System and method of dual laser beam welding of first and second filler metals
    2.
    发明授权
    System and method of dual laser beam welding of first and second filler metals 有权
    第一和第二填充金属的双激光束焊接系统和方法

    公开(公告)号:US08319148B2

    公开(公告)日:2012-11-27

    申请号:US12544494

    申请日:2009-08-20

    IPC分类号: B23K26/00

    摘要: A system and method for laser beam welding at least two adjacent superalloy components involves substantially simultaneous formation of a base weld with a first filler metal placed between the components and cap weld with second filler metal formed over the base weld. A shim is inserted between the components, which may optionally be formed with a groove along the joint surface. A filler wire is fed to a location over the given surface or within the optional groove. Two lasers or a laser and coupled beam splitter supply first and second laser beams that are applied at focal points separated by a predetermined distance (e.g., 0.05-1.5 cm). The first laser beam is used to form a base weld with the first filler metal between the components, and the second laser beam is used to form a cap weld with the second filler metal on top of the base weld.

    摘要翻译: 用于激光束焊接至少两个相邻的超合金部件的系统和方法包括基本上同时形成基部焊缝,其中第一填充金属放置在部件之间,并且帽焊与第二填充金属形成在基础焊缝上。 组件之间插入垫片,其可以可选地沿着接合表面形成有凹槽。 填充线被馈送到给定表面上或在可选凹槽内的位置。 两个激光器或激光和耦合分束器提供施加在被隔开预定距离(例如,0.05-1.5cm)的焦点处的第一和第二激光束。 第一激光束用于与部件之间的第一填充金属形成基底焊缝,并且第二激光束用于与基底焊缝顶部的第二填充金属形成帽焊缝。

    METHOD AND APPARATUS FOR WELDING AN ARTICLE
    3.
    发明申请
    METHOD AND APPARATUS FOR WELDING AN ARTICLE 审中-公开
    焊接方法和装置

    公开(公告)号:US20090026173A1

    公开(公告)日:2009-01-29

    申请号:US11828702

    申请日:2007-07-26

    IPC分类号: B23K9/16 B23K9/00

    摘要: Disclosed is a method for welding an article, the method including the steps of placing the article in an enclosure with walls that enclose the article on all sides, the enclosure having a heating device associated therewith, the heating device configured and sized to uniformly heat the article over at least a substantial entirety of the article, establishing a nonreactive atmosphere in the enclosure, operating the heating device to uniformly heat the article in the enclosure to a welding temperature over at least the substantial entirety of the article, and welding the article in the enclosure while maintaining the welding temperature over at least the substantial entirety of the article.

    摘要翻译: 公开了一种用于焊接物品的方法,所述方法包括以下步骤:将所述物品放置在具有围绕所述物品的所有侧面上的壁的外壳中,所述外壳具有与其相关联的加热装置,所述加热装置被配置并定尺寸成均匀加热 制品在至少大体上的整个物品上,在外壳中建立非反应性气氛,操作加热装置以使外壳中的物品均匀地加热至至少整个制品的焊接温度,并将物品焊接在 外壳,同时保持焊接温度至少在物品的整个整体上。

    NICKEL-BASED ALLOY AND TURBINE COMPONENT HAVING NICKEL-BASED ALLOY
    4.
    发明申请
    NICKEL-BASED ALLOY AND TURBINE COMPONENT HAVING NICKEL-BASED ALLOY 审中-公开
    基于镍的合金和具有镍基合金的涡轮机组件

    公开(公告)号:US20140205490A1

    公开(公告)日:2014-07-24

    申请号:US13562388

    申请日:2012-07-31

    IPC分类号: C22C19/05

    摘要: A nickel-based alloy and a turbine component including a nickel-based alloy are disclosed. The nickel-based alloy includes, by weight, between about 8% and about 11% cobalt, up to about 3% niobium, up to about 3% titanium, up to about 2.3% aluminum, up to about 3% tungsten, up to about 25% chromium, up to about 0.1% carbon, up to about 0.01% boron, and a balance nickel, or the nickel-based alloy includes, by weight, between about 1% and about 3% niobium, between about 1% and about 3% titanium, between about 2.1% and about 2.5% aluminum, up to about 3% tungsten, up to about 11% cobalt, up to about 25% chromium, up to about 0.1% carbon, up to about 0.01% boron, and a balance nickel. The turbine component includes the nickel-based alloy.

