Al—Cu—Mg—Ag—Mn-alloy for structural applications requiring high strength and high ductility
View Patent ↗An aluminum alloy having improved strength and ductility, comprising: Cu 3.5–5.8 wt. %, Mg 0.1–1.8 wt. % Mn 0.1–0.8 wt. % Ag 0.2–0.8 wt. % Ti 0.02–0.12 wt. % and optionally one or more selected from the group consisting of Cr 0.1–0.8 wt. %, Hf 0.1–1.0 wt. %, Sc 0.03–0.6 wt. %, and V 0.05–0.15 wt. %. balance aluminum and incidental elements and impurities, and wherein the alloy is substantially zirconium-free.
1. An aluminum alloy having improved strength and ductility, comprising:
a) Cu4.7–5.2wt. %,
Mg 0.2–0.6 wt. %
Mn 0.2–0.5 wt. %
Ag 0.2–0.5 wt. %
Ti 0.03–0.09 wt. % and
optionally one or more selected from the group consisting of Cr 0.1–0.8 wt. %, Hf 0.1–1.0 wt. %, Sc 0.05–0.6 wt. %, and V 0.05–0.15 wt. %.
b) balance aluminum and normal and/or inevitable elements and impurities, and wherein said alloy is substantially zirconium-free.
2. An aluminum alloy according to claim 1 , wherein Zr is less than 0.03 wt. %.
3. An aluminum alloy according to claim 1 , wherein Zr is less than 0.01 wt. %.
4. A sheet comprising an aluminum alloy that is substantially free of zirconium according to claim 1 , said sheet having a thickness ranging from about 2 mm to aboat 10 mm, and a fracture toughness K C , determined at room temperature from the R-curve measure on a 406 mm wide CCT panel in the L-T orientation, which equals or exceeds about 170 MPa√m, and the fatigue crack propagation rate determined according to ASTM E 647 on a CCT-specimen having a width of 400 mm, at constant amplitude R=0.1 that is equal to or below about 3.0 10 −2 mm/cycle at ΔK=60 Mpa√m.
5. A sheet comprising an aluminum alloy that is substantially free of zirconium according to claim 1 , said sheet having a thickness ranging from about 5 mm to about 25 mm and an elongation of at least about 13.5 % and a UTS of at least about 69.5 ksi (479.2 MPa), and/or an elongation of at least about 15.5% and a UTS of at least about 69 ksi (475.7 MPa).