Aluminum alloy for die-casting
    112.
    发明授权
    Aluminum alloy for die-casting 有权
    铝合金压铸

    公开(公告)号:US09045815B2

    公开(公告)日:2015-06-02

    申请号:US13818118

    申请日:2011-12-20

    CPC classification number: C22C21/00 C22C1/026 C22C1/03

    Abstract: The present invention relates to an aluminum alloy for die-casting. More particularly, the present invention relates to an aluminum alloy being usable for die-casting and including 1.0% to 5.0% by weight of Mn, 0.5% to 1.5% by weight of Zn, 1.0% to 2.0% by weight of Zr, 0.5% to 1.5% by weight of Cu and 85% to 97% by weight of aluminum. Surface smut due from silicon smutting is not caused after a molding process so that a product can have a clear color, Furthermore, the aluminum alloy can increase an adhesion strength of a coating layer thereby increasing a durability of a die-casting product. Furthermore, because the aluminum alloy does not include a heavy metal harmful to human being, the aluminum alloy may be non-toxic and environment-friendly.

    Abstract translation: 本发明涉及一种用于压铸的铝合金。 更具体地说,本发明涉及一种可用于压铸的铝合金,包括1.0%至5.0%的Mn,0.5%至1.5%的Zn,1.0%至2.0%的Zr,0.5 %至1.5重量%的Cu和85重量%至97重量%的铝。 在成型工艺之后,不会产生由于硅化而产生的表面污点,所以能够使产品具有清晰的颜色。此外,铝合金可以提高涂层的粘合强度,从而提高压铸产品的耐久性。 此外,由于铝合金不包含对人体有害的重金属,因此铝合金可以是无毒的且环境友好的。

    Al—Mg—Zn wrought alloy product and method of its manufacture
    113.
    发明授权
    Al—Mg—Zn wrought alloy product and method of its manufacture 有权
    Al-Mg-Zn锻造合金产品及其制造方法

    公开(公告)号:US09039848B2

    公开(公告)日:2015-05-26

    申请号:US12742433

    申请日:2008-11-05

    Abstract: An aluminum alloy wrought product including, in wt. %, Mg 3.0 to 7.0, Zn 0.6 to 2.8, Mn 0 to 1.0, Cu 0 to 2.0, Sc 0 to 0.6, at least one element selected from the group of Zr 0.04 to 0.4, Cr 0.04 to 0.4, Hf 0.04 to 0.4 and Ti 0.01 to 0.3; Fe maximum 0.3, Si maximum 0.3, inevitable impurities, and balance aluminum. The range for the Zn-content in wt. % is a function of the Mg-content according to: lower-limit of the Zn-range: [Zn]=0.34[Mg]−0.4, and upper-limit of the Zn-range: [Zn]=0.34[Mg]+0.4.

    Abstract translation: 铝合金锻造产品,以重量计, %,Mg 3.0〜7.0,Zn 0.6〜2.8,Mn 0〜1.0,Cu 0〜2.0,Sc 0〜0.6,选自Zr 0.04〜0.4,Cr 0.04〜0.4,Hf 0.04〜0.4的至少一种元素 和Ti 0.01〜0.3; Fe最大为0.3,Si最大为0.3,不可避免的杂质,余量为铝。 Zn含量在wt。 %是根据以下的Mg含量的函数:Zn范围的下限:[Zn] = 0.34 [Mg] -0.4,Zn范围的上限:[Zn] = 0.34 [Mg] +0.4。

    HIGH-STRENGTH ALUMINUM ALLOY THIN EXTRUDED SHAPE AND METHOD FOR PRODUCING THE SAME
    115.
    发明申请
    HIGH-STRENGTH ALUMINUM ALLOY THIN EXTRUDED SHAPE AND METHOD FOR PRODUCING THE SAME 审中-公开
    高强度铝合金薄型挤压成型及其制造方法

    公开(公告)号:US20150059934A1

    公开(公告)日:2015-03-05

    申请号:US14472902

    申请日:2014-08-29

    CPC classification number: C22F1/053 C22C21/10

    Abstract: An Al—Zn—Mg—Cu-based high-strength aluminum alloy thin extruded shape has a yield strength of 700 MPa or more. The high-strength aluminum alloy thin extruded shape includes 9.0 to 13.0 mass % of Zn, 2.0 to 3.0 mass % of Mg, 1.0 to 2.0 mass % of Cu, and 0.05 to 0.3 mass % of Zr, with the balance being Al and unavoidable impurities, fine precipitates having a circle equivalent diameter of 5 to 20 nm being dispersed in a crystal grain of the extruded shape in a number of 4000 to 6000 per μm2.

