High-strength, high toughness Al-Zn alloy product and method for producing such product
View Patent ↗Disclosed is a Al—Zn alloy wrought product, and a method of manufacturing such a product, with an improved combination of high toughness and high strength by maintaining good corrosion resistance, the alloy including (in weight percent): Zn 6.0-11.0, Cu 1.4-2.2, Mg 1.4-2.4, Zr 0.05-0.15, Ti <0.05, Hf and/or V <0.25, and optionally Sc and/or Ce 0.05-0.25, and Mn 0.05-0.12, other elements each less than 0.05 and less than 0.50 in total, balance aluminium, wherein such alloy has an essentially fully unrecrystallized microstructure at least at the position T/10 of the finished product.
1. Method for producing a high strength, high toughness Al—Zn alloy product with good corrosion resistance, consisting of the sequential steps of:
a) casting an ingot with the following composition, in weight percent:
Zn 6.0 to 11.0%
Cu 1.4 to 2.2%
Mg 1.4 to 2.4%
Zr 0.05 to 0.15%
Ti <0.05%
Hf and/or V <0.25%,
optionally Sc and/or Ce 0.05 to 0.25%,
optionally Mn 0.05 to 0.12%, and
inevitable impurities and balance aluminium,
b) homogenising or pre-heating the ingot after casting,
c) in a first hot rolling step, hot rolling the homogenised or pre-heated ingot into a pre-worked product,
d) reheating the pre-worked product, and then in a second hot rolling step hot rolling the reheated product to a thickness in a range selected from the group consisting of about 150 to 250 (in final-gauge %) or about 105 to 140 (in final-gauge %) at low temperatures in the range of 300° C. to 420° C. to prevent the alloy product from recrystallising and then, after the second hot rolling step, cold rolling the reheated product to a final gauge, wherein the final gauge has a thickness of from 4 to 60 mm,
e) solution heat-treating the cold-rolled product and quenching the solution heat-treated product,
f) optionally stretching or compressing of the quenched alloy product,
g) artificially ageing the reheated, hot- and cold-rolled, solution heat-treated, quenched and optionally stretched or compressed alloy product by a two-step ageing treatment to produce the alloy product to have a T79 or T76 temper, wherein the first ageing step is at a temperature in a range of 105 to 135° C. for 2 to 20 hours and the second ageing step is at a temperature higher than 135° C. but less than 210° C. for 4 to 12 hours to a temper selected from T79 and T76 temper, and wherein more than 80% of the gauge of the artificially aged alloy product has a substantially unrecrystallised microstructure.
2. Method according to claim 1 , wherein the artificial ageing during step g) consists of a first ageing step at a temperature around 120° C. for 2 to 20 hours and a second ageing step at a temperature higher than 135° C. but less than 210° C. for 4 to 12 hours to a temper selected from T79 and T76 temper.
3. Method according to claim 1 , wherein the artificial ageing during step g) consists of a first ageing step at a temperature around 120° C. for 2 to 20 hours and a second ageing step at a temperature around 155° C. to 160° C. for 4 to 12 hours to a temper selected from T79 and T76 temper.
4. Method according to claim 1 , wherein the amount of Zn is in a range of 7.4 to 9.6 wt. %.
5. Method according to claim 1 , wherein the amount of Zn is in a range of 8.0 to 9.6 wt. %.
6. Method according to claim 1 , wherein the amount of Zn is in a range of 7.4 to 8.9 wt. %.
7. Method according to claim 1 , wherein the amount of Zn is in a range of 8.4 to 8.9 wt. %.
8. Method according to claim 1 , wherein the amount of Cu is in a range of 1.7 to 2.2 wt. %.
9. Method according to claim 1 , wherein the amount of Cu is in a range of 1.8 to 2.1 wt. %.
10. Method according to claim 1 , wherein the amount of Mg is in a range of 1.7 to 2.2 wt. %.
11. Method according to claim 1 , wherein the amount of Mg is in a range of 1.7 to 2.1 wt. %.
12. Method according to claim 1 , wherein the amount of Sc is in a range of [Zr]+1.5 [Sc]<0.15 wt. %.
13. Method according to claim 1 , wherein the amount of Sc is in a range of 0.03 to 0.06 wt. %.
14. Method according to claim 1 , wherein the amount of Ce is in a range of 0.03 to 0.06 wt. %.
15. Method according to claim 1 , wherein the amount of inevitable impurities are <0.5 wt. % in total.
16. Method according to claim 1 , wherein the amount of inevitable impurities are <0.05 wt. % each.
17. Method according to claim 1 , wherein the finished rolled product of more than 90% of the gauge has a substantially unrecrystallised microstructure.