    摘要翻译: 公开了一种镍基合金和包括镍基合金的涡轮部件。 镍基合金包含约8%至约11%的钴,至多约3%的铌,至多约3%的钛,至多约2.3%的铝,至多约3%的钨,至多 约25%的铬,至多约0.1%的碳,至多约0.01%的硼和余量的镍,或镍基合金包括按重量计约1%至约3%的铌,约1%和 约3%的钛,约2.1%至约2.5%的铝,至多约3%的钨,至多约11%的钴,至多约25%的铬,至多约0.1%的碳,至多约0.01%的硼, 和镍的平衡。 涡轮机部件包括镍基合金。

    Apparatus and method for a turbine bucket tip cap
    5.
    发明授权
    Apparatus and method for a turbine bucket tip cap 有权
    一种涡轮机铲斗顶盖的装置和方法

    公开(公告)号:US08371817B2

    公开(公告)日:2013-02-12

    申请号:US12559656

    申请日:2009-09-15

    IPC分类号: B64C11/20 B64C11/26

    摘要: A turbine bucket that includes a pressure side, a suction side opposite the pressure side, and a rib extending between the pressure side and the suction side. A tip cap is attached to the pressure side and the suction side and covers the rib. The tip cap includes a precipitation hardened material and a passage aligned with the rib. A method for assembling a turbine bucket having a pressure side and a suction side and a rib extending between the pressure side and suction side. The method includes receiving a tip cap made from a precipitation hardened material and having a passage in the tip cap. The method further includes locating the rib visually through the passage and aligning the passage with the rib. The method also includes welding the tip cap to the turbine bucket and to the rib.

    摘要翻译: 一种涡轮机桶,包括压力侧,与压力侧相对的吸入侧,以及在压力侧和吸力侧之间延伸的肋。 顶盖附接到压力侧和吸力侧并覆盖肋。 顶盖包括沉淀硬化材料和与肋对准的通道。 一种用于组装具有压力侧和吸力侧的涡轮机的方法以及在压力侧和吸入侧之间延伸的肋。 该方法包括接收由沉淀硬化材料制成并在顶盖中具有通道的尖端盖。 该方法还包括通过通道目视定位肋并将通道与肋对准。 该方法还包括将顶盖焊接到涡轮机桶和肋上。

    SYSTEM AND METHOD OF DUAL LASER BEAM WELDING OF FIRST AND SECOND FILLER METALS
    6.
    发明申请
    SYSTEM AND METHOD OF DUAL LASER BEAM WELDING OF FIRST AND SECOND FILLER METALS 有权
    第一和第二填充金属的双激光束焊接系统和方法

    公开(公告)号:US20110042361A1

    公开(公告)日:2011-02-24

    申请号:US12544494

    申请日:2009-08-20

    IPC分类号: B23K26/20

    摘要: A system and method for laser beam welding at least two adjacent superalloy components involves substantially simultaneous formation of a base weld with a first filler metal placed between the components and cap weld with second filler metal formed over the base weld. A shim is inserted between the components, which may optionally be formed with a groove along the joint surface. A filler wire is fed to a location over the given surface or within the optional groove. Two lasers or a laser and coupled beam splitter supply first and second laser beams that are applied at focal points separated by a predetermined distance (e.g., 0.05-1.5 cm). The first laser beam is used to form a base weld with the first filler metal between the components, and the second laser beam is used to form a cap weld with the second filler metal on top of the base weld.

    摘要翻译: 用于激光束焊接至少两个相邻的超合金部件的系统和方法包括基本上同时形成基部焊缝,其中第一填充金属放置在部件之间,并且帽焊与第二填充金属形成在基础焊缝上。 组件之间插入垫片,其可以可选地沿着接合表面形成有凹槽。 填充线被馈送到给定表面上或在可选凹槽内的位置。 两个激光器或激光和耦合分束器提供施加在被隔开预定距离(例如,0.05-1.5cm)的焦点处的第一和第二激光束。 第一激光束用于与部件之间的第一填充金属形成基底焊缝,并且第二激光束用于与基底焊缝顶部的第二填充金属形成帽焊缝。

    APPARATUS AND METHOD FOR A TURBINE BUCKET TIP CAP
    7.
    发明申请
    APPARATUS AND METHOD FOR A TURBINE BUCKET TIP CAP 有权
    一种涡轮机提篮盖的装置和方法

