Turbine wheel of automotive turbocharger and method for producing the same

    公开(公告)号:US09738954B2

    公开(公告)日:2017-08-22

    申请号:US14631107

    申请日:2015-02-25

    IPC分类号: B22D18/06 C22C19/05 F01D5/28

    CPC分类号: C22C19/056 B22D18/06 F01D5/28

    摘要: The present invention relates to a turbine wheel of an automotive turbocharger, including a Ni-based alloy having a composition which contains, in terms of mass %: C: 0.08 to 0.20%; Mn: 0.25% or less; Si: 0.01 to 0.50%; Cr: 12.0 to 14.0%; Mo: 3.80 to 5.20%; Nb+Ta: 1.80 to 2.80%; Ti: 0.50 to 1.00%; Al: 5.50 to 6.50%; B: 0.005 to 0.015%; Zr: 0.05 to 0.15%; and Fe: 0.01 to 2.5%, with the remainder being Ni and unavoidable impurities, in which the turbine wheel includes a wing part and a shaft part, and a size of γ′ phase in each site of from a tip of the wing part to the shaft part is structure-controlled so as to fall within a range of from 0.4 to 0.8 μm.

    TURBINE WHEEL OF AUTOMOTIVE TURBOCHARGER AND METHOD FOR PRODUCING THE SAME
    2.
    发明申请
    TURBINE WHEEL OF AUTOMOTIVE TURBOCHARGER AND METHOD FOR PRODUCING THE SAME 有权
    汽车涡轮增压器的涡轮及其制造方法

    公开(公告)号:US20150247221A1

    公开(公告)日:2015-09-03

    申请号:US14631107

    申请日:2015-02-25

    IPC分类号: C22C19/05 F01D5/28 B22D18/06

    CPC分类号: C22C19/056 B22D18/06 F01D5/28

    摘要: The present invention relates to a turbine wheel of an automotive turbocharger, including a Ni-based alloy having a composition which contains, in terms of mass %: C: 0.08 to 0.20%; Mn: 0.25% or less; Si: 0.01 to 0.50%; Cr: 12.0 to 14.0%; Mo: 3.80 to 5.20%; Nb+Ta: 1.80 to 2.80%; Ti: 0.50 to 1.00%; Al: 5.50 to 6.50%; B: 0.005 to 0.015%; Zr: 0.05 to 0.15%; and Fe: 0.01 to 2.5%, with the remainder being Ni and unavoidable impurities, in which the turbine wheel includes a wing part and a shaft part, and a size of γ′ phase in each site of from a tip of the wing part to the shaft part is structure-controlled so as to fall within a range of from 0.4 to 0.8 μm.

    摘要翻译: 本发明涉及一种汽车涡轮增压器的涡轮机叶轮,其包括Ni基合金,其组成按质量%计含有:C:0.08〜0.20%; Mn:0.25%以下; Si:0.01〜0.50% Cr:12.0〜14.0% Mo:3.80〜5.20% Nb + Ta:1.80〜2.80% Ti:0.50〜1.00% 铝:5.50〜6.50% B:0.005〜0.015% Zr:0.05〜0.15% Fe:0.01〜2.5%,其余为Ni和不可避免的杂质,其中涡轮机叶轮包括翼部和轴部,以及从翼部的末端到各部位的γ'相的大小 该轴部的结构受控为在0.4〜0.8μm的范围内。

    TI-AL-BASED HEAT-RESISTANT MEMBER
    3.
    发明申请
    TI-AL-BASED HEAT-RESISTANT MEMBER 有权
    基于TI-AL的耐热构件

    公开(公告)号:US20150275673A1

    公开(公告)日:2015-10-01

    申请号:US14665470

    申请日:2015-03-23

    摘要: The present invention relates to a Ti—Al-based heat-resistant member including a Ti—Al-based alloy which includes: 28.0 mass % to 35.0 mass % of Al; 1.0 mass % to 15.0 mass % of at least one selected from the group consisting of Nb, Mo, W and Ta; 0.1 mass % to 5.0 mass % of at least one selected from the group consisting of Cr, Mn and V; and 0.1 mass % to 1.0 mass % of Si, with the balance being Ti and unavoidable impurities, in which a whole or a part of a surface of the Ti—Al-based heat-resistant member includes a hardened layer as a surface layer, the hardened layer having a higher hardness than an inside of the Ti—Al-based heat-resistant member, and the Ti—Al-based heat-resistant member has a hardness ratio (a hardness of the surface layer/a hardness of the inside) of 1.4 to 2.5.

    摘要翻译: 本发明涉及一种包含Ti-Al系合金的Ti-Al类耐热构件,其包括:Al:28.0质量%至35.0质量% 1.0质量%至15.0质量%的选自Nb,Mo,W和Ta中的至少一种; 0.1质量%至5.0质量%的选自Cr,Mn和V中的至少一种; 0.1质量%〜1.0质量%的Si,余量为Ti和不可避免的杂质,其中Ti-Al系耐热构件的表面的全部或一部分包括硬化层作为表面层, 该硬化层的硬度比Ti-Al系耐热构件的内部硬度高,Ti-Al系耐热构件的硬度比(表面层的硬度/内部的硬度 )为1.4〜2.5。