ALUMINUM ALLOY FIN MATERIAL FOR HEAT EXCHANGERS, AND METHOD OF PRODUCING THE SAME, AND HEAT EXCHANGER
    5.
    发明申请
    ALUMINUM ALLOY FIN MATERIAL FOR HEAT EXCHANGERS, AND METHOD OF PRODUCING THE SAME, AND HEAT EXCHANGER 审中-公开
    用于热交换器的铝合金材料及其生产方法和热交换器

    公开(公告)号:US20170003085A1

    公开(公告)日:2017-01-05

    申请号:US15269436

    申请日:2016-09-19

    Abstract: A heat exchanger aluminum alloy fin material, comprising Si 0.5 to 1.5 mass %; Fe 0.1 to 1.0 mass %; Mn 0.8 to 2.2 mass %; Zn 0.4 to 2.5 mass %; and further at least one selected from Cu, Ti, Zr, Cr, and V each in 0.02 to 0.3 mass %, with the balance being Al and unavoidable impurities, wherein a metallographic microstructure before braze-heating is such that a density of second phase particles having a circle-equivalent diameter of less than 0.1 μm is less than 1×107 particles/mm2, and that a density of second phase particles having a circle-equivalent diameter of 0.1 μm or more is 5×104 particles/mm2 or more, wherein a tensile strength before braze-heating, TSB, a tensile strength after braze-heating, TSA, and a sheet thickness of the fin material, t, satisfy: 0.4≦(TSB−TSA)/t≦2.1, and wherein the sheet thickness is 150 μm or less.

    Abstract translation: 一种热交换器铝合金翅片材料,其包含0.5〜1.5质量%的Si; Fe 0.1〜1.0质量% Mn 0.8〜2.2质量% Zn 0.4〜2.5质量% 进一步选自Cu,Ti,Zr,Cr和V中的至少一种为0.02〜0.3质量%,余量为Al和不可避免的杂质,其中钎焊前的金相组织使得第二相的密度 圆当量直径小于0.1μm的颗粒小于1×10 7个/ mm 2,圆当量直径为0.1μm以上的第二相粒子的密度为5×10 4个/ mm 2以上 其中,钎焊加热前的拉伸强度,TSB,钎焊后的拉伸强度,TSA,翅片材料的板厚t满足:0.4≤(TSB-TSA)/t≤2.1,其中, 片材厚度为150μm以下。

    ALUMINUM ALLOY FIN MATERIAL FOR HEAT EXCHANGERS, AND METHOD OF PRODUCING THE SAME
    9.
    发明申请
    ALUMINUM ALLOY FIN MATERIAL FOR HEAT EXCHANGERS, AND METHOD OF PRODUCING THE SAME 审中-公开
    用于热交换器的铝合金材料及其制造方法

    公开(公告)号:US20160116236A1

    公开(公告)日:2016-04-28

    申请号:US14987387

    申请日:2016-01-04

    Abstract: An aluminum alloy fin material for heat exchangers, containing 0.5 to 1.5 mass % of Si; more than 1.0 mass % but not more than 2.0 mass % of Fe; 0.4 to 1.0 mass % of Mn; and 0.4 to 1.0 mass % of Zn, with the balance being Al and unavoidable impurities, wherein a metallographic microstructure before braze-heating is such that a density of second phase particles having a circle-equivalent diameter of less than 0.1 μm is less than 1×107 particles/mm2, and that a density of second phase particles having a circle-equivalent diameter of 0.1 μm or more is 1×105 particles/mm2 or more, wherein a tensile strength before braze-heating, TSB (N/mm2), a tensile strength after braze-heating, TSA (N/mm2), and a fin sheet thickness, t (μm), satisfy: 0.4≦(TSB−TSA)/t≦2.1, and wherein the sheet thickness is 150 μm or less; and a method of producing the same.

    Abstract translation: 一种用于热交换器的铝合金翅片材料,含有0.5至1.5质量%的Si; 大于1.0质量%但不超过2.0质量%的Fe; 0.4〜1.0质量%的Mn; 和0.4〜1.0质量%的Zn,余量为Al和不可避免的杂质,其中钎焊前的金相组织使得圆当量直径小于0.1μm的第二相粒子的密度小于1 ×107个/ mm 2,圆当量直径为0.1μm以上的第二相粒子的密度为1×10 5个/ mm 2以上,钎焊加热前的拉伸强度,TSB(N / mm2) ,钎焊后的拉伸强度,TSA(N / mm2),翅片片厚度t(μm)满足:0.4≦̸(TSB-TSA)/ t≦̸ 2.1,其中片材厚度为150μm 或更少; 及其制造方法。

Patent Agency Ranking