    公开(公告)号:US20110064584A1

    公开(公告)日:2011-03-17

    申请号:US12559656

    申请日:2009-09-15

    IPC分类号: F01D5/28 F01D5/14 B23P15/04

    摘要: A turbine bucket that includes a pressure side, a suction side opposite the pressure side, and a rib extending between the pressure side and the suction side. A tip cap is attached to the pressure side and the suction side and covers the rib. The tip cap includes a precipitation hardened material and a passage aligned with the rib. A method for assembling a turbine bucket having a pressure side and a suction side and a rib extending between the pressure side and suction side. The method includes receiving a tip cap made from a precipitation hardened material and having a passage in the tip cap. The method further includes locating the rib visually through the passage and aligning the passage with the rib. The method also includes welding the tip cap to the turbine bucket and to the rib.

    摘要翻译: 一种涡轮机桶,包括压力侧,与压力侧相对的吸入侧,以及在压力侧和吸力侧之间延伸的肋。 顶盖附接到压力侧和吸力侧并覆盖肋。 顶盖包括沉淀硬化材料和与肋对准的通道。 一种用于组装具有压力侧和吸力侧的涡轮机的方法以及在压力侧和吸入侧之间延伸的肋。 该方法包括接收由沉淀硬化材料制成并在顶盖中具有通道的尖端盖。 该方法还包括通过通道目视定位肋并将通道与肋对准。 该方法还包括将顶盖焊接到涡轮机桶和肋上。

    SUPERALLOY COMPOSITION AND METHOD OF FORMING A TURBINE ENGINE COMPONENT
    8.
    发明申请
    SUPERALLOY COMPOSITION AND METHOD OF FORMING A TURBINE ENGINE COMPONENT 审中-公开
    超级合金组成和形成涡轮发动机部件的方法

    公开(公告)号:US20110062220A1

    公开(公告)日:2011-03-17

    申请号:US12559890

    申请日:2009-09-15

    IPC分类号: B23K31/02 C22C19/05

    摘要: A nickel-base composition is disclosed that includes: about 15 to about 20 wt % Co; about 10 to about 19 wt % Cr; about 2.5 to about 3.4 wt % Al; less than about 0.5 wt % Ta; less than about 1.0 wt % Mo; less than about 0.06 wt % Zr; less than about 0.04 wt % B; about 1.1 to about 1.5 wt % Nb; about 3.0 to about 3.9 wt % Ti; about 3 to about 5 wt. % W; about 0.03 to about 0.07 wt. % C; and balance Ni; wherein aluminum, titanium, niobium, and tantalum are present within the alloy in a combined amount of 9 to 14 atomic percent.

    摘要翻译: 公开了一种镍基组合物,其包括:约15至约20重量%的Co; 约10至约19重量%的Cr; 约2.5至约3.4重量%的Al; 小于约0.5重量%的Ta; 小于约1.0重量%的Mo; 小于约0.06重量%的Zr; 小于约0.04重量%的B; 约1.1至约1.5重量%的Nb; 约3.0至约3.9重量%的Ti; 约3至约5wt。 %W; 约0.03至约0.07重量% % C; 并平衡Ni; 其中铝,钛,铌和钽以9〜14原子%的总量存在于合金中。

    Weld Repair Method for a Turbine Bucket Tip
    9.
    发明申请
    Weld Repair Method for a Turbine Bucket Tip 审中-公开
    涡轮斗尖的焊接修复方法

    公开(公告)号:US20090014421A1

    公开(公告)日:2009-01-15

    申请号:US11775466

    申请日:2007-07-10

    IPC分类号: B23K9/167 B23K28/00

    摘要: A weld repair method uses a gas tungsten or plasma arc welding torch and matching filler. An amperage supplied to the torch and a travel speed of the torch are controlled to produce a weld bead having a mushroom shape. The weld bead is ground from all sides to remove at least one half of a thickness of the weld bead, and another weld bead is formed. The technique produces crack free welds with directionally solidified weld metal that is similar to that of the base material and hence has comparable mechanical properties.

    摘要翻译: 焊接修复方法采用瓦斯钨或等离子弧焊枪和匹配填料。 控制提供给割炬的电流和割炬的移动速度以产生具有蘑菇形状的焊道。 焊缝从所有侧面被研磨以去除焊缝的厚度的至少一半,并且形成另一个焊道。 该技术产生与基本材料类似的定向凝固焊接金属的无裂纹焊缝,因此具有可比较的机械性能。