Method for Welding at Least Two Layers

FIELD OF THE INVENTION

The invention relates to a method for welding at least two layers together over at least a first joint surface.

DESCRIPTION OF PRIOR ART

In 1991, the welding institute developed a technique known as Friction Stir Welding (FSW) for joining metallic alloys that are difficult to weld by conventional fusion welding. A rotating tool with a pin is translated along a butt joint between two clamped pieces that need to be joined. The rotating pin penetrates the two pieces causing the stirred materials (typically metallic materials) to soften without melting. This process involves dynamic recrystallization of the base materials. FSW is a solid-state joining process: the two materials of the two pieces to join are not melted during the process.

Friction Stir Lap Welding (FSLW) is an application of FSW when one aims at joining at least two layers that are typically metallic layers (see for instance R. S. Mishra et al. in Mater. Sci. Eng. R 50 (2005), 1-78). As for FSW, a rotating tool with a pin is used in this technique for mechanically mixing the materials of the different layers. Hence, FSLW is also a solid-state joining technique. As reported in Metall. Mater. Trans. A Vol 42, Issue 9, pp. 2850-2861 by Zhang Guifeng et al., FSLW presents several drawbacks such as inducing voids along the interfaces between the different layers that are joined. The pin of the rotating tool that must penetrate the different layers to allow a mechanical mixing between the different layers is also substantially damaged during the process. One could use a rotating tool without a pin to prevent wear of the pin but then the mechanical mixing between the different layers would be poor, resulting in very poor joint strength.

Therefore, Zhang Guifeng et al. have proposed, in Metall. Mater. Trans. A Vol 42, Issue 9, pp. 2850-2861, a process named Friction Stir Brazing (FSB). In this process, a rotating tool without pin is used and translated on the upper surface of a top layer. A braze layer is placed in between two layers to join. Zn foils are typically chosen as braze layers because of the low melting point of Zn. In Zhang Guifeng et al.'s publication, a Zn foil is used for joining an aluminium (Al) layer to a steel layer. The Al layer is the top layer meaning that the rotating tool is translated over the upper surface of the Al layer. When the rotating tool (without pin) is pressed and translated over the upper surface of the top layer, heat is generated below the rotating tool by friction. This heat induces melting of the Zn foil allowing joining the two layers (of Al and steel in this particular case). The thickness of the Zn foil must be small (typically around 0.1 mm) in order to have a complete melting of the Zn foil all along its whole thickness. As shown and explained in Zhang Guifeng et al.'s publication (for instance in FIG. 3, and in paragraphs III.A, D), a large amount of Zn is squeezed out by the rotating tool when it is translated over the upper surface of the top layer to induce the melting of the Zn foil.

FSB requires the presence of a braze layer between the two layers to join. This braze layer is typically a Zn layer. This leads to different drawbacks. First, the cost is increased as an additional material is needed. Second, the presence of the braze layer can induce contamination to the two layers to join, especially when a heat treatment is after applied to the multilayer structure.

WO2010/067796A1 describes a method for joining a thermoplastic polymeric layer with a metal layer. These two members are overlapped, and a rotating friction stir tool is pressed from the metal member side and the two members are joined by the heat of friction: after the polymer is melted by the heat of friction, the resin fuses to the metal member along a joint surface as the temperature drops, thus forming an interfacial joint. The joining method of WO2010/067796A1 presents several drawbacks. At the interfacial joint surface between the two layers, the properties along the thickness of the two layers (such as thermal conductivity, electrical resistance) present a sharp discontinuity at the level of the interface. In many applications, such a discontinuity in the properties of the set is not desirable as it leads to poor global performances across the thickness. Furthermore, the clear interface between the two layers induces weak mechanical resistance of the joint between the two layers.

SUMMARY OF THE INVENTION

It is an object of the present invention to provide a method for joining at least two layers yielding an improved continuity at the joint surface between the two layers. To this end, the inventors propose the following method.

