发明名称 FORFARANDE FOR FRAMSTELLNING AV EN PRODUKT AV EN ALUMINIUMLEGERING
摘要 A 7000 series aluminum alloy characterized by high strength, high fatigue resistance and high fracture toughness consists essentially of 5.9 to 6.9% zinc, 2.0 to 2.7% magnesium, 1.9 to 2.5% copper, 0.08 to 0.15% zirconium, a maximum of 0.15% iron, a maximum of 0.12% silicon, a maximum of 0.06% titanium, a maximum of 0.04% chromium, a maximum of 0.05% for each of any other trace elements present in the alloy, the total of the other trace elements in the alloy being a maximum of 0.15%, the balance of the alloy being aluminum. The foregoing alloy is hot worked to provide a wrought product, such as an extruded or plate product, in which recrystallization is held to a minimum. The wrought product is subjected to a solution treatment, quench, and elevated temperature aging cycle, normally until the product is at or near its maximum strength.
申请公布号 SE447128(B) 申请公布日期 1986.10.27
申请号 SE19800003997 申请日期 1980.05.29
申请人 THE BOEING COMPANY 发明人 M V * HYATT;W E * QUIST
分类号 C22C21/10;C22F1/04;C22F1/053;(IPC1-7):C22C21/10 主分类号 C22C21/10
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