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    Method of producing a turbine component with multiple interconnected layers of cooling channels
    5.
    发明授权
    Method of producing a turbine component with multiple interconnected layers of cooling channels 有权
    制造具有多个相互连接的冷却通道层的涡轮机部件的方法

    公开(公告)号：US08042268B2

    公开(公告)日：2011-10-25

    申请号：US12052937

    申请日：2008-03-21

    申请人： Douglas J. Arrell ,  Allister W. James ,  Anand A. Kulkarni

    发明人： Douglas J. Arrell ,  Allister W. James ,  Anand A. Kulkarni

    IPC分类号： B23P15/04

    CPC分类号： B21D53/78 ,  B22D25/00 ,  Y10T29/4932 ,  Y10T29/49341 ,  Y10T29/49885 ,  Y10T29/4998 ,  Y10T29/49982

    摘要： A method for making a gas turbine component (100). A central core (20) is positioned to occupy a space that will define a central channel (42), and an outer channel core (30) is positioned spaced apart from the central core (20). A mold (35) is formed around the central core (20) and the outer channel core (30), so that an exterior wall (32) contacts the mold (35). A substrate material, such as a metal alloy (247) in liquid form, is added to the mold (35) to form an internal volume (41) of the component (100). The central core (20) and the outer channel core (30) are removed, and interconnect channels (44) are formed between the thus-formed central channel (42) and the inner portion (49) of the outer channel (62) thus far formed. A preform (55) is placed into the inner portion (49) and may have a desired outer surface (57) shape. An overlay material is applied to form an outer layer (60), thus defining the remainder of the outer channel (62), which is obtained upon removal of the preform (55).

    摘要翻译： 一种制造燃气轮机部件（100）的方法。 中心芯（20）定位成占据将限定中心通道（42）的空间，并且外通道芯（30）定位成与中心芯（20）间隔开。 围绕中心芯（20）和外通道芯（30）形成模具（35），使得外壁（32）接触模具（35）。 液体形式的金属合金（247）等基板材料被加入到模具（35）中以形成部件（100）的内部容积（41）。 去除中心芯（20）和外通道芯（30），并且互连通道（44）形成在如此形成的中心通道（42）和外通道（62）的内部部分（49）之间，因此 远远形成。 将预成型件（55）放置在内部部分（49）中并且可以具有期望的外表面（57）形状。 施加覆盖材料以形成外层（60），从而限定了在移除预成型件（55）时获得的外部通道（62）的剩余部分。

    METHOD OF MAKING RARE-EARTH STRENGTHENED COMPONENTS
    6.
    发明申请
    METHOD OF MAKING RARE-EARTH STRENGTHENED COMPONENTS 有权
    制备稀土强化组分的方法

    公开(公告)号：US20100043597A1

    公开(公告)日：2010-02-25

    申请号：US12194154

    申请日：2008-08-19

    申请人： Douglas J. Arrell ,  Allister W. James ,  Anand A. Kulkarni

    发明人： Douglas J. Arrell ,  Allister W. James ,  Anand A. Kulkarni

    IPC分类号： B22F9/06

    CPC分类号： C22C1/1078 ,  B22F2998/00 ,  B22F2998/10 ,  B22F2999/00 ,  C22C32/0026 ,  B22F5/04 ,  B22F5/009 ,  B22F9/082 ,  B22F9/04 ,  B22F1/0088 ,  B22F1/0085 ,  B22F2201/10 ,  B22F2201/20 ,  B22F2201/03

    摘要： A method of manufacturing a metallic component includes atomizing, in an inert atmosphere, a metallic liquid having at least one rare-earth element and at least one non rare-earth element to form a metallic powder. A series of heat treating steps are performed on the metallic powder. A first heat treating step is performed in an oxidizing atmosphere, and a second heat treating step is performed in an inert atmosphere. A third heat treating step is performed in a reducing atmosphere to form a metallic power having an increased proportion of rare-earth oxides compared to non rare-earth oxides. The metallic component is formed from the metallic powder having the increased proportion of rare-earth oxides compared to non rare-earth oxides.

