Aluminum-alloy clad material and method of manufacturing the same
An aluminum-alloy clad material includes a skin layer clad to and covering at least one surface of a core layer. The core layer is composed of an aluminum alloy containing Cu: 3.8-4.9 mass %, Mg: 1.2-1.8 mass % and Mn: 0.3-0.9 mass %. The core layer has an area number density of microvoids that have a circle-equivalent diameter of 0.5 μm or greater that is 100/mm 2 or less. The skin layer has an Al purity of 99.5 mass % or greater. A method of manufacturing a wrought material from such an aluminum-alloy clad material includes heating the wrought material to the solution heat treatment temperature of the core layer at a temperature-rise rate of 50° C.-200° C./h.
1. An aluminum-alloy clad material comprising:
a skin layer clad to and covering at least one surface of a core layer,
wherein the core layer is composed of an aluminum alloy containing Cu: 3.8-4.9 mass %, Mg: 1.2-1.8 mass % and Mn: 0.3-0.9 mass %,
the core layer has an area number density of microvoids that have a circle-equivalent diameter of 0.5 μm or greater that is 100/mm 2 or less, and
the skin layer has an Al purity of 99.5 mass % or greater.
2. The aluminum-alloy clad material according to claim 1 , wherein the core layer further contains Si: 0.020-0.20 mass % and Fe: 0.020-0.20 mass %.
3. The aluminum-alloy clad material according to claim 2 , wherein the core layer contains Mn: 0.42-0.57 mass %.
4. The aluminum-alloy clad material according to claim 3 , wherein the core layer further contains Cr: 0.02-0.06 mass %.
5. The aluminum-alloy clad material according to claim 4 , wherein the core layer further contains Zn: 0.04-0.20 mass %.
6. The aluminum-alloy clad material according to claim 5 , wherein the core layer further contains Ti: 0.01-0.15 mass %.
7. The aluminum-alloy clad material according to claim 1 , wherein the core layer consists of Cu: 3.8-4.9 mass %, Mg: 1.2-1.8 mass %, Fe: 0.020-0.20 mass %, Si: 0.020-0.20 mass %, Mn: 0.42-0.57 mass %, Cr: 0.02-0.06 mass %, Zn: 0.04-0.20 mass %, and Ti: 0.01-0.15 mass %, the remainder being Al and unavoidable impurities.
8. The aluminum-alloy clad material according to claim 7 , wherein the area number density of microvoids that have a circle-equivalent diameter of 0.5 μm or greater that is 65/mm 2 or less.
9. The aluminum-alloy clad material according to claim 1 , produced by a process comprising:
preparing an ingot of the core layer;
preparing an ingot of the skin layer;
clad bonding the ingot of the core layer to the ingot of the skin layer to form a laminated material;
subjecting the laminated material to a homogenization treatment by heating the laminated material at a temperature of 495° C.−500° C. for 1 h or more;
hot working the laminated material to form a wrought material; and
subjecting the wrought material to a solution heat treatment by heating the wrought material to a solution heat treatment temperature of the core material or higher with the proviso that, after the wrought material reaches 100° C. until the wrought material reaches the solution heat treatment temperature of the core material, the wrought material is heated at a temperature-rise rate of 50° C.−200° C./h, whereby the aluminum-alloy clad material according to claim 1 is formed.
10. The aluminum-alloy clad material according to claim 9 , wherein prior to performing the solution heat treatment, the ingot of the core layer contains less than 0.2 ml of hydrogen per 100 g of the core layer.
11. The aluminum-alloy clad material according to claim 10 , wherein the solution heat treatment temperature is 480° C.−490° C.
12. The aluminum-alloy clad material according to claim 11 , wherein the solution heat treatment time is 30-120 minutes.
13. The aluminum-alloy clad material according to claim 12 , wherein the temperature-rise rate during the solution heat treatment is 130° C.−185° C./h.
14. The aluminum-alloy clad material according to claim 13 , wherein prior to performing the solution heat treatment, the ingot of the core layer contains 0.09-0.16 ml of hydrogen per 100 g of the core layer.
15. The aluminum-alloy clad material according to claim 14 , wherein the core layer further contains Fe: 0.020-0.20 mass % and Si: 0.020-0.20 mass %.
16. The aluminum-alloy clad material according to claim 15 , wherein the core layer contains Mn: 0.42-0.57 mass %, and further contains Cr: 0.02-0.06 mass %, Zn: 0.04-0.20 mass % and Ti: 0.01-0.15 mass %.
17. The aluminum-alloy clad material according to claim 14 , wherein the core layer consists of Cu: 3.8-4.9 mass %, Mg: 1.2-1.8 mass %, Fe: 0.020-0.20 mass %, Si: 0.020-0.20 mass %, Mn: 0.42-0.57 mass %, Cr: 0.02-0.06 mass %, Zn: 0.04-0.20 mass %, and Ti: 0.01-0.15 mass %, the remainder being Al and unavoidable impurities.
18. An aluminum-alloy clad material comprising:
a skin layer clad to and covering at least one surface of a core layer,
wherein the core layer is composed of an aluminum alloy containing Cu: 3.8-4.9 mass % and Mg: 1.2-1.8 mass %,
the core layer has an area number density of microvoids that have a circle-equivalent diameter of 0.5 μm or greater that is 100/mm 2 or less, and
the skin layer has an Al purity of 99.5 mass % or greater.
19. The aluminum-alloy clad material according to claim 18 , wherein the core layer further contains Mn: 0.3-0.9 mass %, Cr: 0.1 mass % or less and Zn: 0.3 mass % or less.
20. The aluminum-alloy clad material according to claim 18 , produced by a process comprising:
preparing an ingot of the core layer;
preparing an ingot of the skin layer;
clad bonding the ingot of the core layer to the ingot of the skin layer to form a laminated material;
subjecting the laminated material to a homogenization treatment by heating the laminated material at a temperature of 495° C.−500° C. for 1 h or more;
hot working the laminated material to form a wrought material; and
subjecting the wrought material to a solution heat treatment by heating the wrought material to a solution heat treatment temperature of the core material or higher with the proviso that, after the wrought material reaches 100° C. until the wrought material reaches the solution heat treatment temperature of the core material, the wrought material is heated at a temperature-rise rate of 50° C.−200° C./h, whereby the aluminum-alloy clad material according to claim 18 is formed.