Nanocrystal titanium alloy and production method for same
    1.
    发明授权
    Nanocrystal titanium alloy and production method for same 有权
    纳米晶钛合金及其制作方法相同

    公开(公告)号:US09260773B2

    公开(公告)日:2016-02-16

    申请号:US13496750

    申请日:2010-09-22

    摘要: A titanium alloy has high strength and superior workability and is preferably used for various structural materials for automobiles, etc. The titanium alloy is obtained by the following production method. An alloy having a structure of α′ martensite phase is hot worked at conditions at which dynamic recrystallization occurs. The working is performed at a heating rate of 50 to 800° C./second at a strain rate of 0.01 to 10/second when the temperature is 700 to 800° C. or at a strain rate of 0.1 to 10/second when the temperature is more than 800° C. and less than 1000° C. so as to provide a strain of not less than 0.5. Thus, equiaxed crystals with an average grain size of less than 1000 nm are obtained.

    摘要翻译: 钛合金的强度高,加工性优异,优选用于汽车等的各种结构材料。钛合金通过以下的制造方法得到。 具有α'马氏体相结构的合金在发生动态再结晶的条件下热加工。 当温度为700至800℃时,以0.1至10 /秒的应变速率,以0.1至10 /秒的应变速率,以50至800℃/秒的加热速率进行加工,应变速率为0.01至10 /秒 温度超过800℃且小于1000℃,以提供不小于0.5的应变。 因此,得到平均粒径小于1000nm的等轴晶体。

    NANOCRYSTAL-CONTAINING TITANIUM ALLOY AND PRODUCTION METHOD THEREFOR
    2.
    发明申请
    NANOCRYSTAL-CONTAINING TITANIUM ALLOY AND PRODUCTION METHOD THEREFOR 有权
    含纳米钛合金及其生产方法

    公开(公告)号:US20130284325A1

    公开(公告)日:2013-10-31

    申请号:US13988123

    申请日:2011-11-22

    IPC分类号: C22F1/18 C22C14/00

    CPC分类号: C22F1/183 C22C14/00 C22F1/00

    摘要: An alloy having an α′ martensite which is a processing starting structure is hot worked. The alloy is heated at a temperature increase rate of 50 to 800° C./sec, and strain is given at not less than 0.5 by a processing strain rate of from 0.01 to 10/sec in a case of a temperature range of 700 to 800° C., or by a processing strain rate of 0.1 to 10/sec in a case of a temperature range of 800° C. to 1000° C. By generating equiaxial crystals having average crystal particle diameters of less than 1000 nm through the above processes, a titanium alloy having high strength and high fatigue resistant property can be obtained, in which hardness is less than 400 HV, tensile strength is not less than 1200 MPa, and static strength and dynamic strength are superior.

    摘要翻译: 具有作为加工起始结构的α'马氏体的合金被热加工。 以50〜800℃/秒的升温速度加热合金,在700〜700℃的温度范围内,通过0.01〜10 /秒的加工变形速度,使应变为0.5以上 800℃,或者在800〜1000℃的温度范围内,通过加工应变速度为0.1〜10 /秒。通过生成平均结晶粒径小于1000nm的等轴晶体,通过 可以得到硬度小于400HV,拉伸强度不小于1200MPa,静态强度和动态强度优异的高强度,高耐疲劳性的钛合金。

    NANOCRYSTAL TITANIUM ALLOY AND PRODUCTION METHOD FOR SAME
    4.
    发明申请
    NANOCRYSTAL TITANIUM ALLOY AND PRODUCTION METHOD FOR SAME 有权
    纳米钛合金及其制造方法

    公开(公告)号:US20120168042A1

    公开(公告)日:2012-07-05

    申请号:US13496750

    申请日:2010-09-22

    IPC分类号: C22F1/16 C22C14/00

    摘要: A titanium alloy has high strength and superior workability and is preferably used for various structural materials for automobiles, etc. The titanium alloy is obtained by the following production method. An alloy having a structure of α′ martensite phase is hot worked at conditions at which dynamic recrystallization occurs. The working is performed at a heating rate of 50 to 800° C./second at a strain rate of 0.01 to 10/second when the temperature is 700 to 800° C. or at a strain rate of 0.1 to 10/second when the temperature is more than 800° C. and less than 1000° C. so as to provide a strain of not less than 0.5. Thus, equiaxed crystals with an average grain size of less than 1000 nm are obtained.

