Aluminum-Copper-Lithium Alloy With Improved Mechanical Strength and Toughness
AssigneeAlcan Rhenalu
InventorsTimothy WARNER, Christophe SIGLI, Cedric GASQUERES, Armelle DANIELOU
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AssigneeAlcan Rhenalu
InventorsTimothy WARNER, Christophe SIGLI, Cedric GASQUERES, Armelle DANIELOU
Estimating the term…
The invention relates to a wrought product such as an extruded, rolled and/or forged aluminum alloy-based product comprising, in weight %: Cu: 3.0-3.9; Li: 0.8-1.3; Mg; 0.6-1.0; Zr: 0.05-0.18; Ag: 0.0-0.05; Mn: 0.0-0.5; Fe+Si≦0.20; Zn≦0.15; at least one element from among: Ti: 0.01-0.15; Sc: 0.05-0.3; Cr: 0.05-0.3; Hf: 0.05-0.5; other elements ≦0.05 each and ≦0.15 total, remainders aluminum. The invention also relates to the process for producing said product. The products according to the invention are particularly useful in the production of thick aluminum products intended for producing structural elements in the aeronautical industry.
An aluminum-based wrought product that is optionally extruded, rolled and/or forged, said product comprising, in weight %:
A process for producing an extruded, rolled and/or forged aluminum alloy-based product, comprising:
A method for improving the compromise between properties of static mechanical strength and properties of damage tolerance and thermal stability, while having a low density, of aluminum-copper-lithium alloy products comprising increasing the magnesium content in said alloy above what has been previously specified for said alloy and optionally subjecting said alloy to near-peak aging.
Dependencies are inferred from the claim text.