SEAL ASSEMBLY AND METHOD FOR ASSEMBLING A TURBINE
    9.
    发明申请
    SEAL ASSEMBLY AND METHOD FOR ASSEMBLING A TURBINE 有权
    密封组件和组装涡轮机的方法

    公开(公告)号:US20130168926A1

    公开(公告)日:2013-07-04

    申请号:US13343296

    申请日:2012-01-04

    摘要: According to one aspect of the invention, a method for assembling a turbine includes placing a middle layer between a first and second outer member, wherein the middle layer includes a non-continuous layer of material and the first and second outer members each include a member of continuous material and welding a primary joint between the middle layer, first outer member and second outer member, the primary joint extending through the first outer member, the middle layer and at least a portion of the second outer member. The method also includes welding a secondary joint between the middle layer and first outer member, the secondary joint extending through the first outer member and at least a portion of the middle layer.

    摘要翻译: 根据本发明的一个方面,一种用于组装涡轮机的方法包括在第一和第二外部构件之间放置中间层,其中中间层包括非连续的材料层,并且第一和第二外部构件各自包括构件 连续材料并焊接在中间层,第一外部构件和第二外部构件之间的主接头,主接头延伸穿过第一外部构件,中间层和第二外部构件的至少一部分。 该方法还包括焊接中间层和第一外部构件之间的次级接头,辅助接头延伸穿过第一外部构件和中间层的至少一部分。

    Seal assembly and method for assembling a turbine
    10.
    发明授权
    Seal assembly and method for assembling a turbine 有权
    密封组件和组装涡轮机的方法

    公开(公告)号:US08919633B2

    公开(公告)日:2014-12-30

    申请号:US13343296

    申请日:2012-01-04

    IPC分类号: B23K31/02 B23K15/00 B23K26/00

    摘要: According to one aspect of the invention, a method for assembling a turbine includes placing a middle layer between a first and second outer member, wherein the middle layer includes a non-continuous layer of material and the first and second outer members each include a member of continuous material and welding a primary joint between the middle layer, first outer member and second outer member, the primary joint extending through the first outer member, the middle layer and at least a portion of the second outer member. The method also includes welding a secondary joint between the middle layer and first outer member, the secondary joint extending through the first outer member and at least a portion of the middle layer.

    摘要翻译: 根据本发明的一个方面,一种用于组装涡轮机的方法包括在第一和第二外部构件之间放置中间层,其中中间层包括非连续的材料层,并且第一和第二外部构件各自包括构件 连续材料并焊接在中间层,第一外部构件和第二外部构件之间的主接头,主接头延伸穿过第一外部构件,中间层和第二外部构件的至少一部分。 该方法还包括焊接中间层和第一外部构件之间的次级接头,辅助接头延伸穿过第一外部构件和中间层的至少一部分。