    摘要翻译: 钛合金的强度高,加工性优异,优选用于汽车等的各种结构材料。钛合金通过以下的制造方法得到。 具有α'马氏体相结构的合金在发生动态再结晶的条件下热加工。 当温度为700至800℃时,以0.1至10 /秒的应变速率,以0.1至10 /秒的应变速率,以50至800℃/秒的加热速率进行加工,应变速率为0.01至10 /秒 温度超过800℃且小于1000℃,以提供不小于0.5的应变。 因此,得到平均粒径小于1000nm的等轴晶体。

    Method of forming fine grains of Co-Cr-Mo alloy with nitrogen addition and Co-Cr-Mo alloy with nitrogen addition
    8.
    发明授权
    Method of forming fine grains of Co-Cr-Mo alloy with nitrogen addition and Co-Cr-Mo alloy with nitrogen addition 有权
    用氮添加和Co-Cr-Mo合金与氮添加形成Co-Cr-Mo合金细晶粒的方法

    公开(公告)号:US08460485B2

    公开(公告)日:2013-06-11

    申请号:US13060593

    申请日:2009-09-02

    IPC分类号: C22F1/10

    摘要: A Co—Cr—Mo alloy with nitrogen addition composed of 26 to 35% by weight of Cr, 2 to 8% by weight of Mo, 0.1 to 0.3% by weight of N, and balance of Co is subjected to solution treatment and then subjected to isothermal aging treatment holding the alloy at 670 to 830° C. for a predetermined period of time to form a multi-phase structure composed of an ε-phase and a Cr nitride by means of an isothermal aging effect. After cooling, the alloy subjected to reverse transformation treatment in which the alloy is heated at a temperature range of 870 to 1100° C. for reverse transformation to a single γ-phase from the multi-phase structure composed of an ε-phase and a Cr nitride.

    摘要翻译: 将由26〜35重量%的Cr,2〜8重量%的Mo,0.1〜0.3重量%的N和余量的Co组成的Co-Cr-Mo合金进行固溶处理,然后 进行等温时效处理,将合金在670〜830℃保持规定时间,通过等温时效作用形成由ε相和Cr氮化物构成的多相结构体。 冷却后,对合金进行逆相变处理,其中将合金在870〜1100℃的温度范围内加热,以便从由ε相和 氮化铬。

    METHOD OF FORMING FINE GRAINS OF CO-CR-MO ALLOY WITH NITROGEN ADDITION AND CO-CR-MO ALLOY WITH NITROGEN ADDITION
    9.
    发明申请
    METHOD OF FORMING FINE GRAINS OF CO-CR-MO ALLOY WITH NITROGEN ADDITION AND CO-CR-MO ALLOY WITH NITROGEN ADDITION 有权
    用硝酸添加剂和CO-CR-MO合金形成具有硝酸添加剂的CO-CR-MO合金微粒的方法

    公开(公告)号:US20110209799A1

    公开(公告)日:2011-09-01

    申请号:US13060593

    申请日:2009-09-02

    IPC分类号: C23C8/24

    摘要: A Co—Cr—Mo alloy with nitrogen addition composed of 26 to 35% by weight of Cr, 2 to 8% by weight of Mo, 0.1 to 0.3% by weight of N, and balance of Co is subjected to solution treatment and then subjected to isothermal aging treatment holding the alloy at 670 to 830° C. for a predetermined period of time to form a multi-phase structure composed of an ε-phase and a Cr nitride by means of an isothermal aging effect. After cooling, the alloy subjected to reverse transformation treatment in which the alloy is heated at a temperature range of 870 to 1100° C. for reverse transformation to a single γ-phase from the multi-phase structure composed of an ε-phase and a Cr nitride.

    摘要翻译: 将由26〜35重量%的Cr,2〜8重量%的Mo,0.1〜0.3重量%的N和余量的Co组成的Co-Cr-Mo合金进行固溶处理,然后 进行等温时效处理,将合金在670〜830℃保持一段时间,通过等温老化作用形成由相等和氮化铬组成的多相结构。 冷却后,将合金进行逆相变处理,其中将合金在870〜1100℃的温度范围内进行加热,以从由相等相组成的多相结构反相转变成单个γ相, 氮化铬。