ABRASIVE CLEANING OF INNER COOLED GENERATOR COILS
    1.
    发明申请
    ABRASIVE CLEANING OF INNER COOLED GENERATOR COILS 审中-公开
    内部冷却发电机线圈的磨损清洁

    公开(公告)号:US20150165495A1

    公开(公告)日:2015-06-18

    申请号:US14107138

    申请日:2013-12-16

    IPC分类号: B08B9/027

    CPC分类号: B08B9/027 H02K3/22 H02K15/00

    摘要: A method for an abrasive cleaning of inner-cooled generator coil is presented. A shear hardening medium with suspended abrasive particles is filled into cooling passages of the generator coil. Hydraulic pressure is applied to the shear hardening medium which locks the abrasive particles into a matrix position. A flow is imparted to the shear hardening medium with the cooling passage which applies a shearing force to the shear hardening medium. The locked abrasives and the shearing force abrade an inner wall of the cooling passage and remove deposits and products of corrosion from the inner wall of the cooling passage. After removing the deposits and products of corrosion, the hydraulic pressure is released and the shear hardening medium is flushed out of the cooling passages.

    摘要翻译: 介绍了内冷发电机线圈研磨清洗方法。 具有悬浮磨料颗粒的剪切硬化介质被填充到发电机线圈的冷却通道中。 将液压施加到剪切硬化介质上,该介质将磨料颗粒锁定在矩阵位置。 通过向剪切硬化介质施加剪切力的冷却通道向剪切硬化介质施加流动。 锁定的磨料和剪切力磨损冷却通道的内壁,并从冷却通道的内壁去除沉积物和腐蚀产物。 在清除沉积物和腐蚀产物后,释放液压并将剪切硬化介质冲出冷却通道。

    METHOD AND SYSTEM FOR ADJUSTING A TURBOMACHINE GLAND SEAL
    2.
    发明申请
    METHOD AND SYSTEM FOR ADJUSTING A TURBOMACHINE GLAND SEAL 有权
    用于调节涡轮喷雾密封的方法和系统

    公开(公告)号:US20100313435A1

    公开(公告)日:2010-12-16

    申请号:US12481736

    申请日:2009-06-10

    IPC分类号: G01B5/25

    摘要: A method of determining an alignment of a floating seal for a turbo machine, including establishing a reference surface on a rotor of the turbomachine that is essentially perpendicular to an instantaneous centerline of the rotor, establishing a control surface that radially aligns a floating seal member that surrounds the rotor, providing an inflatable member arranged between a stationary portion of the turbomachine and a surface of the floating seal, inflating the inflatable member such that the inflatable member urges the floating seal firmly against the control surface, measuring an axial distance between the floating seal and the reference surface at a plurality of locations, determining a parallelism between the facing surfaces of the floating seal and the rotor based upon the plurality of measured axial distances, comparing the determined parallelism with a predetermined threshold, and adjusting an orientation of the control surface based upon the comparison.

    摘要翻译: 一种确定用于涡轮机的浮动密封件的对准的方法,包括在所述涡轮机的转子上建立基本上垂直于所述转子的瞬时中心线的参考表面,建立使所述浮动密封件径向对准的控制表面, 围绕所述转子,提供布置在所述涡轮机的固定部分和所述浮动密封件的表面之间的可充气构件,使所述可膨胀构件膨胀,使得所述可膨胀构件将所述浮动密封件紧紧地推向所述控制表面,测量所述浮动密封件之间的轴向距离 在多个位置处密封和参考表面,基于多个测量的轴向距离确定浮动密封件和转子的相对表面之间的平行度,将所确定的平行度与预定阈值进行比较,以及调整控制的取向 基于比较的表面。

    Method and system for adjusting a turbomachine gland seal
    3.
    发明授权
    Method and system for adjusting a turbomachine gland seal 有权
    用于调整涡轮机密封的方法和系统

    公开(公告)号:US07861435B1

    公开(公告)日:2011-01-04

    申请号:US12481736

    申请日:2009-06-10

    IPC分类号: G01B5/25

    摘要: A method of determining an alignment of a floating seal for a turbo machine, including establishing a reference surface on a rotor of the turbomachine that is essentially perpendicular to an instantaneous centerline of the rotor, establishing a control surface that radially aligns a floating seal member that surrounds the rotor, providing an inflatable member arranged between a stationary portion of the turbomachine and a surface of the floating seal, inflating the inflatable member such that the inflatable member urges the floating seal firmly against the control surface, measuring an axial distance between the floating seal and the reference surface at a plurality of locations, determining a parallelism between the facing surfaces of the floating seal and the rotor based upon the plurality of measured axial distances, comparing the determined parallelism with a predetermined threshold, and adjusting an orientation of the control surface based upon the comparison.

    摘要翻译: 一种确定用于涡轮机的浮动密封件的对准的方法,包括在所述涡轮机的转子上建立基本上垂直于所述转子的瞬时中心线的参考表面,建立使所述浮动密封件径向对准的控制表面, 围绕所述转子,提供布置在所述涡轮机的固定部分和所述浮动密封件的表面之间的可充气构件,使所述可膨胀构件膨胀,使得所述可膨胀构件将所述浮动密封件紧紧地推向所述控制表面,测量所述浮动密封件之间的轴向距离 在多个位置处密封和参考表面,基于多个测量的轴向距离确定浮动密封件和转子的相对表面之间的平行度,将所确定的平行度与预定阈值进行比较,以及调整控制的取向 基于比较的表面。