Method for welding at least two layers together over at least a first joint surface and comprising the steps of:

- (a) providing a first layer of a first material having a first melting temperature, T_m,1, said first layer having an upper surface and a lower surface separated by the thickness t₁of the first layer;
- (b) providing a second layer of a second material having a second melting temperature, T_m,2, lower than the first melting temperature, T_m,1, said second layer having an upper surface and a lower surface separated by the thickness t₂of the second layer;
- (c) forming a layup by stacking the first and second layers such that the lower surface of the first layer contacts and at least partially overlaps the upper surface of the second layer forming an interface;
- (d) pressing and translating over at least one friction portion of the upper surface of the first layer, wherein the portion of the interface which is in registry with the friction portion defines the first joint surface, a rotating tool to raise the temperature of said at least one friction portion of the upper surface of the first layer by friction and to conduct heat through the thickness t₁of the first layer to the second layer such that the temperature reached by at least a portion of the upper surface of the second layer that is comprised in said first joint surface is higher than the second melting temperature T_m,2;
- (e) providing restraining means for preventing molten second material from flowing out of the layup.
  
  The method of the invention is characterized in that said first and second materials of said first and second layers are chosen among the following materials: metals, semi-metals or semiconductors.

The terms metals, semi-metals and semiconductors are known by the one skilled in the art and can be defined according to electronic band theory.

A metal has an electron band structure that is characterized by a partially filled conduction band, CB, and that has a large density of states at the Fermi level.

A semi-metal has an electron band structure that is characterized by a small overlap between the bottom of the conduction band, CB, and the top of the valence band, VB. A semi-metal has no band gap, E_g, and a negligible density of states at the Fermi level. In a semi-metal, the bottom of the conduction band, CB, is generally situated in a different part of momentum space (different k-vector) that the top of the valence band, VB. Semi-metals have charge carriers of both types: holes and electrons.

A semi-conductor has a filled valence band, VB, at 0 K that is separated from an empty conduction band, CB, by a relatively narrow band gap E_g: E_gis smaller than 4 eV in general.

As first and second materials are chosen among metals, semi-metals, or semiconductors, an inter-phase is formed between first and second layers upon joining them with a method according to the present invention. The inter-phase results from the reaction that takes place between the first layer that remains solid and the second layer that is melted at least along a portion of the upper surface of the second layer: atoms or molecules of the first layer diffuse into the liquid phase of the second layer, forming a ‘chemical’ inter-phase when temperature decreases. Concurrently or alternatively, crystals may grow from one layer across the interface and penetrate into the second layer, thus forming a ‘physical’ inter-phase. Alternatively, atoms or molecules of both first and second layers diffuse to the other layer forming an inter-phase. Such an inter-phase can therefore have a chemical composition different from first and second layers and/or a different physical configuration from these two layers. So, contrary to the set obtained with the method of WO2010/067796A1 (that comprises only two phases), a set with three different zones is obtained at the end of the method of the invention: one zone corresponds to the phase of the first layer, one zone corresponds to the phase of the second layer, and one zone corresponds to the inter-phase. Preferably, these three different zones are three different phases. This inter-phase allows obtaining a gradient in the properties of the set instead of a sharp discontinuity as obtained with an interfacial joint. A gradient in the chemical composition can also be obtained. Finally, an improved continuity at the first joint surface between the two layers is obtained resulting in improved global performances of the set. In particular, the mechanical resistance of the first joint surface is higher thanks to the presence of the inter-phase between first and second layers.

In the method of the invention, no braze layer is used to join the first and second layers. Thanks to the heat generated by the rotating tool, the second layer melts allowing welding it to the first layer. As the method of the invention uses retraining means for preventing molten second material from flowing out of the layup, the presence of said second material is maintained at the end of the joining process (or method of the invention). If restraining means were not used, a large amount of second material of second layer would be squeezed out during the joining process as it is the case for the Zn layer in FSB. The use of restraining means also allows having a high control of the thickness of the different layers.

The method of the invention has other advantages. Contrary to FSW or FSLW, the method of the invention does not require the rotating tool to penetrate up to the second layer. The only requirement is that heat generated by friction below the rotating tool is transmitted by conduction through the thickness t₁of the first layer to the second layer. Hence, less sophisticated rotating tools can be used for the method of the invention compared to FSW or FSLW. As the rotating tool can be simpler in the method of the invention, this technique is cheaper than FSW or FSLW. The method of the invention is also less destructive for the rotating tool compared to FSW or FSLW as the rotating tool does not have to penetrate the whole thickness t₁of the first layer.

Preferably, the restraining means comprise a cavity with side walls into which said layup is snugly placed. In this preferred embodiment, the side walls of the cavity into which the layup (of stack) is placed prevent molten second material from flowing out of the layup (of stack).

