STEAM TURBINE AND METHODS OF ASSEMBLING THE SAME
    1.
    发明申请
    STEAM TURBINE AND METHODS OF ASSEMBLING THE SAME 有权
    蒸汽涡轮机及其组装方法

    公开(公告)号:US20150184529A1

    公开(公告)日:2015-07-02

    申请号:US14146292

    申请日:2014-01-02

    Abstract: A steam turbine is provided. The steam turbine includes a housing and a steam inlet configured to discharge a primary steam flow within the housing. A stator is coupled to the housing and a rotor is coupled to the housing and located within the stator. The rotor and the stator are configured to define a primary flow path there between and in flow communication with the primary steam flow. The steam turbine includes a seal assembly coupled to the housing. The seal assembly includes a packing head and a plurality of seals. The packing head is configured to define a cooling flow path in flow communication with the rotor and configured to discharge a cooling steam flow toward the rotor. An anti-swirl device is coupled to the seal assembly and located between the rotor and the packing head.

    Abstract translation: 提供蒸汽轮机。 蒸汽轮机包括壳体和构造成排出壳体内的主蒸汽流的蒸汽入口。 定子联接到壳体并且转子联接到壳体并且定位在定子内。 转子和定子构造成在其间限定主流动路径,并与主蒸汽流动流动连通。 蒸汽轮机包括联接到壳体的密封组件。 密封组件包括密封头和多个密封件。 包装头构造成限定与转子流动连通的冷却流动路径,并且构造成朝向转子排放冷却蒸汽流。 防旋转装置联接到密封组件并且位于转子和包装头之间。

    ROTOR COOLING
    4.
    发明申请
    ROTOR COOLING 有权
    转子冷却

    公开(公告)号:US20150132107A1

    公开(公告)日:2015-05-14

    申请号:US14079610

    申请日:2013-11-13

    CPC classification number: F01D5/085 F01D11/02 F01D25/12 Y02T50/676

    Abstract: Embodiments of the invention relate generally to rotor cooling and, more particularly, to a stator member having at least one passage for the delivery of cooling steam to a bucket root. In one embodiment, the invention provides a turbine comprising: a rotor including a first bucket root; and a stator member having: a rotor bore within which at least a portion of the rotor is disposed; a facing end adjacent to the first bucket root of the rotor; a plurality of seals within the rotor bore for sealing against the rotor, the plurality of seals including a first seal nearest the facing end and a second seal adjacent to the first seal; and a plurality of passages, each extending from a surface of the rotor bore at a point between the first seal and the second seal and extending through the facing end.

    Abstract translation: 本发明的实施方案大体上涉及转子冷却,更具体地,涉及具有用于将冷却蒸汽输送到铲斗根部的至少一个通道的定子构件。 在一个实施例中,本发明提供一种涡轮机,包括:转子,其包括第一铲斗根部; 以及定子构件,其具有:转子孔,所述转子的至少一部分设置在所述转子孔内; 靠近转子的第一铲斗根部的面对端; 所述转子孔内的多个密封件用于密封所述转子,所述多个密封件包括最靠近所述端部的第一密封件和邻近所述第一密封件的第二密封件; 以及多个通道,每个通道在第一密封件和第二密封件之间的点处从转子孔的表面延伸并延伸穿过相对端。

    LOCKING BLADE FOR A ROTOR
    5.
    发明申请
    LOCKING BLADE FOR A ROTOR 有权
    用于转子的锁紧刀片

    公开(公告)号:US20140127026A1

    公开(公告)日:2014-05-08

    申请号:US13668996

    申请日:2012-11-05

    CPC classification number: F01D5/3038 F01D5/225 F01D5/32

    Abstract: A locking blade for a rotor can include an airfoil portion with a root from which a tongue extends. Opposed bucket segments can engage the tongue and can be retained in a longitudinal direction of the blade by a fastener, such as a pin, that can extend through holes in the segments and tongue. Tines parallel to and on opposite sides of the tongue can extend from the root and include holes through which the fastener can extend, the bucket segments extending between respective tines and the tongue. The structure can eliminate an assembly gate in a rotor.

