VANE CARRIER FOR A COMPRESSOR OR A TURBINE SECTION OF AN AXIAL TURBO MACHINE
    1.
    发明申请
    VANE CARRIER FOR A COMPRESSOR OR A TURBINE SECTION OF AN AXIAL TURBO MACHINE 有权
    压缩机的VANE承运人或轴流式涡轮机的涡轮部分

    公开(公告)号:US20150292341A1

    公开(公告)日:2015-10-15

    申请号:US14680292

    申请日:2015-04-07

    Abstract: A vane carrier is provided for a compressor or a turbine section of an axial turbo machine, especially one of a gas turbine, steam turbine, compressor, expander, comprises least a first and second functional means. The first functional means is a cylinder made of a material with a coefficient of thermal expansion (CTE) below 1.3×10−5 [1/K]. The cylinder is provided for carrying a plurality of vanes on its inner side. The second functional means is a support structure made of a material different to and less expensive than the material of said first functional means. The support structure is provided for defining an axial and lateral position of the first functional means within an outer casing of the axial turbo machine.

    Abstract translation: 提供了一种用于轴流涡轮机的压缩机或涡轮机部分的叶片载体,特别是燃气轮机,蒸汽轮机,压缩机,膨胀机中的一个,包括至少一个第一和第二功能装置。 第一功能装置是由热膨胀系数(CTE)低于1.3×10-5 [1 / K]的材料制成的圆筒。 气缸被设置用于在其内侧上承载多个叶片。 第二功能装置是由与所述第一功能装置的材料不同并且便宜的材料制成的支撑结构。 提供支撑结构用于在轴向涡轮增压机的外壳内限定第一功能装置的轴向和横向位置。

    System for compensating rotor vibrations

    公开(公告)号:US10020764B2

    公开(公告)日:2018-07-10

    申请号:US14868546

    申请日:2015-09-29

    CPC classification number: H02P9/26 F16F15/00 F16F15/03 F16F15/10 G01H1/10

    Abstract: The present disclosure relates to a system to compensate for mechanical forces on a rotating rotor of an electric machine, to a method for compensating mechanical forces on a rotating rotor of an electric machine, and to a use of a corresponding system. Disclosed is a system for compensating torsions at a rotating rotor. The system includes at least one measuring device for measuring specific properties of the rotor, an analyzer unit for analyzing the measurement data of the measuring device, a compensation means for compensating the torsions at the rotor, the compensation means comprise a power supply unit generating a signal adapted in amplitude and frequency to the measured properties of the rotor, and to apply the generated signal to the rotor, and the power supply unit is a frequency converter.

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