Preferably, the restraining means prevent the rotating tool from reaching a fringe extending along at least a portion of the perimeter of the upper surface of the first layer. In this preferred embodiment, the rotating tool is not pressed and translated over a fringe running around at least a portion of the perimeter of the first upper surface. This induces that the second layer is not melted in a whole plane perpendicular to the thickness t₂. The non melted parts of the second layer restrain molten second material from flowing out of the layup. More preferably, the rotating tool is not pressed and translated over the whole perimeter of the first upper surface.

Preferably, the restraining means comprise a solid lower surface of the second layer. In this preferred embodiment, the second layer is not melted along its whole thickness t₂as the temperature reached by the second lower surface of the second layer is lower than the second melting temperature, T_m,2. Such a situation is different from what takes place in FSB. Hence, molten second material does not flow out of the layup in this preferred embodiment as the non melted part of the second layer prevent it.

Preferably, at least one of said first and second materials of first and second layers is a metal. Then, an intermetallic layer is preferably formed between first and second layers.

Preferably, the at least two layers are metal layers. More preferably, the first material is steel and the second material is aluminium. Hence, contrary to FSB disclosed in Guifeng Zhang et al.'s publication, the first layer over which the rotation tool is pressed and translated comprises steel rather than aluminum in this preferred embodiment.

Preferably, the ratio between the first and second melting temperatures, T_m,1/T_m,2is higher than 1.2. Preferably, the thickness t₁of the first layer and the thickness t₂of the second layer are comprised between 0.3 mm and 2 mm. Preferably, the rotating tool is made of a material comprising cemented carbide. Preferably, the rotating tool has a cylindrical shape with an external diameter comprised between 10 mm and 20 mm. Preferably, the rotating tool is translated over said at least one friction portion of the upper surface of the first layer with a speed that is comprised between 50 mm/min and 1000 mm/min. More preferably, the rotating tool is translated over said at least one friction portion of the upper surface of the first layer with a speed that is comprised between 100 mm/min and 500 mm/min. Preferably, the rotating tool has a speed of rotation comprised between 1000 and 3000 revolutions per minute.

Preferably:

- the method of the invention further comprises between steps (b) and (c) the step of providing a third layer of a third material having a third melting temperature, T_m,3, higher than the second melting temperature, T_m,2, of the second layer, said third layer having an upper surface and a lower surface; wherein in step (c):
- the layup further comprises said third layer such that the upper surface of the third layer contacts and at least covers the portion of the lower surface of the second layer which is in registry with the first joint surface; and wherein in step (d):
- the rotating tool raises the temperature of the lower surface of the second layer to a value higher than the second melting temperature T_m,2thereof.
  
  This preferred version of the method of the invention allows welding more than two layers. In this case, at least a portion of the second layer melts over its whole thickness t₂. In this preferred embodiment, the restraining means preferably comprise the third layer that remains solid.

Preferably, the third material is vanadium. Preferably, the third material is steel.

SHORT DESCRIPTION OF THE DRAWINGS

These and further aspects of the invention will be explained in greater details by way of examples and with reference to the accompanying drawings in which:

FIG. 1 schematically shows a layup of two layers with a rotating tool that is pressed and translated over the upper surface of the first layer;

FIG. 2 schematically shows examples of profiles of temperature that are induced along the thicknesses of the two layers of FIG. 1 and under the rotating tool when it is pressed on the upper surface of the first layer;

FIG. 3 shows an example of configuration where the first layer does not overlap the whole second layer;

FIG. 4 schematically shows how the rotating tool can be positioned with respect to the upper surface of the first layer;

FIG. 5 schematically shows a cavity with side walls into which a layup comprising at least two layers is snugly placed;

FIG. 6 schematically shows the upper surface of the first layer that is covered by a mask;

FIG. 7 schematically shows a layup of two layers when the lower surface of the second layer is solid;

FIG. 8 shows images of microstructures of two layers that are welded according to the method of the invention;

FIG. 9 shows images of microstructures of two layers that are welded according to the method of the invention;

FIG. 10 schematically shows a layup of three layers;

FIG. 11 shows images of microstructures of three layers that are welded according to the method of the invention.

The figures are not drawn to scale. Generally, identical components are denoted by the same reference numerals in the figures.

DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS

The method of the invention is a welding method for joining at least two layers of two different materials. Hence, it is neither a brazing method nor a soldering method. Generally, the one skilled in the art names as soldering methods techniques for joining at least two layers (that can comprise a same material or not) by melting and flowing a filler metal or a solder into the interface between the two layers. The filler metal or solder has a lower melting temperature than the two layers to join. Hence, soldering appears to be a hot glue process where the filler metal or solder, when it is cooled, allows obtaining a solid junction between the two layers. Brazing technique is a particular case of soldering and typically corresponds to a soldering method requiring a relatively high temperature to melt the solder allowing obtaining strong joints between the two layers to joint. An example of braze material is Zn that melts at around 420° C. in atmospheric pressure.

FIG. 1 schematically shows, along a two-dimensional view, how the method of the invention is carried out. First, at least two layers to weld are provided. In the case of FIG. 1, it is assumed that a first 20 and a second 30 layers are to be joined or welded. The first layer 20 (respectively second layer 30) comprises a first (respectively second) material having a first (respectively second) melting temperature, T_m,1(respectively T_m,2). The second melting temperature of the second material is lower than the first melting temperature of the first material: T_m,1>T_m,2. The term ‘melting temperature’ is known by the one skilled in the art. First and second materials of the first 20 and second 30 layer are chosen among the following materials: metals, semi-metals or semiconductors. The first layer 20 has an upper surface 20u and a lower surface 20b separated by the thickness t₁of the first layer 20. The second layer 30 has an upper surface 30u and a lower surface 30b separated by the thickness t₂of the second layer 30.

As shown in FIG. 1, a layup 50 (or stack) has to be formed by stacking the first and second layers (20,30) such that the lower surface 20b of the first layer 20 contacts and at least partially overlaps the upper surface 30u of the second layer 30. The overlap of the first layer 20 with the second layer 30 defines an interface 17. In FIG. 1, it is assumed that the lower surface 20b of the first layer 20 totally overlaps the upper surface 30u of the second layer 30. However, this is not required for the method of the invention. FIG. 3 shows another example of the layup 50 that is formed for carrying out the method of the invention. In this example, the lower surface 20b of the first layer 20 does not totally overlap the upper surface 30u of the second layer 30. In this case, the interface 17 has an area that is smaller than the areas of the lower surface 20b of the first layer 20 and of the upper surface 30u of the second layer 30. The lower surface 20b of the first layer 20, the upper surface 30u of the second layer 30, and the interface 17 can be planar, smooth or rough. In fact, not specific shape of these surfaces is required for carrying out the method of the invention.

A rotating tool 70 is pressed and translated over at least a friction portion 15 of the upper surface 20u of the first layer 20. The layup 50 is preferably firmly clamped to a backing plate when the rotating tool 70 is pressed and translated over at least a friction portion 15 of the upper surface 20u of the first layer 20. As shown in FIG. 3, the portion of the interface 17 that is in registry with the friction portion 15 defines the first joint surface 10 along which the at least two layers (20,30) are welded or joined. The terms ‘in registry with’ means that the friction portion 15 of the upper surface 20u of the first layer 20 along which the rotating tool 70 is translated comprises the orthogonal projection of the first joint surface 10 on said upper surface 20u of the first layer 20. In FIG. 1, the first joint surface 10 is equivalent to the interface 17. In FIG. 3, the first joint surface 10 is smaller than the interface 17.

