• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:

    公开号:FR3017562A1
    申请号:FR1451293
    申请日:2014-02-18
    公开日:2015-08-21
    发明作者:Florian Chotard；Cyrille Collart；Didier Trichet；Javad Fouladgar
    申请人:Airbus Operations SAS；
    IPC主号:
    专利说明:

    [0001] The present invention relates to a method and a device for induction welding of parts made of composite materials. The invention relates in particular to the assembly of parts made of composite materials in the aeronautical field.
    [0002] The composite material parts generally comprise carbon fibers embedded in a resin, which are deposited, for example by draping, so as to form folds superimposed on each other. In each fold, the fibers are aligned in a main direction (0 °, 45 °, 90 °). The planes of the folds of carbon fibers are parallel to each other and define a so-called plane main plane. In addition, the manufacturing processes of such a part generate points of contact between the folds whose distribution is random and depends on the nature of the resin and the rate of deposition of carbon fibers. Induction welding of thermoplastic composite material parts consists in using an inductor emitting a magnetic field and an interface element, generally made of conductive metal, disposed at the interface of the parts to be welded in order to concentrate the magnetic fields. The conductive metal is heated to a so-called process temperature corresponding at least to the transformation temperature of the composite materials causing the softening of the structure of the composite parts to locally mix the two parts and thus allow them to be welded together. The parts to be welded together must be made of composite materials called "compatible", that is to say that are such that at the transformation temperature, the materials adhere to each other. However, the main disadvantages of this type of process are, on the one hand, the very localized presence of conductive metal in the final product, and on the other hand, the difficulty of controlling the temperature of the process. Certain induction welding devices circulate the currents induced in the carbon of the surface folds of the composite materials. These devices, in general, tend to heat the contact walls by circulating induced currents in paramagnetic materials, such as the carbon of the carbon fibers of the composite materials, that is to say with a low sensitivity magnetic fields and with electrical conductivity to transform the circulation of eddy currents temperature by Joule effect. This involves applying intense magnetic fields to generate currents induced in these materials. Induced currents can also flow in the folds that are not at the interface and along the points of contact between the folds. In composite material parts subjected to the magnetic field of an induction welding device, the induced currents circulate in two directions: - the main direction, in the folds, along the carbon fibers of the parts, and - a secondary direction , perpendicular to the main direction, between the folds, along which are positioned the points of contact between folds. These induced current flow welding processes are therefore difficult to control in terms of temperature and welding interface. Indeed, it is difficult to control the magnetic field to limit its effect only to the surface carbon folds that are at the interface of the two composite materials to be welded. EP1326741B1 discloses a polymer matrix composition comprising ferromagnetic elements dispersed in a polymer matrix and a method for generating homogeneous hysteresis heating in the composition. With such a matrix, the heating of the polymer matrix is homogeneous, localized and precisely controlled in temperature. In addition, the induction welding of thermoplastic composites, especially high performance, is implemented in the usual manner using an inductor having a mono-facial configuration.
