High strength L1
View Patent ↗High strength heat treatable aluminum alloys that can be used at temperatures from about −420° F. (−251° C.) up to about 650° F. (343° C.) are described. The alloys are strengthened by dispersion of particles based on the L1 2 intermetallic compound Al 3 X. These alloys comprise aluminum, copper, magnesium, at least one of scandium, erbium, thulium, ytterbium, and lutetium; and at least one of gadolinium, yttrium, zirconium, titanium, hafnium, and niobium.
1. A heat treatable aluminum alloy consisting of:
about 1.0 to about 8.0 weight percent copper;
about 0.2 to about 4.0 weight percent magnesium;
at least one first element selected from the group consisting of about 0.1 to about 0.5 weight percent scandium; about 0.1 to about 6.0 weight percent erbium, about 0.1 to about 10.0 weight percent thulium, about 0.1 to about 15.0 weight percent ytterbium, and about 0.1 to about 12.0 weight percent lutetium;
at least one second element selected from the group consisting of about 0.1 to about 4.0 weight percent gadolinium, about 0.1 to about 4.0 weight percent yttrium, about 0.05 to about 1.0 weight percent zirconium, about 0.05 to about 2.0 weight percent titanium, about 0.05 to about 2.0 weight percent hafnium, and about 0.05 to about 1.0 weight percent niobium; and
the balance substantially aluminum.
2. The alloy of claim 1 , wherein the alloy has an aluminum solid solution matrix containing a plurality of dispersed Al 3 X second phases having L1 2 structures, wherein X includes at least one first element and at least one second element.
3. A heat treatable aluminum alloy consisting of:
about 1.0 to about 8.0 weight percent copper;
about 0.2 to about 4.0 weight percent magnesium;
at least one first element selected from the group consisting of about 0.1 to about 0.5 weight percent scandium;
about 0.1 to about 6.0 weight percent erbium, about 0.1 to about 10.0 weight percent thulium, about 0.1 to about 15.0 weight percent ytterbium, and about 0.1 to about 12.0 weight percent lutetium;
at least one second element selected from the group consisting of about 0.1 to about 4.0 weight percent gadolinium, about 0.1 to about 4.0 weight percent yttrium, about 0.05 to about 1.0 weight percent zirconium, about 0.05 to about 2.0 weight percent titanium, about 0.05 to about 2.0 weight percent hafnium, and about 0.05 to about 1.0 weight percent niobium;
at least one of about 0.001 weight percent to about 0.1 weight percent sodium, about 0.001 weight percent to about 0.1 weight calcium, about 0.001 weight percent to about 0.1 weight percent strontium, about 0.001 weight percent to about 0.1 weight percent antimony, about 0.001 weight percent to about 0.1 weight percent barium and about 0.001 weight percent to about 0.1 weight percent phosphorus; and the balance substantially aluminum.
4. A heat treatable aluminum alloy consisting of:
about 1.0 to about 8.0 weight percent copper;
about 0.2 to about 4.0 weight percent magnesium;
at least one first element selected from the group consisting of about 0.1 to about 0.5 weight percent scandium; about 0.1 to about 6.0 weight percent erbium, about 0.1 to about 10.0 weight percent thulium, about 0.1 to about 15.0 weight percent ytterbium, and about 0.1 to about 12.0 weight percent lutetium;
at least one second element selected from the group consisting of about 0.1 to about 4.0 weight percent gadolinium, about 0.1 to about 4.0 weight percent yttrium, about 0.05 to about 1.0 weight percent zirconium, about 0.05 to about 2.0 weight percent titanium, about 0.05 to about 2.0 weight percent hafnium, and about 0.05 to about 1.0 weight percent niobium; and
no more than about 0.1 weight percent iron, about 0.1 weight percent chromium, about 0.1 weight percent manganese, about 0.1 weight percent vanadium, about 0.1 weight percent cobalt, and about 0.1 weight percent nickel; and
the balance substantially aluminum.
5. The alloy of claim 1 , wherein the alloy is formed by a process selected from casting, deformation processing, or rapid solidification processing.
6. The alloy of claim 5 , wherein the alloy is heat treated after forming.
7. The alloy of claim 6 , wherein the alloy is heat treated by a solution anneal at about 800° F. (426° C.) to about 1100° F. (593° C.) for about 30 minutes to four hours, followed by quenching.
8. The alloy of claim 7 , wherein the quenching is in liquid.
9. The alloy of claim 8 , wherein the alloy is aged after quenching.
10. The alloy of claim 9 , wherein the aging occurs at a temperature of about 200° F. (93° C.) to about 600° F. (316° C.) for about two to forty-eight hours.
11. The heat treatable aluminum alloy of claim 1 , wherein the alloy is capable of being used at temperatures from about −420° F. (−251° C.) up to about 650° F. (343° C.).