Turbine bucket airfoil profile
    4.
    发明授权

    公开(公告)号:US08734116B2

    公开(公告)日:2014-05-27

    申请号:US13304725

    申请日:2011-11-28

    IPC分类号: F01D9/04 F01D5/14

    CPC分类号: F01D5/142 F05D2250/74

    摘要: A turbine bucket is provided including a bucket airfoil having an airfoil shape, the bucket airfoil having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in Table 1 wherein the Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances in inches by multiplying the Cartesian coordinate values of X, Y and Z by a height of the airfoil in inches, and wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z, the airfoil profile sections at Z distances being joined smoothly with one another to form a complete airfoil shape.

    Systems, Methods, and Apparatus for Sealing a Bucket Dovetail in a Turbine
    5.
    发明申请
    Systems, Methods, and Apparatus for Sealing a Bucket Dovetail in a Turbine 有权
    用于在涡轮机中密封桶形蜗杆的系统,方法和装置

    公开(公告)号:US20130028708A1

    公开(公告)日:2013-01-31

    申请号:US13191214

    申请日:2011-07-26

    IPC分类号: F03D11/00 F16J15/06 F16J15/02

    CPC分类号: F01D11/006 F01D5/3015

    摘要: Certain embodiments of the invention may include systems methods, and apparatus for sealing a bucket dovetail in a turbine. According to an example embodiment of the invention, a method is provided for sealing a gap between a bucket dovetail and a rotor wheel slot. The method can include providing a bucket tab associated with a bucket dovetail, wherein the bucket tab is configured to accept a seal tab; configuring the bucket tab and the seal tab to engage at least one dimension upon insertion of the seal tab into the bucket tab; and sealing a gap between the bucket dovetail and a rotor wheel slot with the seal tab; wherein at least a portion of the seal tab changes as a function of temperature for further sealing gap between the bucket dovetail and the rotor wheel slot.

    摘要翻译: 本发明的某些实施例可以包括系统方法和用于在涡轮机中密封铲斗燕尾榫的装置。 根据本发明的示例性实施例,提供了一种用于密封桶形燕尾榫和转子轮槽之间的间隙的方法。 该方法可以包括提供与铲斗燕尾榫相关联的铲斗翼片,其中铲斗翼片构造成接受密封片; 在将密封片插入到铲斗翼片中时,构造铲斗翼片和密封翼片以接合至少一个尺寸; 并用所述密封片密封所述铲斗燕尾榫与转子轮槽之间的间隙; 其中所述密封片的至少一部分作为温度的函数而变化,以进一步密封所述铲斗燕尾榫与所述转子轮槽之间的间隙。

    Systems, methods, and apparatus for sealing a bucket dovetail in a turbine
    6.
    发明授权
    Systems, methods, and apparatus for sealing a bucket dovetail in a turbine 有权
    用于在涡轮机中密封铲斗燕尾榫的系统,方法和装置

    公开(公告)号:US08894378B2

    公开(公告)日:2014-11-25

    申请号:US13191214

    申请日:2011-07-26

    IPC分类号: F01D5/30 F01D11/00

    CPC分类号: F01D11/006 F01D5/3015

    摘要: Certain embodiments of the invention may include systems methods, and apparatus for sealing a bucket dovetail in a turbine. According to an example embodiment of the invention, a method is provided for sealing a gap between a bucket dovetail and a rotor wheel slot. The method can include providing a bucket tab associated with a bucket dovetail, wherein the bucket tab is configured to accept a seal tab; configuring the bucket tab and the seal tab to engage at least one dimension upon insertion of the seal tab into the bucket tab; and sealing a gap between the bucket dovetail and a rotor wheel slot with the seal tab; wherein at least a portion of the seal tab changes as a function of temperature for further sealing gap between the bucket dovetail and the rotor wheel slot.

    摘要翻译: 本发明的某些实施例可以包括系统方法和用于在涡轮机中密封铲斗燕尾榫的装置。 根据本发明的示例性实施例,提供了一种用于密封桶形燕尾榫和转子轮槽之间的间隙的方法。 该方法可以包括提供与铲斗燕尾榫相关联的铲斗翼片,其中铲斗翼片构造成接受密封片; 在将密封片插入到铲斗翼片中时,构造铲斗翼片和密封翼片以接合至少一个尺寸; 并用所述密封片密封所述铲斗燕尾榫与转子轮槽之间的间隙; 其中所述密封片的至少一部分作为温度的函数而变化,以进一步密封所述铲斗燕尾榫与所述转子轮槽之间的间隙。