FIG. 2 shows different temperature profiles that can be induced along the thickness (t₁+t₂) of the layup 50 and below the rotating tool 70 when it is pressed on the upper surface 20u of the first layer 20. Because of the rotation and of the translation of the rotating tool 70, the temperature of the friction portion 15 is raised by friction. The heat that is generated is transferred to the second layer 30 through the thickness t₁of the first layer 20. For the method of the invention, the temperature reached by at least a portion of the upper surface 30u of the second layer 30, because of the translation of the rotating tool 70 along the friction portion 15, has to be higher than the second melting temperature T_m,2of the second layer 30 (or of the second material). The at least one portion of the upper surface 30u of the second layer 30 that has to reach a temperature higher than T_m,2is comprised in the first joint surface 10. Hence, a liquid phase of the second material is formed at a portion of the upper surface 30u of the second layer 30 that is included in the first joint surface 10. In FIG. 2, temperature profile 130 does not correspond to a situation where a portion of the upper surface 30u of the second layer 30 reaches a temperature higher than T_m,2. However, temperature profiles 120, 110, and 100 allow obtaining a liquid phase of the second material at a portion of the upper surface 30u of the second layer 30. Indeed, at least a portion of the upper surface 30u of the second layer 30 reaches a temperature higher than T_m,2in these cases. Hence, such temperature profiles correspond to normal conditions when the method of the invention is carried out. Temperature profile 100 corresponds to a situation where the second layer 30 is melted over its whole thickness t₂: at least a portion of the lower surface 30b of the second layer 30 reaches a temperature higher than T_m,2in this case. When the portion of the upper surface 30u of the second layer 30 that has reached a temperature higher than T_m,2cools down below this temperature T_m,2, the two layers (20,30) are welded and an inter-phase is formed between first 20 and second 30 layers. The inter-phase results from the reaction that takes place between the first 20 layer that remains solid and the second 30 layer that is melted at least along a portion of the upper surface 30u of the second layer 30: atoms or molecules of the first layer 20 diffuse into the liquid phase of the second layer 30, forming a ‘chemical’ inter-phase when temperature decreases. Concurrently or alternatively, crystals may grow from one layer across the interface and penetrating into the second layer, thus forming a ‘physical’ inter-phase. Alternatively, atoms or molecules of both first 20 and second 30 layers diffuse to the other layer forming an inter-phase. Such an inter-phase can therefore have a chemical composition different from first 20 and second 30 layers and/or a different physical configuration from these two layers (20,30).

Restraining means allow preventing molten second material of the second layer 30 from flowing out of the layup 50. Different examples of restraining means are presented below. So, contrary to the FSB technique, the layer that is melted is one of the layers to join. In the FSB technique, the layer that is melted only serves as a solder and is squeezed out during the joining process.

The rotating tool 70 that is pressed and translated over at least a friction portion 15 of the upper surface 20u of the first layer 20 can be tilted of a angle α with respect to an axis that is perpendicular to the upper surface 20u of the first layer 20. This is illustrated in FIG. 4. Preferably, the angle α is comprised between 0° and 5°, and more preferably between 0.5° and 1°. Tilting the rotating tool 70 with respect to an axis that is perpendicular to the upper surface 20u of the first layer 20 ensures a good mechanical contact between this tool 70 and the upper surface 20u of the first layer 20. Moreover, such an inclination of the rotation tool 70 allows obtaining a smoother surface behind it.

The distance of the rotating tool 70 with respect to the upper surface 20u of the first layer 20 (parameter z in FIG. 4) can be adjusted by force (pressure) or position control. When controlled by force, the machine holding the rotating tool 70 automatically adjusts its position to keep the pressure applied to the upper surface 20u of the first layer 20 constant. When using a position control, the position of the rotating tool 70 follows instructions but the pressure applied by the rotating tool 70 on the upper surface 20u of the first layer 20 can vary. Parameter z in FIG. 4 is generally named ‘plunge’ by the one skilled in the art. Preferably, the plunge z is negative to generate enough heat by friction. A negative plunge z means that the rotating tool 70 penetrates the first layer 20. Preferably, the plunge z is comprised between −0.7 mm and 0 mm, and is more preferably equal to −0.55 mm. Still more preferably, z is comprised between −0.2 mm and 0 mm, and still more preferably between −0.08 mm and −0.01 mm. The rotating tool 70 can have various shapes. Preferably, it has a cylindrical shape.

FIG. 5 shows an example of restraining means for preventing molten second material from flowing out of the layup 50. In this example, said restraining means comprise a cavity 90 with side walls 95 into which the layup 50 is snugly placed. Hence, when the rotating tool 70 is pressed and translated over at least a friction portion 15 of the upper surface 20u of the first layer 20 molten second material is retained in the layup 50 because of the side walls 95.

