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PROCESS FOR THE PREPARATION OF A HIGH RESISTANCE AI-Zn-Mg-Cu ALLOY

机译:高电阻Al-Zn-Mg-Cu合金的制备方法

摘要

The present invention relates to a process for the preparation of a high strength Al-Zn-Mg-Cu alloy, which has improved tensile strength and high damage tolerance, including the molding steps of an ingot having the following composition (in weight percent): Zn 5.5-9.5, Cu 1.5-3.5, Mg 1.5-3.5, Mn 0.25 Zr 0.25 , Cr 0, 10, Fe 0, 25, Si 0, 25, Ti 0, 10, Hf and / or V 0, 25, other elements each present in a proportion of less than 0.05 % and in total in a proportion of minus 0, 15%, the balance being aluminum, homogenization and / or preheating the ingot after molding, hot working and possibly cold working to obtain a more worked product 50 mm thick, solution heat treatment, quenching of the solution heat treatment product, and artificial aging of the worked and heat-treated product, the artificial aging step comprising a first heat treatment at a temperature of 105 to 135 ° C for more than two hours to less than 8 hours and a second heat treatment at a temperature of more than 135 ° C but less than 170 ° C for more than 5 hours to less than 15 hours. The present invention relates to a plate weldable product prepared from such Al-ZnMg-Cu alloy having a thickness of more than 50 mm and a prepared aircraft structural part of such alloy. / P
机译:本发明涉及一种制备高强度Al-Zn-Mg-Cu合金的方法,该方法具有提高的拉伸强度和高的损伤耐受性,包括具有以下组成(重量百分比)的铸锭的模制步骤:锌5.5-9.5,铜1.5-3.5,镁1.5-3.5,Mn <0.25 Zr <0.25,Cr <0,10,Fe <0,25,Si <0,25,Ti <0,10,Hf和/或V <0,25,其他元素的含量均小于0.05%,总含量为负0、15%,其余为铝,均质化和/或在成型,热加工后可能预热铸锭进行冷加工以获得厚度为50 mm的更多加工产品,固溶热处理,固溶热处理产品的淬火以及经加工和热处理的产品的人工时效,该人工时效步骤包括在105°C的温度下进行第一次热处理到135°C超过2小时至不到8小时,然后在135°C以上进行第二次热处理C但在低于170°C的温度下超过5小时到不到15小时。本发明涉及一种由这种厚度大于50mm的Al-ZnMg-Cu合金制成的板状可焊接产品,以及由这种合金制成的飞机结构部件。

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