Aluminum composite material and forming method

Patent metadata

Field	Value
Publication number	US-10279385-B2
Application number	US-201715821528-A
Country	US
Kind code	B2
Filing date	Nov 22, 2017
Priority date	Oct 30, 2012
Publication date	May 7, 2019
Grant date	May 7, 2019

Abstract

The invention relates to a method for forming an aluminium composite material which has a core alloy made from an aluminium alloy of type AA5xxx or AA6xxx and at least one outer aluminium alloy layer provided on one or both sides, wherein the aluminium composite material is formed and the outer aluminium alloy layer provided on one or both sides has a yield strength Rp0.2 of 25 MPa to 60 MPa in the soft or solution-annealed state. The method enables the production of large-surface, heavily formed aluminium alloy sheet metal parts, in particular also in outer skin quality.

First claim

The invention claimed is:

1. Sheet metal part manufactured by forming an aluminium composite material which has a core alloy made from an aluminium alloy of type AA5xxx or AA6xxx and at least one outer aluminium alloy layer provided on one or both sides, wherein the aluminium composite material is formed in a forming tool and the outer aluminium alloy layer provided on one or both sides has a yield strength R p0.2 of 25 MPa to 60 MPa in the soft or solution-annealed state, characterised in that,
k f,outside /k f,core <0.5
for the flow stresses of the aluminium alloys of the core and of the at least one outer layer in the soft or solution-annealed state, the frictional shear stress τ R between the tool and the aluminium composite material in the contact surface reaches the shear flow stress k outside of the outer aluminium alloy layer at at least one local position in the forming tool during the formation of the aluminium composite material.

2. Sheet metal part according to claim 1 , characterised in that, the forming comprises a deep drawing or stretch forming procedure.

3. Sheet metal part according to claim 1 , characterised in that, at least one outer aluminium alloy layer having a thickness of 5% to 15% of the total aluminium composite material is formed.

4. Sheet metal part according to claim 1 , characterised in that, the frictional shear stress τ R is enlarged during the formation by an increase of the surface pressure between the aluminium composite material and the hold-down clamp.

5. Sheet metal part according to claim 1 , characterised in that, an aluminium core alloy of type AA6xxx or AA5xxx is formed which has a uniform strain A g of at least 20% in the solution-annealed or soft state.

6. Sheet metal part according to claim 1 , characterised in that, an alloy of type AA6xxx is used as an aluminium core alloy and an aluminium alloy of type AA8xxx is used as at least one outer aluminium alloy layer or an alloy of type AA5xxx is used as an aluminium core alloy and an aluminium alloy of type AA8xxx, AA1xxx, AA5005, AA5005A is used as at least one outer aluminium alloy layer.

7. Sheet metal part according to claim 6 , characterised in that, an aluminium core alloy of type AA6016 and at least one outer aluminium alloy layer of type AA8079 is used.

8. Sheet metal part according to claim 1 , characterised in that, an aluminium core alloy of type AlMg6 and at least one outer aluminium alloy layer of type AA8079, AA1050 or AA5005 or AA5005A is used.

9. Sheet metal part according to claim 1 , characterised in that, an aluminium composite material having an AA6xxx aluminium core alloy having a thickness of 0.5 mm to 2.0 mm or an aluminium composite material having an AA5xxx aluminium core alloy having a thickness of 0.5 mm to 3.5 mm is formed.

10. Sheet metal part according to claim 1 , characterised in that, the sheet metal part is a structural part or an outer skin part of a motor vehicle.

11. A deep drawn or stretch formed structural part or outer skin part of a motor vehicle formed with a method for forming an aluminium composite material which has a core alloy made from an aluminium alloy of type AA5xxx or AA6xxx and at least one outer aluminium alloy layer provided on one or both sides, the method comprising forming the aluminium composite material in a forming tool wherein the outer aluminium alloy layer provided on one or both sides has a yield strength R p0.2 of 25 MPa to 60 MPa in the soft or solution-annealed state, wherein,
k f,outside /k f,core <0.5
applies for the flow stresses of the aluminium alloys of the core and of the at least one outer layer in the soft or solution-annealed state, the frictional shear stress τ R between the tool and the aluminium composite material in the contact surface reaches the shear flow stress k outside of the outer aluminium alloy layer at at least one local position in the forming tool during the formation of the aluminium composite material and the formation comprises a deep drawing and/or stretch forming procedure and wherein an alloy of type AA6xxx is used as an aluminium core alloy and an aluminium alloy of type AA8xxx is used as at least one outer aluminium alloy layer or an alloy of type AlMg6 is used as an aluminium core alloy and an aluminium alloy of type AA8079, AA1050, AA5005, AA5005A is used as at least one outer aluminium alloy layer.

Assignees

• Brinkman Henk Jan
• Keller Stefan
• Engler Olaf
• Hoerster Natalie
• Schroeder Dietmar
• Aretz Holger
• Hydro Aluminium Rolled Prod

Inventors

• Brinkman Henk-Jan
• Keller Stefan
• Engler Olaf
• Hörster Natalie
• Schröder Dietmar
• Aretz Holger

Classifications

• C22C21/00

  Alloys based on aluminium · CPC title

• B21D22/208 Primary

  by heating the blank or deep-drawing associated with heat treatment (C21D takes precedence) · CPC title

• B21D22/203

  of compound articles · CPC title

• B32B15/011 Primary

  all layers being formed of iron alloys or steels · CPC title

• B32B15/016

  all layers being formed of aluminium or aluminium alloys · CPC title