FIG. 6 shows another example of restraining means for preventing molten second material from flowing out of the layup 50. In this case, a mask 200 is placed on top of the upper surface 20u of the first layer 20 such that the rotating tool 70 cannot reach a fringe extending along the perimeter 20p of the upper surface 20u of the first layer 20. Hence, the rotating tool 70 is pressed and translated over the hatched surface of FIG. 6 in this case. As the rotating tool 70 does not reach the perimeter 20p of the upper surface 20u of the first layer 20, some regions of the first material remain solid close to the borders of the layup 50 preventing molten second material from flowing out of the layup 50. Alternatively, means controlled by a computer or a central processing unit (CPU) could prevent the rotating tool 70 from reaching a fringe extending along the perimeter 20p of the upper surface 20u of the first layer 20.

FIG. 7 shows another example of restraining means for preventing molten second material from flowing out of the layup 50. In this case, the lower surface 30b of the second layer 30 remains solid. Hence, the temperature reached by the lower surface 30b of the second layer 30 is lower than T_m,2. This solid surface allows preventing molten second material from flowing out of the layup 50. In this preferred embodiment of the method of the invention, the second layer 30 comprises a liquid zone 31 and a solid zone 32 as shown in FIG. 7. Each of the three examples of restraining means that are shown in FIGS. 5 to 7 can be combined to each other. So, one can place the layup 50 in a cavity 90 with side walls 95 and provide a mask 200 on the upper surface 20u of the first layer 20. Alternatively, one can use the mask 200 of FIG. 6 and choose the experimental parameters such that the lower surface 30b of the second layer 30 remains solid.

Preferably, the two layers (20,30) are two metal layers. This means that the first 20 and second 30 layers preferably comprise a metallic material. More preferably, the first material of the first layer 20 is steel and the second material of the second layer 30 is aluminium. In such a case, the first melting temperature, T_m,1, is typically comprised between 1300° C. and 1400° C. whereas the second melting temperature, T_m,2, can be about 660° C. or less. Preferably, the first material of the first layer 20 has a thermal conductivity at 20° C. higher than 1 W(m*K), and more preferably higher than 10 W(m*K).

Preferably, the first melting temperature, T_m,1, of the first material is higher than T_m,2+50° C., where T_m,2is the second melting temperature of the second material of the second layer 30. More preferably, the ratio T_m,1/T_m,2is higher than 1.2, and more preferably, higher than 1.5.

Preferably, the thickness t₁of the first layer 20 and the thickness t₂of the second layer 30 are comprised between 0.1 and 5 mm, and more preferably between 0.3 and 2 mm. Still more preferably, t₁and t₂are comprised between 0.6 and 1.4 mm. However, other values of the thickness t₁and t₂could be used. In particular, any values of the thickness t₂can be used.

Preferably, the rotating tool 70 is made of a material comprising cemented carbide or tungsten carbide. Preferably, the rotating tool 70 has a cylindrical shape with an external diameter comprised between 10 and 20 mm, and more preferably between 12 and 16 mm.

Preferably, the rotating tool 70 is translated over the at least one friction portion 15 of the upper surface 20u of the first layer 20 with a speed that is comprised between 50 mm/min and 1000 mm/min, and more preferably between 100 mm/min and 500 mm/min. By using a speed higher than 500 mm/min (and more preferably a speed of translation equal to 1000 mm/min), the quality of the inter-phase can be increased. Moreover, one can obtain an inter-phase that has a smaller thickness. When an intermetallic layer 220 is formed between first 20 and second 30 layers, its thickness is reduced by using a speed of translation of the rotating tool 70 that is comprised between 500 mm/min and 1000 mm/min. Still more preferably, this translation speed is comprised between 200 and 400 mm/min, and is still more preferably equal to 300 mm/min. When the speed of translation of the rotating tool 70 over the friction portion 15 of the upper surface 20u of the first layer 20 is increased, the raise in temperature induced in the first layer 20 decreases.

Preferably, the speed of rotation of the rotating tool 70 is comprised between 1000 and 4000 revolutions per minute, more preferably between 2000 and 3000 revolutions per minute, and is still more preferably equal to 2500 revolutions per minute.

Preferably, the following sets of first and second materials of first 20 and second 30 layers are used:

- ULC steel (first layer 20) with Al2024 (second layer 30);
- ULC steel (first layer 20) with Al6061 (second layer 30);
- FeV (33 at % V)—Al.

First 20 and second 30 layers are preferably submitted to a surface treatment before carrying out the method of the invention. More preferably, at least one of these layers (20, 30) can be galvanized steel or anodized aluminium.