    [0003] Such processes, with or without a conductive metal, suffer from several limitations which prevent their industrialization in the aeronautical field. Indeed, the design of the geometry of the inductor is complex for simple plane surface geometries. It requires simulations demanding significant computing resources, for example an L shape requires fifteen days of simulation to obtain the shape of the inductor, without guarantee of homogeneity of the thermal effect. There is, in addition, a strong sensitivity to the distance between the inductor and the interface element, which influences the thermal balance at the interface. The magnetic fields emitted by the inductor are at first very intense in its near environment, then decrease exponentially while moving away from the inductor. This configuration implies a geometric sensitivity, that is to say a tolerance of the distance between the inductor and the metal, less than one-tenth of a millimeter. In the case of a single-face type inductor, this distance acts strongly on the thermal balance at the interface. If this distance varies, the temperature is too high or, on the contrary, not important enough. Thus, there is a close connection between the geometry of the single-face inductor and those of the parts to be welded. For each configuration, it is necessary to design a different inductor, with an adaptation of the welding parameters, such as the frequency, the intensity of the field, or the impedance of the inductive system. The present invention aims to remedy all or part of the disadvantages of the prior art. It relates to a method of induction welding of at least two composite material parts comprising carbon fibers embedded in a resin and oriented along a main direction belonging to a main plane, said method comprising the following steps: a) formation of at least one field absorber configured to absorb a magnetic field and comprising a ferromagnetic material; b) forming an assembly comprising the parts to be welded and the field absorber arranged at the contact walls of the parts; and c) generating, for a predefined duration, a homogeneous alternating magnetic field in the assembly with a bifacial inductor, in a direction of incidence, so as to heat the contact walls of the assembly. up to a so-called process temperature. According to the invention, the welding method is remarkable in that it further comprises a step of inclining at least one of the following elements: the assembly and the bifacial inductor, so as to orient the direction of incidence of the magnetic field with respect to the principal plane at an angle different from 90 ° and different from a null angle. Thus, the method according to the invention provides for applying a uniform (homogeneous) field via a bifacial inductor and no longer a mono-facial inductor. The homogeneity of the field lines favors a uniform temperature on all the contact walls. In addition, the method makes it possible to optimize the preponderance of hysteresis heating on induced current heating, by applying a magnetic field in a direction of incidence with respect to the principal plane at an angle different from 90 ° and different from a zero angle. This makes it possible to uniformly heat the assembly, particularly at the level of the contact walls of the composite material. The generation of this uniform magnetic field makes it possible to dispense with the geometry of the assembly to be welded. It is therefore no longer necessary, thanks to the invention, to adapt the inductor to each surface or form of the assembly to be welded. This method can be used regardless of the shape and profile of the parts to be welded.
    [0004] The present invention can present various embodiments, which can be taken in combination or separately: the method comprises a step of applying a contact pressure on the assembly; the method comprises an additional step, subsequent to the step c) and consisting in cooling the assembly while maintaining the contact pressure, after stopping the generation of the magnetic field as a whole, - the process temperature is defined between a resin conversion temperature and a temperature greater than this transformation temperature of the resin by at least 50 ° C, in step c), the assembly is displaced with respect to the bifacial inductor according to a speed of displacement, the generation time of the magnetic field in the set being controlled according to the speed of movement. The present invention also relates to a composite element comprising at least two pieces of composite materials welded to each other by the aforementioned method. The present invention furthermore relates to a device for induction welding of at least two parts made of composite materials comprising carbon fibers embedded in a resin and oriented in a main direction belonging to a main plane, the device comprising at least one heating unit provided with at least one bifacial inductor comprising two walls spaced apart and distributed on either side of a support on which is disposed, in use, an assembly comprising the parts to be welded and a field absorber, the field absorber being configured to absorb a magnetic field and comprising a ferromagnetic material, the field absorber being arranged at the contact walls of the two parts, so as to heat them to a so-called process temperature, the device comprising , also, generation means and means for adapting an alternating current for use in generating a n homogeneous magnetic field between the two walls of the bifacial inductor.
    [0005] According to the invention, this device further comprises means for inclining at least one of the following elements: the assembly and the bifacial inductor, so as to orient the direction of incidence of the magnetic field by compared to the main plane at an angle different from 90 ° and different from a zero angle. Said field absorber can be realized in different ways. In particular, it may comprise: a ferromagnetic grid embedded in a film of composite material compatible with those of the parts to be welded, and forming an interface element; ferromagnetic particles embedded in a film of composite material compatible with those of the parts soldering, and forming an interface element, - ferromagnetic particles embedded in the contact wall of at least one of said parts. In a preferred embodiment, each wall of the bifacial inductor comprises a Helmholtz coil. The appended figures will make it clear how the invention can be realized. In these figures, identical references designate similar elements. Figure 1 is a schematic perspective view of a particular embodiment of a welding device illustrating the invention, and Figure 2 shows schematically a side view of the welding device of Figure 1. The welding device 1, shown in Figures 1 and 2, is intended to quickly weld parts 2, 3 compatible thermoplastic composite materials (continuous fibers or long fibers, short or without reinforcement), such as a skin and a foot clip for example. The parts 2, 3 comprise carbon fibers aligned in a main direction Dp and embedded in a resin, the fibers forming folds parallel to a plane called the main plane Pp. This main plane Pp is perpendicular to a secondary direction Di, along which can be positioned points of contact between folds during the manufacture of the parts 2, 3. To do this, the device 1 comprises in particular a support 25, a pressure generating unit 17 and a heating unit 18. L ' heating unit 18 comprises a bifacial inductor 19 and is configured to generate a homogeneous alternating magnetic field 7 in an assembly 21 comprising the two parts 2 and 3 and a field absorber 4, as shown in Figure 2, for a predefined duration. The invention is however not limited to the welding of two parts, and could be applied to several parts to be assembled together, a field absorber then being disposed between each piece.
