port identifiers are specified. A node port receives a request to access the node port. A node port identifier, which identifies the device that is attempting to access the node port, is determined from the request. A fabric port identifier is determined that identifies a fabric port through which the device transmitted the request. Access to the node port is granted if the fabric port identifier and node port identifier form a permitted combination.

    摘要翻译： 公开了一种计算机实现的方法，装置和计算机程序产品，用于保护交换式结构存储区域网络中的节点端口访问。 指定了Fabric端口标识符和节点端口标识符的允许组合。 节点端口接收到访问节点端口的请求。 根据请求确定标识尝试访问节点端口的设备的节点端口标识符。 确定结构端口标识符，其标识设备通过其发送请求的结构端口。 如果结构端口标识符和节点端口标识符形成允许的组合，则允许访问节点端口。

    Connection for generator in a gas turbine engine
    2.
    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

    申请人： Barry Barnett ,  Daniel Alecu ,  Andreas Eleftheriou

    发明人： Barry Barnett ,  Daniel Alecu ,  Andreas Eleftheriou

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

    CPC分类号： F02C7/06 ,  F02C7/32 ,  F02C7/36 ,  F05D2260/202

    摘要： 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.

    摘要翻译： 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
    3.
    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

    申请人： Barry Barnett

    发明人： Barry Barnett

    IPC分类号： F01D5/14 ,  F02K3/06

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

    摘要： 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.

    摘要翻译： 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
    5.
    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

    申请人： Barry Barnett ,  David Denis

    发明人： Barry Barnett ,  David Denis

    IPC分类号： F03B11/02

    CPC分类号： F01D9/042 ,  F02C7/05 ,  F05D2260/30

    摘要： 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.

    摘要翻译： 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
    8.
    发明授权
    Coupling element for torque transmission in a gas turbine engine 有权
    用于燃气涡轮发动机中的扭矩传递的耦合元件

    公开(公告)号：US09297422B2

    公开(公告)日：2016-03-29

    申请号：US13660039

    申请日：2012-10-25

    申请人： Barry Barnett ,  Phillipe Bonniere ,  Daniel Alecu

    发明人： Barry Barnett ,  Phillipe Bonniere ,  Daniel Alecu

    IPC分类号： F16D3/80 ,  F02C7/12 ,  F16D1/10 ,  F01D5/02

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

    摘要： 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.

    摘要翻译： 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。

    CONNECTION FOR GENERATOR IN A GAS TURBINE ENGINE
    9.
    发明申请
    CONNECTION FOR GENERATOR IN A GAS TURBINE ENGINE 有权
    发电机在气体发动机中的连接

    公开(公告)号：US20130014513A1

    公开(公告)日：2013-01-17

    申请号：US13183848

    申请日：2011-07-15

    申请人： Barry Barnett ,  Daniel Alecu ,  Andreas Eleftheriou

    发明人： Barry Barnett ,  Daniel Alecu ,  Andreas Eleftheriou

    IPC分类号： F02C6/00

    CPC分类号： F02C7/06 ,  F02C7/32 ,  F02C7/36 ,  F05D2260/202

    摘要： 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.

    摘要翻译： 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。