Aluminum alloy
The present disclosure relates to an alloy containing aluminum and magnesium, a method for the preparation of the alloy, a method for the preparation of a product containing the alloy, and a product containing the alloy. An aluminium alloy having good mechanical properties, in particular high tensile strength, high yield strength and high elongation, while allowing the use of the alloy in both casting and forming processes is disclosed.
1. An aluminum alloy, comprising:
a. from 9 to 14% by mass of magnesium (Mg);
b. from 0.15 to 1% by mass of titanium (Ti);
c. from 0.0001 to 0.1% by mass of manganese (Mn);
d. from 0 to 0.1% by mass of iron (Fe);
e. from 0.001 to 0.1% by mass of beryllium (Be);
f. from 0.0009 to 0.2% by mass of boron (B);
g. from 0 to 0.01% by mass of copper (Cu);
h. from 0 to 0.5% by mass of silicon (Si); and
i. from 0 to 0.01% by mass of zinc (Zn),
and inevitable impurities in a total amount of less than 0.15% by mass, with the balance being aluminum (Al);
wherein each is in relation to the total mass of the aluminum alloy, and wherein all compounds a. through i., Al plus inevitable impurities of the aluminum alloy add up to a total of 100% by mass; and
wherein said aluminum alloy has an elongation of at least 20%.
2. The aluminum alloy according to claim 1 , wherein the aluminum alloy comprises
inevitable impurities, wherein each individual impurity is present in an amount of less than 0.05% by mass.
3. The aluminum alloy according to claim 1 , wherein Mg is present in an amount of from 9.1 to 13.9% by mass.
4. The aluminum alloy according to claim 1 , wherein Ti is present in an amount of from 0.2 to 0.9% by mass.
5. The aluminum alloy according to claim 1 , wherein Mn is present in an amount of from 0.0005 to 0.09% by mass.
6. The aluminum alloy according to claim 1 , wherein Fe is present in an amount of from 0.01 to 0.09% by mass.
7. The aluminum alloy according to claim 1 , wherein Be is present in an amount of from 0.002 to 0.09% by mass.
8. The aluminum alloy according to claim 1 , wherein Bis present in an amount of from 0.001 to 0.15% by mass.
9. The aluminum alloy according to claim 1 , wherein Si is present in an amount of from 0.01 to 0.5% by mass.
10. The aluminum alloy according to claim 1 , wherein Cu is present in an amount of 0.0001 to 0.005% by mass.
11. The aluminum alloy according to claim 1 , wherein Zn is present in an amount of from 0.001 to 0.01% by mass.
12. The aluminum alloy according to claim 2 , wherein the inevitable impurities are present in an amount of less than 0.05% by mass, and wherein each individual impurity is present in an amount of less than 0.001% by mass.
13. The aluminum alloy according to claim 1 , wherein said aluminum alloy has a tensile strength of at least 290 MPa.
14. The aluminum alloy according to claim 1 , wherein said aluminum alloy has a yield strength of at least 170 MPa.
15. The aluminum alloy according to claim 1 , wherein said aluminum alloy has an elongation of at least 30%.
16. The aluminum alloy according to claim 1 , wherein the elongation is determined after said aluminum alloy was heat treated at a temperature of at least 380° C. for at least 1 h.
17. The aluminum alloy according to claim 1 , wherein the elongation is determined after said aluminum alloy was heat treated at a temperature of at least 430° C. for at least 3 h.
18. The aluminum alloy according to claim 1 , wherein the elongation is determined after said aluminum alloy was heat treated at a temperature of at least 450° C. for at least 3 h.