    摘要翻译： 制造金属成分的方法包括在惰性气氛中使具有至少一种稀土元素和至少一种非稀土元素的金属液体雾化，形成金属粉末。 对金属粉末进行一系列热处理步骤。 在氧化气氛中进行第一热处理工序，在惰性气氛中进行第二热处理工序。 在还原性气氛中进行第3热处理工序，与非稀土类氧化物相比，形成稀土类氧化物比例增加的金属粉末。 与非稀土氧化物相比，金属组分由稀土氧化物比例增加的金属粉末形成。

    Method of Producing a Turbine Component with Multiple Interconnected Layers of Cooling Channels
    7.
    发明申请
    Method of Producing a Turbine Component with Multiple Interconnected Layers of Cooling Channels 有权
    制造具有冷却通道多个互连层的涡轮机部件的方法

    公开(公告)号：US20090235525A1

    公开(公告)日：2009-09-24

    申请号：US12052937

    申请日：2008-03-21

    申请人： Douglas J. Arrell ,  Allister W. James ,  Anand A. Kulkarni

    发明人： Douglas J. Arrell ,  Allister W. James ,  Anand A. Kulkarni

    IPC分类号： B23P15/02 ,  B21D53/78 ,  B22D25/06

    CPC分类号： B21D53/78 ,  B22D25/00 ,  Y10T29/4932 ,  Y10T29/49341 ,  Y10T29/49885 ,  Y10T29/4998 ,  Y10T29/49982

    摘要： A method for making a gas turbine component (100). A central core (20) is positioned to occupy a space that will define a central channel (42), and an outer channel core (30) is positioned spaced apart from the central core (20). A mold (35) is formed around the central core (20) and the outer channel core (30), so that an exterior wall (32) contacts the mold (35). A substrate material, such as a metal alloy (247) in liquid form, is added to the mold (35) to form an internal volume (41) of the component (100). The central core (20) and the outer channel core (30) are removed, and interconnect channels (44) are formed between the thus-formed central channel (42) and the inner portion (49) of the outer channel (62) thus far formed. A preform (55) is placed into the inner portion (49) and may have a desired outer surface (57) shape. An overlay material is applied to form an outer layer (60), thus defining the remainder of the outer channel (62), which is obtained upon removal of the preform (55).

    摘要翻译： 一种制造燃气轮机部件（100）的方法。 中心芯（20）定位成占据将限定中心通道（42）的空间，并且外通道芯（30）定位成与中心芯（20）间隔开。 围绕中心芯（20）和外通道芯（30）形成模具（35），使得外壁（32）接触模具（35）。 液体形式的金属合金（247）等基板材料被加入到模具（35）中以形成部件（100）的内部容积（41）。 去除中心芯（20）和外通道芯（30），并且互连通道（44）形成在如此形成的中心通道（42）和外通道（62）的内部部分（49）之间，因此 远远形成。 将预成型件（55）放置在内部部分（49）中并且可以具有期望的外表面（57）形状。 施加覆盖材料以形成外层（60），从而限定了在移除预成型件（55）时获得的外部通道（62）的剩余部分。

    Combustion Turbine Component Having Rare-Earth Elements and Associated Methods
    10.
    发明申请
    Combustion Turbine Component Having Rare-Earth Elements and Associated Methods 审中-公开
    具有稀土元素和相关方法的燃烧涡轮机组件

    公开(公告)号：US20100061875A1

    公开(公告)日：2010-03-11

    申请号：US12205956

    申请日：2008-09-08

    申请人： Anand A. Kulkarni ,  Allister W. James ,  Douglas J. Arrell

    发明人： Anand A. Kulkarni ,  Allister W. James ,  Douglas J. Arrell

    IPC分类号： B22F3/12

    CPC分类号： B22F5/009 ,  B22F2998/10 ,  B22F1/0096 ,  B22F3/12 ,  B22F3/24

    摘要： A method of making a combustion turbine component includes forming a nanosized powder including a plurality of metals and at least one rare-earth element and agglomerating the nanosized powder to form a microsized powder including a plurality of metals and at least one rare-earth element. The microsized powder is processed to form a cohesive metallic mass and a primary aging heat treating is performed on the cohesive metallic mass. A solution heat treating may be performed on the cohesive metallic mass prior to the primary aging heat treating. A secondary aging treating may be performed on the cohesive metallic mass after the primary aging treating.

    摘要翻译： 制造燃气轮机部件的方法包括形成包含多种金属和至少一种稀土元素的纳米尺寸粉末，并且使纳米尺寸粉末附聚以形成包含多种金属和至少一种稀土元素的微细粉末。 将微细粉末加工成粘结金属物质，并对粘性金属物质进行初期时效热处理。 在一次老化热处理之前，可以对内聚金属质量进行固溶热处理。 二次老化处理可以在一次老化处理后对粘性金属块进行。