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    WIRELESS TELEMETRY SYSTEM FOR A TURBINE ENGINE
    1.
    发明申请
    WIRELESS TELEMETRY SYSTEM FOR A TURBINE ENGINE 有权
    涡轮发动机无线电报系统

    公开(公告)号：US20120197597A1

    公开(公告)日：2012-08-02

    申请号：US13018469

    申请日：2011-02-01

    Applicant: David J. Mitchell ,  Ramesh Subramanian ,  Cora Schillig ,  Anand A. Kulkarni ,  Vinay Jonnalagadda ,  Bulent Acar ,  Sankar Nellian ,  James P. Williams ,  Edward R. Roesch

    Inventor： David J. Mitchell ,  Ramesh Subramanian ,  Cora Schillig ,  Anand A. Kulkarni ,  Vinay Jonnalagadda ,  Bulent Acar ,  Sankar Nellian ,  James P. Williams ,  Edward R. Roesch

    IPC: G06F15/00

    CPC classification number: F01D17/02 ,  F01D17/20

    Abstract: A telemetry system for use in a combustion turbine engine (10) having a compressor (12), a combustor and a turbine (16) and includes a sensor (118) in connection with a turbine blade (111) or vane (23). A transmitter assembly (117) includes a telemetry transmitter circuit/transceiver may be affixed on a turbine blade (111) or seal plate (115) proximate the turbine blade with a first connecting material (119) deposited on the turbine blade (111) for routing electronic data signals, indicative of a condition of the turbine blade (111), from the sensor (118) to the telemetry transmitter circuit/transceiver. An induction power system for powering the telemetry transmitter circuit/transceiver may include a rotating data antenna (116) affixed to the seal plate (115) with an electrical connection (122) between the telemetry transmitting circuit/transceiver for routing electronic data signals from the telemetry transmitter circuit/transceiver to the rotating data antenna (119).

    Abstract translation: 一种用于具有压缩机（12），燃烧器和涡轮机（16）的燃气涡轮发动机（10）中的遥测系统，并且包括与涡轮机叶片（111）或叶片（23）连接的传感器（118）。 发射器组件（117）包括遥测发射器电路/收发器可以用沉积在涡轮叶片（111）上的第一连接材料（119）固定在靠近涡轮机叶片的涡轮叶片（111）或密封板（115）上，用于 将表示涡轮叶片（111）的状况的电子数据信号从传感器（118）路由到遥测发射机电路/收发器。 用于为遥测发射器电路/收发器供电的感应电力系统可以包括在遥测发射电路/收发器之间的电连接（122）固定到密封板（115）的旋转数据天线（116），用于从 遥测发射机电路/收发器到旋转数据天线（119）。

    Tip Shrouded Turbine Blade
    2.
    发明申请
    Tip Shrouded Turbine Blade 有权
    尖头罩罩涡轮叶片

    公开(公告)号：US20100290897A1

    公开(公告)日：2010-11-18

    申请号：US12464492

    申请日：2009-05-12

    Applicant: Alexander R. Beeck ,  Sankar Nellian

    Inventor： Alexander R. Beeck ,  Sankar Nellian

    IPC: F01D11/08 ,  F01D5/22

    CPC classification number: F01D11/08 ,  F01D5/225

    Abstract: A turbine blade is provided comprising: an airfoil including upper and lower ends; a root coupled to the airfoil lower end; a shroud coupled to the airfoil upper end; and at least one sealing rail extending radially outwardly from an upper surface of the shroud and extending generally along a circumferential length of the shroud. The sealing rail may comprise a mid-section, opposing end sections and at least one intermediate section located between the mid-section and one of the opposing end sections. An axial thickness of the rail may vary.

