Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE BLADE
    1.
    发明申请
    Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE BLADE 审中-公开
    镍基单晶超级合金和涡轮叶片

    公开(公告)号:US20120070303A1

    公开(公告)日:2012-03-22

    申请号:US13375987

    申请日:2010-08-09

    IPC分类号: F01D5/14 C22C19/05

    摘要: The present invention provides a Ni-based single crystal superalloy which has the following composition by weight: 0.1 wt % or more and 9.9 wt % or less of Co, 5.1 wt % or more and 10.0 wt % or less of Cr, 1.0 wt % or more and 4.0 wt % or less of Mo, 8.1 wt % or more and 11.0 wt % or less of W, 4.0 wt % or more and 9.0 wt % or less of Ta, 5.2 wt % or more and 7.0 wt % or less of Al, 0.1 wt % or more and 2.0 wt % or less of Ti, 0.05 wt % or more and 0.3 wt % or less of Hf, 1.0 wt % or less of Nb and less than 3.0 wt % of Re with the remainder including Ni and unavoidable impurities. This Ni-based single crystal superalloy has a low Re content and also has excellent high-temperature strength, mainly creep strength.

    摘要翻译: 本发明提供一种Ni基单晶超耐热合金,其具有以下重量组成:0.1重量%以上且9.9重量%以下的Co,5.1重量%以上10.0重量%以下的Cr,1.0重量% 以上,4.0重量%以下,W:8.1重量%以上,11.0重量%以下,W:4.0重量%以上9.0重量%以下,Ta:5.2重量%以上7.0重量%以下 的Al,0.1重量%以上且2.0重量%以下的Ti,0.05重量%以上且0.3重量%以下的Hf,1.0重量%以下的Nb和小于3.0重量%的Re,余量包括 Ni和不可避免的杂质。 这种Ni基单晶超合金具有低的Re含量,并且具有优异的高温强度,主要是蠕变强度。

    Turbine blade capable of inhibiting reaction
    2.
    发明申请
    Turbine blade capable of inhibiting reaction 有权
    能够抑制反应的涡轮叶片

    公开(公告)号:US20070026256A1

    公开(公告)日:2007-02-01

    申请号:US10558648

    申请日:2004-02-25

    IPC分类号: B32B15/00 B32B15/20 B32B15/01

    摘要: A reaction control turbine blade is formed by applying a reaction control material to the surface of an Ni-base superalloy before applying aluminum diffusion coating to the Ni-base superalloy. The reaction control material is Co, Cr or Ru, or an alloy of which main component is selected from a group consisting of Co, Cr, Ru. Thereby, it is possible to enhance the oxidation resistance of the Ni-base superalloy, and to control formation of a secondary reaction zone.

    摘要翻译: 在向Ni基超级合金施加铝扩散涂层之前,通过将反应控制材料施加到Ni基超级合金的表面上来形成反应控制涡轮叶片。 反应控制材料是Co,Cr或Ru,或者主要成分选自Co,Cr,Ru的合金。 由此,可以提高Ni基超合金的抗氧化性,并且可以控制二次反应区的形成。

    Reaction control turbine blade
    5.
    发明授权
    Reaction control turbine blade 有权
    反应控制涡轮叶片

    公开(公告)号:US07514157B2

    公开(公告)日:2009-04-07

    申请号:US10558648

    申请日:2004-02-25

    摘要: A reaction control turbine blade is formed by applying a reaction control material to the surface of an Ni-base superalloy before applying aluminum diffusion coating to the Ni-base superalloy. The reaction control material is Co, Cr or Ru, or an alloy of which main component is selected from a group consisting of Co, Cr, Ru. Thereby, it is possible to enhance the oxidation resistance of the Ni-base superalloy, and to control formation of a secondary reaction zone.

    摘要翻译: 在向Ni基超级合金施加铝扩散涂层之前,通过将反应控制材料施加到Ni基超级合金的表面上来形成反应控制涡轮叶片。 反应控制材料是Co,Cr或Ru,或者主要成分选自Co,Cr,Ru的合金。 由此,可以提高Ni基超合金的抗氧化性,并且可以控制二次反应区的形成。

    Ni-based single crystal superalloy and turbine blade incorporating the same
    6.
    发明授权
    Ni-based single crystal superalloy and turbine blade incorporating the same 有权
    镍基单晶超合金和含有其的涡轮叶片

    公开(公告)号:US08877122B2

    公开(公告)日:2014-11-04

    申请号:US13264220

    申请日:2010-04-16

    IPC分类号: C22C19/05

    摘要: A Ni-based single crystal superalloy which has the following composition: Co: 0.0 wt % or more to 15.0 wt % or less, Cr: 4.1 to 8.0 wt %, Mo: 2.1 to 4.5 wt %, W: 0.0 to 3.9 wt %, Ta: 4.0 to 10.0 wt %, Al: 4.5 to 6.5 wt %, Ti: 0.0 to 1.0 wt %, Hf: 0.00 to 0.5 wt %, Nb: 0.0 to 3.0 wt %, Re: 8.1 to 9.9 wt % and Ru: 0.5 to 6.5 wt % with the remainder including Ni and unavoidable impurities. As a result, the Ni-based single crystal superalloy which includes more than 8 wt % of Re in the composition ratio and has excellent specific creep strength and the turbine blade incorporating the Ni-based single crystal superalloy may be made.