Some examples of the welding of two layers with the method of the invention are now presented. For these examples, the top layer 20 comprises ULC (Ultra-Low Carbon) steel, and the second layer 30 comprises aluminium of high purity (aluminium 1050: purity of 99.5%). The thickness t₁of the first layer 20 is equal to 0.8 mm whereas the thickness t₂of the second layer 30 is equal to 0.6 mm. The layup 50 comprising the first 20 and second 30 layers was firmly clamped on a backing plate. In this case, the second layer 30 did not melt along its whole thickness t₂. Hence, the restraining means comprise a solid lower surface 30b of the second layer 30 in this case. The rotating tool 70 was a cylinder comprising tungsten carbide and having an external diameter equal to 16 mm. The speed of rotation of the rotating tool 70 was equal to 2000 revolutions per minute. The rotating tool 70 was translated over the upper surface 20u of the first steel layer 20 with an angle α equal to 0.5° with respect to an axis perpendicular to the upper surface 20u of the first layer 20 (see in FIG. 4 how the angle α is defined).

FIGS. 8 and 9 show images of microstructures of two layers that are welded according to the method of the invention. For these experiments, the temperature profiles induced along the thickness of the layup (t₁+t₂) during the welding process corresponds to curves 120 or 110. The images of FIGS. 8 and 9 were obtained by a SEM (Scanning Electron Microscope) technique detecting backscattered electrons (BSE). Such a technique is known by the one skilled in the art. Heavy elements (high atomic number) backscatter electrons more strongly than light elements (low atomic number), and thus appear brighter in the images. The two layers that appear in FIGS. 8 and 9 and that are welded have the characteristics detailed in previous paragraph. FIG. 8 (respectively FIG. 9) corresponds to a case where the speed of translation of the rotating tool 70 over the upper surface 20u of the first layer 20 is equal to 200 mm/min (respectively 400 mm/min). The other experimental parameters have been detailed in the previous paragraph. A structure of solidification 210 in the second aluminium layer 30 can be observed in both FIGS. 8 and 9, next to the interface with the first steel layer 20 (right part of the second aluminium layer 30). Hence, the aluminium has been melted in this region 210. In both cases (FIGS. 8 and 9), an intermetallic layer 220 comprising Fe and Al is formed next to the boundary between the two layers (20,30). Such an intermetallic layer 220 indicates that aluminium of the second layer 30 has melted as a chemical reaction between aluminium and steel took place. When the speed of translation of the rotating tool 70 is equal to 200 mm/min (case of FIG. 8), the intermetallic layer 220 has a thickness around 6 μm. When the speed of translation of the rotating tool 70 is equal to 400 mm/min (case of FIG. 9), the intermetallic layer 220 has a thickness around 3 μm. This difference of thickness of the intermetallic layer 220 between cases of FIGS. 8 and 9 is due to different values of the speed of translation of the rotating tool 70 over the upper surface 20u of the first layer 20. The raise in temperature under the rotating tool 70 and in the second layer 30 is higher when this rotating tool 70 is translated with a smaller speed of translation over the upper surface 20u of the first layer 20. Preferably, the thickness of the intermetallic layer 220 that is formed between the first 20 and second 30 layer with the method of the invention is comprised between 0.5 and 1.5 μm. In the examples shown in FIGS. 8 and 9, the intermetallic layer 220 is the inter-phase between first 20 and second 30 layers.