18. Method according to claim 1 , wherein the Al—Zn product is a thin plate having a gauge in a range of 20 to 60 mm.
19. Method according to claim 1 , wherein the Al—Zn product is a thin plate having a gauge in the range of 30 to 50 mm.
20. Method according to claim 1 , wherein the Al—Zn product is a thin aircraft member and wherein the reheated product is hot-rolled and then the hot-rolled product is cold rolled 10 to 20% to the final gauge.
21. Method according to claim 1 , wherein the Al—Zn product is an upper-wing member of an aircraft.
22. Method according to claim 1 , wherein the Al—Zn product is a thin skin member of an upper-wing or of a stringer of an aircraft.
23. Method according to claim 1 , wherein Al—Zn product is stringer of an aircraft.
24. Method according to claim 1 , wherein the ingot consists essentially of the following composition, in weight percent:
Zn 6.0 to 11.0%
Cu 1.4 to 2.2%
Mg 1.4 to 2.4%
Zr 0.05 to 0.15%
Ti <0.05%
Hf and/or V <0.25%
optionally Sc and/or Ce 0.05 to 0.25%,
optionally Mn 0.05 to 0.12%, and
inevitable impurities and balance aluminium.
25. Method according to claim 1 , wherein the method performed from step (b) through (e) consists essentially of steps (b), (c), (d) and (e).
26. Method according to claim 1 , wherein the method performed from step (b) through (e) consists of steps (b), (c), (d) and (e).
27. Method according to claim 26 , wherein the reheated product is hot rolled to about 105 to 140 (in final-gauge %) and then the hot rolled product is cold rolled to the final gauge.
28. Method according to claim 26 , wherein the reheated product is hot rolled and then the hot rolled product is cold rolled 10 to 20% to the final gauge and the quenched alloy product is stretched 1.5 to 2.0% after quenching,
wherein the amount of Cu is in a range of 1.7 to 2.2 wt. %, the amount of Mg is in a range of 1.7 to 2.2 wt. %, the amount of Zn is in a range of 8.0 to 8.7 wt. %.
29. Method according to claim 1 , wherein the amount of Cu is in a range of 1.7 to 2.2 wt. %, wherein the amount of Mg is in a range of 1.7 to 2.2 wt. %, wherein the amount of Zn is in a range of 8.0 to 8.7 wt. %.
30. Method according to claim 1 , wherein the ingot consists of the following composition, in weight percent:
Zn 6.0 to 11.0%
Cu 1.4 to 2.2%
Mg 1.4 to 2.4%
Zr 0.05 to 0.15%
Ti <0.05%
Hf and/or V <0.25%
optionally Sc and/or Ce 0.05 to 0.25%,
optionally Mn 0.05 to 0.12%, and
inevitable impurities and balance aluminium.
31. Method according to claim 30 ,
wherein the method performed from step (b) through (e) consists of steps (b), (c), (d) and (e),
wherein the reheated product is hot rolled and then the hot rolled product is cold rolled 10 to 20% to the final gauge and the quenched alloy product is stretched 1.5 to 2.0% after quenching, wherein the final gauge is in the range of 4 to 50 mm, wherein the amount of Cu is in a range of 1.7 to 2.2 wt. %, the amount of Mg is in a range of 1.7 to 2.2 wt. %, the amount of Zn is in a range of 8.0 to 8.7 wt. %, wherein the artificial ageing during step g) consists of a first ageing step at a temperature around 155° C. to 160° C. for 4 to 12 hours to a temper selected from T79 and T76 temper.
32. Method according to claim 31 , wherein the ingot includes, in weight percent, 0.06 to 0.25% Sc.