High fracture toughness aluminum-copper-lithium sheet or light-gauge plate suitable for use in a fuselage panel
AssigneeAlcan Rhenalu
InventorsBernard Bés, Hervé Ribes, Christophe Sigli, Timothy Warner
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AssigneeAlcan Rhenalu
InventorsBernard Bés, Hervé Ribes, Christophe Sigli, Timothy Warner
Estimating the term…
A low density aluminum based alloy useful in aircraft structure for fuselage sheet or light-gauge plate applications which has high strength, high fracture toughness and high corrosion resistance, comprising 2.7 to 3.4 weight percent Cu, 0.8 to 1.4 weight percent Li, 0.1 to 0.8 weight percent Ag, 0.2 to 0.6 weight percent Mg and a grain refiner such as Zr, Mn, Cr, Sc, Hf, Ti or a combination thereof, the amount of which being 0.05 to 0.13 wt. % for Zr, 0.1 to 0.8 wt. % for Mn, 0.05 to 0.3 wt. % for Cr and Sc, 0.05 to 0.5 wt. % for Hf and 0.05 to 0.15 wt. % for Ti. The amount of Cu and Li preferably corresponds to the formula Cu(wt. %)+5/3 Li(wt. %)<5.2.
A method for producing an aluminum alloy sheet or a light-gauge plate having
A method for producing an aluminum alloy sheet or light-gauge plate having high fracture toughness and strength, said method comprising:
A method for producing an aluminum alloy sheet or a light-gauge plate having high fracture toughness and strength, said method comprising:
A rolled, forged and/or extruded aluminum alloy consisting essentially of 2.7 to 3.4 wt. % Cu,
Dependencies are inferred from the claim text.