    Abstract translation: 用于转子的锁定刀片可以包括具有舌部的根部的翼型部分。 相对的铲斗段可以接合舌部并且可以通过诸如销的紧固件保持在刀片的纵向方向上,该紧固件可以延伸穿过节段和舌头中的孔。 舌头平行于舌片和相对侧上的齿可以从根部延伸,并且包括紧固件可以延伸穿过的孔,铲斗段在相应的尖齿和舌部之间延伸。 该结构可以消除转子中的组装门。

    Turbomachine bucket with radial support, shim and related turbomachine rotor

    公开(公告)号:US10400614B2

    公开(公告)日:2019-09-03

    申请号:US15355818

    申请日:2016-11-18

    Abstract: Various aspects include a turbomachine bucket, corresponding shim and related turbine rotor. In some cases, a steam turbine bucket includes: a blade having a first end, and a second end opposite the first end; a tip at the first end of the blade; and a base at the second end, the base including a dovetail for complementing a corresponding dovetail slot in a steam turbine rotor, the dovetail having: a body; a plurality of projections extending from the body in opposing directions for complementing a plurality of recesses in the corresponding dovetail slot; and a shim locking slot extending through the body along the opposing directions, the shim locking slot being open at a bottom surface of the body and sized to engage a shim.

    Rotor cooling
    9.
    发明授权
    Rotor cooling 有权
    转子冷却

    公开(公告)号:US09388698B2

    公开(公告)日:2016-07-12

    申请号:US14079610

    申请日:2013-11-13

    CPC classification number: F01D5/085 F01D11/02 F01D25/12 Y02T50/676

    Abstract: Embodiments of the invention relate generally to rotor cooling and, more particularly, to a stator member having at least one passage for the delivery of cooling steam to a bucket root. In one embodiment, the invention provides a turbine comprising: a rotor including a first bucket root; and a stator member having: a rotor bore within which at least a portion of the rotor is disposed; a facing end adjacent to the first bucket root of the rotor; a plurality of seals within the rotor bore for sealing against the rotor, the plurality of seals including a first seal nearest the facing end and a second seal adjacent to the first seal; and a plurality of passages, each extending from a surface of the rotor bore at a point between the first seal and the second seal and extending through the facing end.

    Abstract translation: 本发明的实施方案大体上涉及转子冷却,更具体地,涉及具有用于将冷却蒸汽输送到铲斗根部的至少一个通道的定子构件。 在一个实施例中,本发明提供一种涡轮机,包括:转子,其包括第一铲斗根部; 以及定子构件,其具有:转子孔,所述转子的至少一部分设置在所述转子孔内; 靠近转子的第一铲斗根部的面对端; 所述转子孔内的多个密封件用于密封所述转子,所述多个密封件包括最靠近所述端部的第一密封件和邻近所述第一密封件的第二密封件; 以及多个通道,每个通道在第一密封件和第二密封件之间的点处从转子孔的表面延伸并延伸穿过相对端。

    SHROUDED TURBINE BLISK AND METHOD OF MANUFACTURING SAME
    10.
    发明申请
    SHROUDED TURBINE BLISK AND METHOD OF MANUFACTURING SAME 审中-公开
    SHROUDED涡轮机气泡及其制造方法

    公开(公告)号:US20150098802A1

    公开(公告)日:2015-04-09

    申请号:US14048431

    申请日:2013-10-08

    Abstract: Shrouded turbine blisks and methods of manufacturing same are provided. A shrouded turbine blisk includes a central disk portion including an axis of rotation, an inner rim, a plurality of airfoils that extends radially outwardly from the inner rim; and a shroud integrally coupled to each of the plurality of airfoils. The shroud includes a plurality of circumferentially-arranged arcuate shroud segments defined at least in part by gaps positioned between adjacent shroud segments. The central disk portion, the inner rim, the plurality of airfoils, and the shroud are defined from a single billet of blisk material.

    Abstract translation: 提供有罩涡轮叶片及其制造方法。 带盖的涡轮叶片包括包括旋转轴线的中心盘部分,内缘,从内缘径向向外延伸的多个翼型件; 以及与所述多个翼型件中的每一个一体地联接的护罩。 护罩包括多个周向布置的弓形护罩段,其至少部分地由相邻护罩段之间的间隙限定。 中心圆盘部分,内缘,多个翼型件和护罩由单一的圆盘坯料限定。

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