    摘要翻译: 具有以下组成的Ni基单晶超合金:Co:0.0wt%以上至15.0wt%以下,Cr:4.1〜8.0wt%,Mo:2.1〜4.5wt%,W:0.0〜3.9wt% ,Ta:4.0〜10.0wt%,Al:4.5〜6.5wt%,Ti:0.0〜1.0wt%,Hf:0.00〜0.5wt%,Nb:0.0〜3.0wt%,Re:8.1〜9.9wt% :0.5〜6.5重量%,余量包括Ni和不可避免的杂质。 结果,可以制备包含组合比大于8重量%的Re且具有优异的抗蠕变强度的Ni基单晶超合金,以及并入Ni基单晶超耐热合金的涡轮叶片。

    Method for reaction control coating
    7.
    发明授权
    Method for reaction control coating 有权
    反应控制涂层方法

    公开(公告)号:US07442417B2

    公开(公告)日:2008-10-28

    申请号:US10558685

    申请日:2004-02-25

    IPC分类号: C23C16/06 C23C16/12

    摘要: A method for reaction control coating includes: (a) a step of applying a reaction control material to a surface of an Ni-base superalloy before applying aluminum diffusion coating to the Ni-base superalloy, wherein the reaction control material is Co, Cr or Ru, or an alloy of which main component is selected from the group consisting of Co, Cr, and Ru; and (b) a step of applying the aluminum diffusion coating to the Ni-base superalloy.

    摘要翻译: 反应控制涂料的方法包括:(a)在Ni基超合金施加铝扩散涂层之前,向Ni基超合金的表面施加反应控制材料的步骤,其中反应控制材料为Co,Cr或 Ru或其主要组分选自Co,Cr和Ru的合金; 和(b)将铝扩散涂层施加到Ni基超级合金的步骤。

    Method of build up welding to thin-walled portion
    8.
    发明授权
    Method of build up welding to thin-walled portion 有权
    堆焊到薄壁部分的方法

    公开(公告)号:US06991150B2

    公开(公告)日:2006-01-31

    申请号:US10651203

    申请日:2003-08-29

    IPC分类号: B23K31/02 B23P6/04

    摘要: A recess formed in close contact with a thin-walled portion 3a of a workpiece to store molten metal at a surfaced portion, a jig 4 manufactured from a material with a higher heat-resisting temperature than that of the molten metal and a satisfactorily large heat capacity, a step (A) wherein the jig is installed on the workpiece, a preheating step (B) in which the workpiece and the jig are preheated to a predetermined temperature under the condition that jig 4 is installed, a build up welding step (C) for build up welding the thin-walled portion of the workpiece and forming weld beads at surfaced portion, and a jig-removing step (D) for removing the jig after weld beads solidify completely.

    摘要翻译: 形成为与工件的薄壁部分3a紧密接触以形成表面部分处的熔融金属的凹部,由耐熔温度高于熔融金属的材料制成的夹具4,并且具有令人满意的大 热容量,其中夹具安装在工件上的步骤(A),在安装夹具4的条件下将工件和夹具预热到预定温度的预热步骤(B),建立焊接步骤 (C),用于堆焊工件的薄壁部分并在表面部分形成焊缝;以及用于在焊珠完全固化之后移除夹具的夹具去除步骤(D)。

    Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE BLADE INCORPORATING THE SAME
    10.
    发明申请
    Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE BLADE INCORPORATING THE SAME 有权
    镍基单晶超级合金和涡轮叶片并入其中

    公开(公告)号:US20120034098A1

    公开(公告)日:2012-02-09

    申请号:US13264220

    申请日:2010-04-16

    IPC分类号: F01D5/14 C22C30/00 C22C19/05

    摘要: A Ni-based single crystal superalloy which has the following composition: Co: 0.0 wt % or more to 15.0 wt % or less, Cr: 4.1 to 8.0 wt %, Mo: 2.1 to 4.5 wt %, W: 0.0 to 3.9 wt %, Ta: 4.0 to 10.0 wt %, Al: 4.5 to 6.5 wt %, Ti: 0.0 to 1.0 wt %, Hf: 0.00 to 0.5 wt %, Nb: 0.0 to 3.0 wt %, Re: 8.1 to 9.9 wt % and Ru: 0.5 to 6.5 wt % with the remainder including Ni and unavoidable impurities. As a result, the Ni-based single crystal superalloy which includes more than 8 wt % of Re in the composition ratio and has excellent specific creep strength and the turbine blade incorporating the Ni-based single crystal superalloy may be made.

    摘要翻译: 具有以下组成的Ni基单晶超合金:Co:0.0wt%以上至15.0wt%以下,Cr:4.1〜8.0wt%,Mo:2.1〜4.5wt%,W:0.0〜3.9wt% ,Ta:4.0〜10.0重量%,Al:4.5〜6.5重量%,Ti:0.0〜1.0重量%,Hf:0.00〜0.5重量%,Nb:0.0〜3.0重量%,Re:8.1〜9.9重量% :0.5〜6.5重量%,余量包括Ni和不可避免的杂质。 结果,可以制备包含组合比大于8重量%的Re且具有优异的抗蠕变强度的Ni基单晶超合金,以及并入Ni基单晶超耐热合金的涡轮叶片。