The invention relates to a process for manufacturing a thin sheet made of an aluminum-based alloy comprising, in percent by weight, 2.2 to 2.7% Cu,1.3 to 1.6% Li, less than 0.1% Ag, 0.2 to 0.5% Mg, 0.1 to 0.5% Mn, 0.01 to 0.15% Ti, less than 0.3% Zn, no more than 0.1% Fe and no more than 0.1% Si, and inevitable impurities at a content of no more than 0.05% by weight each and 0.15% by weight in total, the remainder being aluminum, wherein, in particular, the hot-rolling input temperature is between 400°C and 460°C and the hot-rolling output temperature is less than 300°C, the mean heating rate during the solution heat treatment is at least approximately 17°C/min between 300°C et 400°C, and the tempering conditions such as the 0.2% offset yield strength in the transverse direction Rp0.2(TL) ranges from 350 to 380 MPa. The sheets according to the invention have advantageous mechanical properties and are used in particular for manufacturing aircraft fuselage panels.
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机译:本发明涉及一种制造由铝基合金制成的薄片的方法,其包含百分比重量为2.2-2.7%Cu,1.3至1.6%Li,小于0.1%Ag,0.2至0.5%Mg,0.1 0.5%Mn,0.01至0.15%Ti,小于0.3%Zn,不超过0.1%Fe,不超过0.1%Si,并且不可避免的杂质,含量不超过0.05重量%和0.15%总重量总,剩余的铝,其中,特别地,热轧制输入温度在400℃和460℃之间,热轧输出温度小于300°C,溶液期间的平均加热速率热处理在300℃/ met 400℃之间至少约17℃/ min,以及诸如0.2%偏移屈服强度的回火条件Rp0.2(T1)的范围为350至380MPa。根据本发明的片材具有有利的机械性能,特别用于制造飞机机身面板。
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