    Abstract translation: Al-Zn-Mg-Cu系高强度铝合金薄型挤压成型的屈服强度为700MPa以上。 高强度铝合金薄型挤出形状包括Zn:9.0〜13.0质量%,Mg:2.0〜3.0质量%,Cu:1.0〜2.0质量%,Zr:0.05〜0.3质量%,余量:Al:不可避免 杂质,具有5〜20nm的圆当量直径的微细析出物分散在挤出形状的晶粒中,数量为4000〜6000个/μm2。

    WEAR-RESISTANT ALLOYS HAVING COMPLEX MICROSTRUCTURE
    118.
    发明申请
    WEAR-RESISTANT ALLOYS HAVING COMPLEX MICROSTRUCTURE 审中-公开
    具有复合微结构的耐磨合金

    公开(公告)号:US20140334969A1

    公开(公告)日:2014-11-13

    申请号:US14270628

    申请日:2014-05-06

    Inventor: Hee Sam Kang

    CPC classification number: C22C21/10

    Abstract: A wear-resistant alloy having a complex microstructure is provided. from the microstructure includes a range of about 19 to about 27 wt % of zinc (Zn), a range of about 3 to about 5 wt % of tin (Sn), a range of about 7.6 to about 11 wt % of silicon (Si), and a balance of aluminum (Al).

    Abstract translation: 提供具有复杂微结构的耐磨合金。 从微结构包括约19至约27重量%的锌(Zn),约3至约5重量%的锡(Sn)的范围,约7.6至约11重量%的硅(Si )和余量的铝(Al)。

    HIGH THERMAL CONDUCTIVITY Al-Si-Fe-Zn ALLOY FOR DIE CASTING
    119.
    发明申请
    HIGH THERMAL CONDUCTIVITY Al-Si-Fe-Zn ALLOY FOR DIE CASTING 审中-公开
    高导热性Al-Si-Fe-Zn合金用于铸造

    公开(公告)号:US20140234159A1

    公开(公告)日:2014-08-21

    申请号:US14350080

    申请日:2012-10-09

    CPC classification number: C22C21/10 C22C21/00 C22C21/02

    Abstract: Disclosed is high thermal conductivity Al—Si—Fe—Zn alloy for die casting which comprises 1.0 weight % to 2.0 weight % of silicon (Si), 0.5 weight % to 1.6 weight % of iron (Fe), 0.6 weight % to 1.6 weight % of zinc (Zn), with the remainder being aluminum (Al) and inevitable impurities.

    Abstract translation: 公开了用于压铸的高导热性Al-Si-Fe-Zn合金,其包含1.0重量%至2.0重量%的硅(Si),0.5重量%至1.6重量%的铁(Fe),0.6重量%至1.6重量% %的锌(Zn),其余为铝(Al)和不可避免的杂质。

    Aluminum alloy products having improved property combinations and method for artificially aging same
    120.
    发明授权
    Aluminum alloy products having improved property combinations and method for artificially aging same 有权
    铝合金产品具有改善的性能组合和人造老化方法

    公开(公告)号:US08673209B2

    公开(公告)日:2014-03-18

    申请号:US11748021

    申请日:2007-05-14

    Abstract: Aluminum alloy products about 4 inches thick or less that possesses the ability to achieve, when solution heat treated, quenched, and artificially aged, and in parts made from the products, an improved combination of strength, fracture toughness and corrosion resistance, the alloy consisting essentially of: about 6.8 to about 8.5 wt. % Zn, about 1.5 to about 2.00 wt. % Mg, about 1.75 to about 2.3 wt. % Cu; about 0.05 to about 0.3 wt. % Zr, less than about 0.1 wt. % Mn, less than about 0.05 wt. % Cr, the balance Al, incidental elements and impurities and a method for making same. The invention alloy is useful in making structural members for commercial airplanes including, but not limited to, upper wing skins and stringers, spar caps, spar webs and ribs of either built-up or integral construction. The invention alloy may be aged by 2 or 3 step practices while exceeding the SCC requirements for applications for which the invention alloy is primarily intended. The flexibility of the invention in this regard is useful for its application in multi-alloy or multi-material systems joined by welding or bonding and subsequently aged.

    Abstract translation: 约4英寸厚或以下的铝合金产品具有在固溶热处理,淬火和人工老化的同时实现的能力,以及由产品制成的零件中,改进了强度,断裂韧性和耐腐蚀性的组合,该合金组成 基本上为:约6.8至约8.5wt。 %Zn,约1.5至约2.00wt。 %Mg,约1.75至约2.3wt。 %Cu; 约0.05至约0.3wt。 %Zr,小于约0.1wt。 %Mn,小于约0.05wt。 %Cr,余量为Al,附带元素和杂质及其制备方法。 本发明合金可用于制造商用飞机的结构构件,包括但不限于上部翼皮和桁条,翼梁盖,翼梁腹板和构成或整体结构的肋。 本发明合金可以通过2或3步骤的方式老化,同时超过本发明合金主要用途的应用的SCC要求。 在这方面,本发明的灵活性对于其在通过焊接或粘合并随后老化而连接的多合金或多材料体系中的应用是有用的。

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