    [0006] As shown in FIG. 1, the heating unit 18 comprises, in addition to the bifacial inductor 19, an alternating electric current generator 14, and means 15 for adapting this current. In the embodiments shown, the bifacial inductor 19 comprises two parallel walls 5, 6 spaced apart and forming respectively a pair of Helmholtz coils which are connected to the means 15 and which generate a homogeneous alternating magnetic field between the coils. Each Helmholtz coil comprises at least one circular turn 5A, 6A of defined radius, the two coils being substantially identical. An electric current flowing in the coil produces a magnetic field, in a direction of incidence DB, shown in Figure 2 by field lines 7 perpendicular to the plane of the turns 5A, 6A. The two coils are arranged in parallel, at a distance from each other substantially equal to their radius. Thus, a homogeneous magnetic field is obtained on a circular area. Alternatively, the Helmholtz coils may comprise several turns 5A, 6A activatable independently of each other, in order to adapt the power of the magnetic field to the types of composite materials to be welded. As illustrated in FIG. 2, the welding device 1 furthermore comprises tilting means 27 of the support 25 intended to orient the parts 2, 3. For example, the inclining means 27 comprise an assembly of at least three pneumatic cylinders located under the sides of the support 25. Thus, by a set of movements different from one jack to the other, the parts 2,3 can be inclined along at least three axes so that an angle between the direction of incidence DB of the magnetic field 7 and the main plane Pp of the folds of the carbon fibers is: - different from 90 °, in order to limit heating by circulation of induced currents along the main direction Dp of carbon fibers; and - different from 0 °, in order to limit heating by circulation of induced currents, on the points of contact between folds, along the secondary direction Di. The inclination means 27 can also be applied to the bifacial inductor 19. In this variant embodiment (not shown), the two walls 5, 6 of the bifacial inductor 19 are oriented while the support 25, on which the assembly 21 is disposed, remains fixed. In another variant not shown, the tilting means 27 may comprise first inclination elements applied to the bifacial inductor 19 and second inclination elements applied to the assembly 21. To weld two parts 2 and 3 in compatible composites, a field absorber 4 is arranged at the interface of the two parts 2 and 3. The field absorber 4 is configured to absorb the magnetic field 7 emitted by the Helmholtz coils. The field absorber 4 is, for example, a polymer resin loaded with ferromagnetic particles, as described in patent EP1326741B1. The field absorber 4 comprises a ferromagnetic material (in the form of a grid or in the form of ferromagnetic particles) whose relative magnetic permeability is higher than the magnetic permeability of the resin used and that of the carbon of the fibers (magnetic permeability relative p <2 TmA-1), for example iron powder (relative magnetic permeability p = 250 TmA-1 and Curie temperature = 770 °).
