Method for producing fine-grained, high strength aluminum alloy material
    11.
    发明授权
    Method for producing fine-grained, high strength aluminum alloy material 失效
    生产细粒度,高强度铝合金材料的方法

    公开(公告)号:US4462843A

    公开(公告)日:1984-07-31

    申请号:US355058

    申请日:1982-03-05

    申请人: Yoshio Baba Teruo Uno

    发明人: Yoshio Baba Teruo Uno

    CPC分类号: C22F1/053

    摘要: An aluminum alloy material having a high strength, small grain size, good resistance to stress corrosion cracking and very high degree of workability is produced from an aluminum base alloy consisting essentially of 5.1 to 8.1 wt. % Zn, 1.8 to 3.4 wt. % Mg, 1.2 to 2.6 wt. % Cu, up to 0.2 wt. % Ti and at least one of 0.18 to 0.35 wt. % Cr and 0.05 to 0.25 wt. % Zr, the balance being aluminum and impurities by an improved production method described in detail in the disclosure. The improved method is particularly characterized by a special annealing step in a continuous annealing furnace under the application of a tension not exceeding 2 kg/mm.sup.2 to a coiled alloy sheet to be annealed, the annealing including rapid heating of the coiled alloy sheet to a temperature of 400.degree. to 500.degree. C. at a heating rate exceeding 50.degree. C./min.

    摘要翻译: 具有高强度,小晶粒尺寸,良好的耐应力腐蚀开裂性和非常高的可加工性的铝合金材料由基本上由5.1至8.1重量%组成的铝基合金制成。 %Zn,1.8〜3.4wt。 %Mg,1.2〜2.6wt。 %Cu,高达0.2wt。 %Ti和0.18〜0.35重量%中的至少一个。 %Cr和0.05〜0.25wt。 %Zr,余量为铝和杂质,通过本公开中详细描述的改进的制备方法。 该改进方法的特征在于,在连续退火炉中,对于待退火的盘绕合金板,在不超过2kg / mm 2的张力下施加特殊的退火步骤,所述退火包括将盘绕的合金板快速加热至温度 400℃〜500℃,加热速度超过50℃/分钟。

    Aircraft stringer material
    13.
    发明授权
    Aircraft stringer material 失效
    飞机纵梁材料

    公开(公告)号:US4569703A

    公开(公告)日:1986-02-11

    申请号:US500200

    申请日:1983-06-01

    IPC分类号: B64C1/06 C22F1/053 C22C21/10

    摘要: An aircraft stringer material having high strength, small grain size, good resistance to stress corrosion cracking and a very high degree of workability is produced from an aluminum base alloy consisting essentially of 5.1 to 8.1 wt. % Zn, 1.8 to 3.4 wt. % Mg, 1.2 to 2.6 wt. % Cu, up to 0.20 wt. % Ti and at least one of 0.18 to 0.35 wt. % Cr and 0.05 to 0.25 wt. % Zr, the balance being aluminum and impurities, by a production method characterized by a special annealing step including rapid heating to a temperature of 320.degree. to 500.degree. C. at a heating rate exceeding 11.degree. C./min.Further, a corrosion-resistant stringer material is produced in a manner very similar to the above production method, using the above aluminum alloy as a core and AA7072 alloy as cladding.

    摘要翻译: 具有高强度,小颗粒尺寸,良好的耐应力腐蚀开裂性和非常高的可加工性的飞机纵梁材料由基本上由5.1至8.1重量%组成的铝基合金制成。 %Zn,1.8〜3.4wt。 %Mg,1.2〜2.6wt。 %Cu,高达0.20wt。 %Ti和0.18〜0.35重量%中的至少一个。 %Cr和0.05〜0.25wt。 %Zr,余量为铝和杂质,通过特殊退火步骤的制备方法,包括以超过11℃/分钟的加热速度快速加热至320至500℃的温度。 此外,使用上述铝合金作为芯和AA7072合金作为包层,以与上述制造方法非常相似的方式制造耐腐蚀纵梁材料。

    Process for preparing hard tempered aluminum alloy sheet
    14.
    发明授权
    Process for preparing hard tempered aluminum alloy sheet 失效
    硬质铝合金板的制备方法

