Method for producing a vehicle component, and vehicle component
Method for producing a vehicle component, in particular a motor vehicle component, in particular a B-pillar, including providing a first aluminum alloy and a second aluminum alloy. The second alloy composition substantially matches the first aluminum alloy composition. Performing a heat-treatment of the first alloy to increase the ductility of the first alloy. Performing a heat-treatment of the second alloy. The heat-treatment of the first alloy differing from the heat-treatment of the second alloy. Welding together the heat-treated first alloy and the heat-treated second alloy to obtain a composite part. Shaping the composite parts into a motor vehicle component. The motor vehicle component sub-region of the first alloy can be designed as a predetermined deformation region when a force is applied due to an accident to achieve a good combination of rigid regions for example forming a safety cell, and deformable regions forming a crumple zone for absorbing energy.
1. A method for producing a motor vehicle component, wherein the motor vehicle component is a B-pillar, comprising the following steps:
a) providing a first aluminum alloy;
b) performing a heat-treatment of the first aluminum alloy to increase the ductility of the first aluminum alloy;
c) providing a second aluminum alloy;
d) performing a heat-treatment of the second aluminum alloy, the heat-treatment of the first aluminum alloy differing from the heat-treatment of the second aluminum alloy;
e) welding together the heat-treated first aluminum alloy and the heat-treated second aluminum alloy, to obtain a composite part;
f) shaping the composite part into the motor vehicle component, wherein the B-pillar has deformable regions in combination with rigid regions; and
g) cathodic dip coating and/or coating cycle of the B-pillar;
wherein the first aluminum alloy and second aluminum alloy are each a metal sheet having a thickness range between 0.5 to 3.5 mm;
wherein the region of the B-pillar made of the first aluminum alloy is designed as a predetermined deformation region for deforming when force is applied due to an accident; and
wherein the region of the B-pillar made of the second aluminum alloy is designed to have higher rigidness than the region of the B-pillar made of the first aluminum alloy.
2. The method according to claim 1 , wherein each of the first aluminum alloy and the second aluminum alloy independently of each other, in % by weight, have the following chemical composition:
Zn: 6.9-8.4
Mg: 1.2-2.4
Cu: 1.3-2.6
Mn: <0.3
Cr or Zr: 0.05-0.25
Si: <0.3
Fe: <0.35
Ti: <0.1
other elements: <0.05 each, <0.2 in total
balance: aluminum.
3. The method according to claim 2 , wherein the heat treatment of the first aluminum alloy results in a T6 degree of hardness and the heat treatment of the second aluminum alloy results in a T6 degree of hardness.
4. The method according to claim 3 , wherein the heat treatment of the second aluminum alloy is not for increase in ductility but for increase of strength.
5. The method according to claim 2 , wherein each of the first aluminum alloy and the second aluminum alloy contains 0.05-0.25% by weight, of zirconium.
6. The method according to claim 2 , wherein each of the first aluminum alloy and the second aluminum alloy contains 0.07-0.18% by weight, of zirconium.
7. The method according to claim 2 , wherein each of the first aluminum alloy and the second aluminum alloy contains 1.4-1.8% by weight, of copper.
8. The method according to claim 1 , wherein the composition of the second aluminum alloy differs by maximally 0.5% by weight in regard to each of its elemental components from composition of the first aluminum alloy.
9. The method according to claim 8 , wherein each of the first aluminum alloy and the second aluminum alloy independently of each other, in % by weight, have the following chemical composition:
Zn: 6.9-7.8
Mg: 1.4-2.1
Cu: 1.3-2.6
Mn: <0.3
Cr or Zr: 0.05-0.25
Si: 0.1-0.25
Fe: 0.1-0.25
Ti: <0.1
other elements: <0.05 each, <0.2 in total
balance: aluminum.
10. The method according to claim 9 , wherein the heat treatment of the first aluminum alloy results in a T73 heat treatment and the heat treatment of the second aluminum alloy is a T74, T76, T77, T78 or T79 heat treatment.
11. The method according to claim 9 , wherein the heat treatment of the first aluminum alloy results in a T73 heat treatment and the heat treatment of the second aluminum alloy is a T76 heat treatment.
12. The method according to claim 8 , wherein each of the first aluminum alloy and the second aluminum alloy independently of each other, in % by weight, have the following chemical composition:
Zn: 6.9-8.4
Mg: 1.2-2.4
Cu: 1.3-2.6
Mn: <0.3
Cr or Zr: 0.05-0.25
Si: <0.3
Fe: <0.35
Ti: <0.1
other elements: <0.05 each, <0.2 in total
balance: aluminum.
13. The method according to claim 1 , wherein each of the first aluminum alloy and the second aluminum alloy is an AA 7xxx class aluminum alloy.
14. The method according to claim 13 , wherein each of the first aluminum alloy and the second aluminum alloy is an aluminum alloy selected from the group consisting of AA 7055, AA7081, AA 7181, AA 7085, and AA 7185class alloys.
15. The method according to claim 1 , wherein each of the first aluminum alloy and the second aluminum alloy independently of each other, in % by weight, have the following chemical composition:
Zn: 6.9- 7.8
Mg: 1.4-2.1
Cu: 1.3-2.6
Mn: <0.3
Cr or Zr: 0.05-0.25
Si: 0.1-0.25
Fe: 0.1-0.25
Ti: <0.1
other elements: <0.05 each, <0.2 in total
balance: aluminum.
16. The method according to claim 15 , wherein each of the first aluminum alloy and the second aluminum alloy contains 0.07-0.18% by weight, of zirconium.
17. The method according to claim 1 , wherein welding together the two aluminum alloys is done by way of friction stir welding or laser beam welding.
18. The method according to claim 1 , wherein the shaping is W-temper shaping.