Process for manufacturing a bimetallic part using a dilation-causing thermal treatment

Patent metadata

Field	Value
Publication number	US-12247264-B2
Application number	US-201916973111-A
Country	US
Kind code	B2
Filing date	Jun 27, 2019
Priority date	Jul 3, 2018
Publication date	Mar 11, 2025
Grant date	Mar 11, 2025

Abstract

A process for manufacturing a bimetallic part by means of a first component formed by a first aluminum alloy and a second component formed by a second aluminum alloy, said process involving: assembling the first component and the second component to obtain an assembled part; applying a thermal treatment to the assembled part at a temperature of 100 to 250° C., the thermal treatment causing the assembled part to deform, in particular as a result of a metallurgical deformation by a precipitation of hardening phases of the first component and/or the second component; cooling the part to ambient temperature, upon which the part remains deformed. The process involves, prior to the assembling step, an estimation of the degree of deformation that the assembled part will undergo under the effect of the thermal treatment.

First claim

The invention claimed is:

1. A method for manufacturing a bimetallic part, comprising:
providing a first component formed by a first aluminium alloy and a second component formed by a second aluminium alloy, the first and second aluminium alloys being different from each other, the first component and the second component extending: along a longitudinal axis, over a length greater than five meters; and along a lateral axis perpendicular to the longitudinal axis, over a width greater than one tenth of the length;
carrying out the following steps:
a) determining a reference form corresponding to a form that is desired at the end of manufacture;
b) estimating the deformation of the assembled part induced by the heat treatment by digital modelling;
c) defining an initial form of the first component and an initial form of a second component, taking into account the reference form determined during step a) and the induced deformation estimated during step b), so that, at the end of the heat treatment, the part extends in the reference form; and
d) obtaining the first component and the second component according to the respective initial forms thereof defined during step c);
assembling the first component against the second component along the longitudinal axis to obtain an assembled part;
applying a heat treatment to the assembled part, at a temperature of between 100° C. and 250° C., the heat treatment causing an induced deformation of the assembled part, under the effect of a change in metallurgical nature in at least one of the first aluminium alloy and the second aluminium alloy;
cooling to ambient temperature, after which, said induced deformation remains.

2. The method according to claim 1 , wherein the heat treatment is an ageing, the change in metallurgical nature being a recrystallisation or a solution heat treatment or a precipitation of alloy elements.

3. The method according to claim 1 , wherein the assembling is carried out by welding.

4. The method according to claim 1 , wherein, in step b), the deformation caused by the assembled part is estimated by digital modelling.

5. The method according to claim 4 , wherein step b) includes the following steps:
bi) allocating a first virtual thermal expansion coefficient to the first alloy and a second virtual thermal expansion coefficient to the second alloy, and defining a virtual temperature change over time;
bii) taking into account the first and second virtual thermal expansion coefficients and the auxiliary virtual temperature change over time, and modelling the deformation of the assembled part during the heat treatment.

6. The method according to claim 5 , wherein the virtual temperature change defined in step bi) is different from a temperature variation to which the assembled part is subjected during the heat treatment.

7. The method according to claim 6 , wherein the virtual temperature change defined in step bi) extends between a minimum temperature and a maximum temperature, the amplitude between the minimum temperature and the maximum temperature being different from the temperature variation to which the assembled part is subjected during the heat treatment.

8. The method according to claim 5 , wherein, in step bi), the first virtual thermal expansion coefficient, the second virtual thermal expansion coefficient, and the virtual temperature change, are defined experimentally by:
applying the heat treatment to a test piece, representative of the assembled part, in order to obtain an induced deformed test piece;
digitally modelling the test piece, in order to obtain a modelled deformation, the modelling taking into account the first virtual thermal expansion coefficient, the second virtual thermal expansion coefficient, and the virtual temperature change;
adjusting the first virtual thermal expansion coefficient, the second virtual thermal expansion coefficient, and the virtual temperature change so that the modelled deformation corresponds to the deformation of the test piece.

9. The method according to claim 5 , wherein, in substep bi), the first virtual thermal expansion coefficient, the second virtual thermal expansion coefficient, and the virtual temperature change are defined experimentally from a measurement, by dilatometry, on specimens, each specimen being respectively representative of the first component and the second component.

10. The method according to claim 4 , wherein, in step b), the modelling takes into account the respective Young's moduli of the first alloy and the second alloy.

11. The method according to claim 5 , wherein the first alloy is an aluminium alloy of the type 2XXX, and the second alloy is an aluminium alloy of the type 7XXX.

12. The method according to claim 11 , wherein the heat treatment is an ageing, and wherein the first virtual thermal expansion coefficient is strictly greater than the second virtual thermal expansion coefficient.

13. The method according to claim 1 , wherein the assembly is carried out by welding, the heat treatment being an ageing.

14. The method according to claim 13 , also including a step b′) of estimating an expansion of at least one of the first component and of the second component during the welding, in order to define an intermediate form of the assembled part, between the welding and the ageing, so that, in step c), in defining the initial form of the first component and the second component, account is taken of the reference form and the intermediate form of the assembled part.

15. The method according to claim 14 , wherein step b′) is carried out by digital modelling.

16. The method according to claim 15 , wherein step b′) includes the following steps:
allocating a first auxiliary virtual thermal expansion coefficient to the first alloy and a second auxiliary virtual thermal expansion coefficient to the second alloy and defining an auxiliary virtual temperature change over time;
taking into account the first and second auxiliary virtual thermal expansion coefficients and the auxiliary virtual temperature change over time, and modelling the deformation of the part during welding.

Assignees

• Constellium Issoire

Inventors

• Ehrstrom Jean-Christophe
• Laye Julien
• Arsene Sylvie
• Warner Timothy

Classifications

• B23K20/2336

  both layers being aluminium · CPC title

• G16C60/00

  Computational materials science, i.e. ICT specially adapted for investigating the physical or chemical properties of materials or phenomena associated with their design, synthesis, processing, characterisation or utilisation · CPC title

• B23K2101/006

  Vehicles · CPC title

• B23K2103/10

  Aluminium or alloys thereof · CPC title

• B23K2101/28

  Beams · CPC title