In another preferred embodiment, the method of the invention is used for welding three layers (see FIG. 10). In this case, a third layer 40 of a third material is provided. This third material has a third melting temperature, T_m,3, that is higher than the second melting temperature, T_m,2, of the second layer 30. As shown in FIG. 10, the layup 50 that is formed then comprises the three layers (20,30,40). The upper surface 40u of the third layer 40 contacts and at least covers the portion of the lower surface 30b of the second layer 30 that is in registry with the first joint surface 10. In FIG. 10, it is assumed that the first joint surface 10 comprises the whole lower surface 20b of the first layer 20 (or equivalently that the friction portion 15 comprises the whole upper surface 20u of the first layer 20). However, this is not necessary for the method of the invention as explained with FIG. 3. In the preferred embodiment of the method of the invention for welding three layers, the rotating tool 70 that is pressed and translated over at least a friction portion 15 of the upper surface 20u of the first layer 20 raises the temperature of the lower surface 30b of the second layer 30 to a value higher than the second melting temperature, T_m,2, of the second layer 30. Hence, the second layer 30 melts over its whole thickness t₂in this case. Restraining means whose examples have been given above allow preventing molten second material from flowing out of the layup 50. When the method of the invention is used for welding three layers, the thickness t₂of the second layer 30 is preferably comprised between 0.1 mm and 30 mm, and more preferably, between 0.5 mm and 20 mm. When the method of the invention is used for welding three layers, the thermal conductivity of the first layer 20 is preferably higher than 1 W(m*K) at 20° C., more preferably higher than 10 W(m*K) at 20° C., and still more preferably higher than 100 W(m*K) at 20° C. When the method of the invention is used for welding three layers, the thermal conductivity of the second layer 30 is preferably higher than 1 W(m*K) at 20° C., more preferably higher than 10 W(m*K) at 20° C., and still more preferably higher than 100 W(m*K) at 20° C. Any material for the third layer 40 can be used. Preferably, the material of the third layer 40 is chosen among the following materials: ceramics, polymers, metals, semimetals or semiconductors.

Preferably, the third material of the third layer 40 of FIG. 10 is vanadium. More preferably, this third material is steel.

FIG. 11 shows images of microstructures of three layers (20,30,40) when the method of the invention is used for welding such three layers. These images were obtained by a SEM technique using BSE. In this example, the first layer 20 comprises ULC steel, the second layer 30 comprises aluminium, and the third layer 40 comprises vanadium (purity of 99.8%). The left part of FIG. 11 shows parts of the third 40 and second 30 layers whereas the right part of FIG. 11 shows parts of the second 30 and of the first 20 layers. The thickness t₁of the first layer 20 is equal to 0.8 mm; the thickness t₂of the second layer 30 is equal to 0.6 mm, and the thickness t₃of the third layer 40 is equal to 0.5 mm. All three layers (20,30,40) are 200 mm long and 60 mm large. For welding such three layers (20,30,40), the rotating tool 70 was not translated over the whole upper surface 20u of the first layer 20. Hence, the restraining means in this case correspond to means (and more precisely to a clamping system for keeping the layup 50 on a backing plate) preventing the rotating tool 70 from reaching a fringe extending along the perimeter 20p of the upper surface 20u of the first layer 20.

From FIG. 11, it can be seen that the aluminium second layer 30 melted over its whole thickness t₂. It can also be observed that chemical affinity between materials of the different layers strongly affect the thickness of the intermetallic layers 220 between each layers (20,30,40). The thickness of the intermetallic layer 220 between third 40 and second 30 layers is around 1 μm whereas the thickness of the intermetallic layer 220 between second 30 and first 20 layers is around 50 μm.

The present invention has been described in terms of specific embodiments, which are illustrative of the invention and not to be construed as limiting. More generally, it will be appreciated by persons skilled in the art that the present invention is not limited by what has been particularly shown and/or described hereinabove. Reference numerals in the claims do not limit their protective scope. Use of the verbs “to comprise”, “to include”, “to be composed of”, or any other variant, as well as their respective conjugations, does not exclude the presence of elements other than those stated. Use of the article “a”, “an” or “the” preceding an element does not exclude the presence of a plurality of such elements.

Summarized, the invention may also be described as follows. The method of the invention relates to a method for welding a first 20 and a second 30 layers together. The second melting temperature of the second layer 30, T_m,2, is lower than the first melting temperature of the first layer 20, T_m,1. After having formed a layup 50 by placing the first layer 20 on top of the second layer 30, a rotating tool 70 is pressed and translated over at least a friction portion 15 of the upper surface 20u of the first layer 20 such that the temperature reached by at least a portion of the upper surface 30u of the second layer 30 is higher than the second melting temperature, T_m,2. Restraining means allow preventing molten second material from flowing out of the layup 50. Materials of first 20 and second 30 layers are chosen among the following materials: metals, semi-metals, or semiconductors. It is preferred that at least one of the first 20 and second 30 layers is a metal. It is most preferred that both layers (20, 30) are metals. In particular, the first 20 and second 30 layers may preferably consist of aluminium, steel, copper, vanadium.

Number	Date	Country	Kind
12166124.3	Apr 2012	EP	regional
PCT/EP2013/058844	Apr 2013	EP	regional

Method for Welding at Least Two Layers

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