    公开(公告)号:US4284437A

    公开(公告)日:1981-08-18

    申请号:US105008

    申请日:1979-12-18

    CPC分类号: C22F1/047 C22F1/08

    摘要: A hard tempered aluminum alloy sheet useful for deep drawing is prepared by a process comprising the steps of hot rolling an ingot of aluminum alloy consisting essentially of 4.0 to 6.0 Mg wt. %, at least one component selected from the group consisting of 0.1 to 0.7 wt. % Mn, 0.01 to 0.05 wt. % Zr, 0.005 to 0.12 wt. % V and up to 0.05 wt. % Ti and the balance aluminum to a sheet not more than 2.5 mm thick, intermediate annealing the hot rolled alloy and final cold rolling the annealed alloy to effect a rolling reduction of less than 85%.In case the finishing temperature of the hot rolling is adjusted to a temperature of 300.degree. to 350.degree. C., the above intermediate annealing can be omitted.

    摘要翻译: 用于深拉伸的硬质回火铝合金板通过包括以下步骤的方法制备,所述方法包括以下步骤:将基本上由4.0至6.0重量% %,选自0.1至0.7重量%的至少一种组分。 %Mn,0.01〜0.05重量% %Zr,0.005〜0.12重量% %V和高达0.05wt。 %Ti,余量为铝到不超过2.5mm厚的板,中间退火热轧合金,最终冷轧退火合金,以实现小于85%的轧制压下率。 在热轧的终轧温度调节至300〜350℃的温度的情况下,可以省略上述的中间退火。

    Aluminum alloy sheet
    15.
    发明授权
    Aluminum alloy sheet 失效
    铝合金板

    公开(公告)号:US4140556A

    公开(公告)日:1979-02-20

    申请号:US788157

    申请日:1977-04-14

    申请人: Yoshio Baba Teruo Uno

    发明人: Yoshio Baba Teruo Uno

    IPC分类号: C22C21/06

    CPC分类号: C22C21/06

    摘要: An aluminum alloy, excellent concurrently in strength and formability, suitably used in car bodies, essentially contains Mg within the range between 3.5 and 5.5%, Zn within the range between 0.5 and 2.0%, and Cu within the range between 0.3 and 1.2%, wherein percents are all by weight; and another still further improved aluminum alloy, excellent concurrently in strength and formability, suitable for similar use, and finer in grain size, indispensably contains all the abovementioned three essential elements in the same ranges of percent by weight, and has optionally added thereto one or more of the elements selected from Mn within the range between 0.05 and 0.4%, Cr within the range between 0.05 and 0.25%, Zr within the range between 0.05 and 0.25%, and V within the range between 0.01 and 0.15%, wherein percents are all by weight.

    摘要翻译: 合适地用于车身中的铝合金的强度和成形性优异,基本上含有Mg在3.5〜5.5%的范围内,Zn在0.5〜2.0%的范围内,Cu在0.3〜1.2%的范围内, 其中百分比全部为重量; 另外还有进一步改进的铝合金,强度和成型性同时优异,适用于类似用途,粒度更细,在相同重量百分比范围内必不可少地含有上述所有三种必需元素,并且任选加入一种或多种 选自Mn在0.05〜0.4%范围内的更多元素,Cr在0.05〜0.25%的范围内,Zr在0.05〜0.25%范围内,V在0.01〜0.15%的范围内,其中百分比为 全部重量

    Process for the desulfurization of light oils
    16.
    发明授权
    Process for the desulfurization of light oils 失效
    轻油脱硫工艺

    公开(公告)号:US3960683A

    公开(公告)日:1976-06-01

    申请号:US491103

    申请日:1974-07-23

    申请人: Yoshio Baba

    发明人: Yoshio Baba

    摘要: A process for the desulfurization of light oils, which comprises irradiat light oils containing sulfur compounds such as mercaptans and sulfides with ultraviolet rays to decompose the sulfur compounds into water-soluble compounds and thereafter, washing the light oils with water to remove the water-soluble compounds.

    摘要翻译: 一种轻油脱硫的方法,其中包括用紫外线照射含硫化合物如硫醇和硫化物的轻油将硫化合物分解为水溶性化合物,然后用水洗涤轻油以除去水溶性 化合物。