| CPC C22C 21/06 (2013.01) [B32B 15/016 (2013.01); C22C 21/16 (2013.01); C22F 1/047 (2013.01)] | 14 Claims |
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1. A rolled composite aerospace product comprising a 2XXX-series core layer and an Al—Mg alloy clad layer coupled to at least one surface of the 2XXX-series core layer, wherein the Al—Mg alloy is a 5XXX-series aluminium alloy comprising 0.4% to 4.8% Mg, wherein the 2XXX-series alloy of the 2XXX-series core layer has a composition comprising, in wt. %,
Cu 1.9% to 7.0%,
Mg 0.30% to 1.8%,
Mn up to 1.2%,
Si up to 0.40%,
Fe up to 0.40%,
Cr up to 0.35%,
Zn up to 1.0%,
Ti up to 0.15%,
Zr up to 0.25%,
V up to 0.25%,
Li up to 2.0%,
Ag up to 0.80%,
Ni up to 2.5%,
balance being aluminium and impurities.
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