    Abstract translation: 提供一种涡轮叶片，其包括：包括上端和下端的翼型件; 与翼型件下端相连的根部; 联接到翼型件上端的护罩; 以及至少一个密封轨道，其从护罩的上表面径向向外延伸并且大致沿着护罩的圆周长度延伸。 密封轨道可以包括中间部分，相对的端部部分和位于中间部分和相对的端部部分之一之间的至少一个中间部分。 轨道的轴向厚度可以变化。

    Tip shrouded turbine blade with sealing rail having non-uniform thickness
    3.
    发明授权
    Tip shrouded turbine blade with sealing rail having non-uniform thickness 有权
    带密封导轨的尖端罩式涡轮叶片具有不均匀的厚度

    公开(公告)号：US08192166B2

    公开(公告)日：2012-06-05

    申请号：US12464492

    申请日：2009-05-12

    Applicant: Alexander R. Beeck ,  Sankar Nellian

    Inventor： Alexander R. Beeck ,  Sankar Nellian

    IPC: F01D5/22

    CPC classification number: F01D11/08 ,  F01D5/225

    Abstract: A turbine blade is provided comprising: an airfoil including upper and lower ends; a root coupled to the airfoil lower end; a shroud coupled to the airfoil upper end; and at least one sealing rail extending radially outwardly from an upper surface of the shroud and extending generally along a circumferential length of the shroud. The sealing rail may comprise a mid-section, opposing end sections and at least one intermediate section located between the mid-section and one of the opposing end sections. An axial thickness of the rail may vary.

    Abstract translation: 提供一种涡轮叶片，其包括：包括上端和下端的翼型件; 与翼型件下端相连的根部; 联接到翼型件上端的护罩; 以及至少一个密封轨道，其从护罩的上表面径向向外延伸并且大致沿着护罩的圆周长度延伸。 密封轨道可以包括中间部分，相对的端部部分和位于中间部分和相对的端部部分之一之间的至少一个中间部分。 轨道的轴向厚度可以变化。

    Wireless telemetry system for a turbine engine
    4.
    发明授权
    Wireless telemetry system for a turbine engine 有权
    用于涡轮发动机的无线遥测系统

    公开(公告)号：US08527241B2

    公开(公告)日：2013-09-03

    申请号：US13018469

    申请日：2011-02-01

    Applicant: David J. Mitchell ,  Ramesh Subramanian ,  Cora Schillig ,  Anand A. Kulkarni ,  Vinay Jonnalagadda ,  Bulent Acar ,  Sankar Nellian ,  James P. Williams ,  Edward R. Roesch

    Inventor： David J. Mitchell ,  Ramesh Subramanian ,  Cora Schillig ,  Anand A. Kulkarni ,  Vinay Jonnalagadda ,  Bulent Acar ,  Sankar Nellian ,  James P. Williams ,  Edward R. Roesch

    IPC: G06F11/00 ,  G08C19/16 ,  G01K1/08

    CPC classification number: F01D17/02 ,  F01D17/20

    Abstract: A telemetry system for use in a combustion turbine engine (10) having a compressor (12), a combustor and a turbine (16) and includes a sensor (118) in connection with a turbine blade (111) or vane (23). A transmitter assembly (117) includes a telemetry transmitter circuit/transceiver may be affixed on a turbine blade (111) or seal plate (115) proximate the turbine blade with a first connecting material (119) deposited on the turbine blade (111) for routing electronic data signals, indicative of a condition of the turbine blade (111), from the sensor (118) to the telemetry transmitter circuit/transceiver. An induction power system for powering the telemetry transmitter circuit/transceiver may include a rotating data antenna (116) affixed to the seal plate (115) with an electrical connection (122) between the telemetry transmitting circuit/transceiver for routing electronic data signals from the telemetry transmitter circuit/transceiver to the rotating data antenna (119).

    Abstract translation: 一种用于具有压缩机（12），燃烧器和涡轮机（16）的燃气涡轮发动机（10）中的遥测系统，并且包括与涡轮机叶片（111）或叶片（23）连接的传感器（118）。 发射器组件（117）包括遥测发射器电路/收发器可以用沉积在涡轮叶片（111）上的第一连接材料（119）固定在靠近涡轮叶片的涡轮叶片（111）或密封板（115）上，用于 将表示涡轮叶片（111）的状况的电子数据信号从传感器（118）路由到遥测发射机电路/收发器。 用于为遥测发射器电路/收发器供电的感应电力系统可以包括在遥测发射电路/收发器之间的电连接（122）固定到密封板（115）的旋转数据天线（116），用于从 遥测发射机电路/收发器到旋转数据天线（119）。

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