Method of processing recurrent surge oscillograph data to enable more precise location of generator rotor inter-turn shorts and ground faults
    1.
    发明授权
    Method of processing recurrent surge oscillograph data to enable more precise location of generator rotor inter-turn shorts and ground faults 有权
    处理循环浪涌示波器数据的方法,以实现发电机转子匝间短路和接地故障的更精确定位

    公开(公告)号:US09383413B2

    公开(公告)日:2016-07-05

    申请号:US14077632

    申请日:2013-11-12

    IPC分类号: G01R31/34 G01R31/02

    摘要: A system and method for locating inter-turn short circuits or ground faults in a rotor winding of an electrical generator. The method analyzes data from a Recurrent Surge Oscillograph (RSO) test, identifies a spike or anomaly in a reflected RSO signal, determines an elapsed time between a transmitted signal and the anomaly in the reflected signal, calculates a distance along the winding conductor to the inter-turn short circuit or ground fault based on the elapsed time, and uses a geometric model of the winding conductor to identify a location of the fault based on the distance. The location of the inter-turn short circuit or ground fault specifies a coil number, a turn number within the coil and a position within the turn.

    摘要翻译: 一种用于定位发电机的转子绕组中的匝间短路或接地故障的系统和方法。 该方法分析来自经常浪涌示波器(RSO)测试的数据,识别反射RSO信号中的尖峰或异常,确定发射信号与反射信号中的异常之间的经过时间,计算沿绕组导体到 基于经过时间的匝间短路或接地故障,并且使用绕组导体的几何模型来基于距离来识别故障的位置。 匝间短路或接地故障的位置指定线圈数,线圈内的匝数和匝内的位置。

    Locking arrangement for radial entry turbine blades
    2.
    发明申请
    Locking arrangement for radial entry turbine blades 有权
    径向入口涡轮叶片的锁定装置

    公开(公告)号:US20060216152A1

    公开(公告)日:2006-09-28

    申请号:US11088639

    申请日:2005-03-24

    IPC分类号: F01D5/30

    摘要: A locking arrangement for a row of radial entry blades (62) of a turbo-machine. A closing blade (66) includes a root portion (74) having an axial attachment shape (78) for engagement with an axially oriented slot having an axial attachment shape (76) formed at the entering slot location (34) of the radial entry rotor disk (56). For applications utilizing blades with curved platform faces (112), a preceding blade (108) and a following blade (110) in the row are designed with one curved face for abutting adjacent radial entry blades and one flat face (120) for abutting the flat closing blade faces (116). The closing blade (84) may be designed with a root portion (88) having two legs (90,92) that are urged apart by a key (86) into tight contact with the adjacent blades. A closing blade (62) substantially identical to the radial entry blades may be affixed in the entering slot location with a connecting member (96) that has a radially inner portion (98) having an axial attachment shape and a radially outer portion (100) having a radial attachment shape. A flaw in a perimeter portion of a radial entry rotor disk (56) may be repaired without welding by removing the flaw along with adjoining material to form an axial attachment shape in the rotor disk, and then installing closing blade with a complementary axial attachment shape into the repair location.

    摘要翻译: 用于涡轮机的一排径向进入叶片(62)的锁定装置。 闭合叶片(66)包括具有轴向附接形状(78)的根部(74),用于与形成在径向进入转子的进入槽位置(34)处的轴向附接形状(76)的轴向定向的槽接合 盘(56)。 对于使用具有弯曲平台面(112)的刀片的应用,行中的前刀片(108)和后刀片(110)设计有一个弯曲面,用于邻接相邻的径向入口刀片和一个平面(120),用于邻接 平的闭合叶片面(116)。 封闭叶片(84)可以设计成具有两个腿部(90,92)的根部(88),所述两个腿部(90,92)被钥匙(86)推压而与相邻叶片紧密接触。 基本上与径向入口叶片相同的闭合叶片(62)可以在进入槽位置中与具有轴向附接形状的径向内部部分(98)和径向外部分(100)的连接构件(96)固定, 具有径向附着形状。 径向进入转子盘(56)的周边部分的缺陷可以通过与相邻材料一起移除缺陷而在不进行焊接的情况下被修复,以在转子盘中形成轴向附着形状,然后安装具有互补的轴向附着形状的封闭刀片 进入修理位置。

    Centerline suspension for turbine internal component
    3.
    发明授权
    Centerline suspension for turbine internal component 有权
    涡轮内部组件的中心悬挂

    公开(公告)号:US08430625B2

    公开(公告)日:2013-04-30

    申请号:US12018980

    申请日:2008-01-24

    IPC分类号: F01D25/26

    CPC分类号: F01D25/28 F05D2230/64

    摘要: A centerline suspension arrangement (42) for a turbine (40). A turbine inner casing (44) is supported within an outer casing (46) via a support member (60) that includes an inner portion (62) contacting the inner casing and an outer portion (66) extending into a slot (68) formed in the outer casing. The support member is slid into an axially oriented slot (64) formed in the inner casing and is body bound therein with respect to radial movements, with the support member and the inner casing slot including opposed vertical support surfaces (82, 90) and a pair of oppositely facing opposed horizontal support surfaces (80, 88 and 86, 92). Thus, dead weight and operating loads from the inner casing are reacted through the support member and into the outer casing without the necessity for any bolting or other fastener attachment in the design load path between the support member and the inner casing.

    摘要翻译: 一种用于涡轮机(40)的中心线悬挂装置(42)。 涡轮机内壳(44)经由支撑构件(60)支撑在外壳(46)内,支撑构件(60)包括接触内壳的内部部分(62)和延伸到形成的槽(68)的外部部分(66) 在外壳中。 支撑构件滑动到形成在内壳体中的轴向定向的狭槽(64)中,并且相对于径向运动被限制在其中,支撑构件和内壳狭槽包括相对的垂直支撑表面(82,90)和 一对相对的相对的水平支撑表面(80,88和86,92)。 因此,来自内壳体的自重和操作载荷通过支撑构件反应并进入外壳,而不需要在支撑构件和内壳之间的设计载荷路径中进行任何螺栓连接或其他紧固件附接。

    Locking arrangement for radial entry turbine blades
    4.
    发明授权
    Locking arrangement for radial entry turbine blades 有权
    径向入口涡轮叶片的锁定装置

    公开(公告)号:US07261518B2

    公开(公告)日:2007-08-28

    申请号:US11088639

    申请日:2005-03-24

    IPC分类号: B63H1/20

    摘要: A locking arrangement for a row of radial entry blades (62) of a turbo-machine. A closing blade (66) includes a root portion (74) having an axial attachment shape (78) for engagement with an axially oriented slot having an axial attachment shape (76) formed at the entering slot location (34) of the radial entry rotor disk (56). For applications utilizing blades with curved platform faces (112), a preceding blade (108) and a following blade (110) in the row are designed with one curved face for abutting adjacent radial entry blades and one flat face (120) for abutting the flat closing blade faces (116). The closing blade (84) may be designed with a root portion (88) having two legs (90,92) that are urged apart by a key (86) into tight contact with the adjacent blades.

    摘要翻译: 用于涡轮机的一排径向进入叶片(62)的锁定装置。 闭合叶片(66)包括具有轴向附接形状(78)的根部(74),用于与形成在径向进入转子的进入槽位置(34)处的轴向附接形状(76)的轴向定向的槽接合 盘(56)。 对于使用具有弯曲平台面(112)的刀片的应用,行中的前刀片(108)和后刀片(110)设计有一个弯曲面,用于邻接相邻的径向入口刀片和一个平面(120),用于邻接 平的闭合叶片面(116)。 封闭叶片(84)可以设计成具有两个腿部(90,92)的根部(88),所述两个腿部(90,92)被钥匙(86)推压而与相邻叶片紧密接触。