    [0007] In a first embodiment, the grid or the ferromagnetic particles are embedded in a resin film compatible with those of the two parts 2 and 3, and form an interface element 20 disposed between the contact walls of the two parts 2 and 3 , so that the welding takes place during the transformation of the composite materials. According to another embodiment, the ferromagnetic particles are mixed with the resin of the composite material on the contact wall of at least one of the parts 2 and 3 at the time of manufacture of the parts 2 and 3. The ferromagnetic material is present in the form of spherical ferromagnetic particles embedded in the resin, for example polysulfone (PSU), with volume fractions ranging from 10% to 20%. The diameter of the ferromagnetic particles is small (between 22 microns and 300 microns). The homogeneity of the resin-particle mixture is a function of the resin grade, the granulometry of the ferromagnetic material particles and the impregnation between the resin and the carbon fibers (quality of the fiber / resin interface, viscosity of the resin). the resin, porosity rate). This other embodiment makes it possible to directly contact the two parts 2 and 3, without having to provide for the welding an interface element (such as the interface element 20) containing the ferromagnetic material between the parts 2 and 3. 3. The two parts 2 and 3, as well as the field absorber 4 (integrated in one of the parts 2 and 3 or in an interface element 20), form an assembly 21 which is maintained by a contact pressure , represented by one or more arrows 9 in FIGS. 1 and 2, exerted by the pressure generating unit 17, by means of pressure-applying elements 10. The contact pressure is directed so that the parts 2 and 3 are pressed against each other. The assembly 21, placed in the space between the coils, is subjected to the effect of the magnetic field emitted by the coils, the grid made of ferromagnetic material or the ferromagnetic particles producing, in particular, heat. Thus, the field absorber 4 heats homogeneously the interface between the two parts 2 and 3, thanks to the magnetic field uniformly distributed in the zone 8 where is placed the assembly 21.
    [0008] In the case of hysteresis heating, the homogeneity of the thermal response in the surface is obtained thanks to the regularity of the surface distribution of the particles of ferromagnetic material (in one of the parts 2 and 3 or in the element of interface 20). The impact of the surface with respect to the field and the shape of the surface to be welded have no impact on the thermal distribution. This process is constrained, in particular, by the size of the ferromagnetic particles, their nature, the intensity of the magnetic field 7 and its frequency. In order to guarantee appropriate temperature levels at the interface of parts 2 and 3, a ferromagnetic material having a Curie temperature characteristic adapted to the resins used is used. Thus, the ferromagnetic material is chosen such that its Curie temperature is identical to a defined temperature, called "process temperature", corresponding, for example, to the temperature of transformation of the resin increased by a value of 0 ° to 50 ° according to the geometry of the parts to be welded. The Curie temperature corresponds to the temperature at which the ferromagnetic material becomes paramagnetic and loses, in particular, its thermal and electrical conduction properties. The transformation temperature depends on the nature of the resin and is, for example: either the supercooling temperature in the case where the resin of the parts 2, 3 is of semicrystalline material; or the melting temperature (or "softening" start temperature) in the case where the resin of the parts 2, 3 is of amorphous material; or the polymerization temperature in the case where the resin of the parts 2, 3 is of thermosetting material. For example, in the case of carbon fibers embedded in a polyetheretherketone resin (referred to as PEEK), the ferromagnetic material used may be NiFe5.
    [0009] The Curie temperature is the temperature at which the ferromagnetic material becomes paramagnetic. This ferromagnetic material has a sensitivity to the magnetic field 7 much larger than the composite material to be welded. The conductivity and magnetic permeability of ferromagnetic materials change with temperature. At a fixed magnetic field frequency, the electrical permittivity of the materials also changes as a function of the temperature and reaches a threshold beyond which it no longer evolves. Therefore, the application of a magnetic field 7 makes it possible to increase the temperature of the assembly 21 up to the Curie temperature, at which the ferromagnetic material loses its magnetization and stabilizes in temperature, which makes it possible to obtain a constant heating temperature. The temperature of the ferromagnetic material subjected to a magnetic field follows a hysteresis cycle. These characteristics therefore make it possible to define a window around a characteristic temperature of the ferromagnetic material. By adapting the inductive parameters such as the frequency of the alternating current and the power injected by the generator 14, associated with a homogeneous field configuration, a homogeneous heating is generated at the interface at a controlled and reproducible temperature level. This avoids the temperature variations on the contact walls, because the applied field is homogeneous and acts on the ferromagnetic material which has a specific Curie point corresponding to the transformation temperature of the composite materials. The homogeneity of the electromagnetic field is furthermore guaranteed by the geometry of the inductor. In a Helmholtz coil, the field is homogeneous in the central part (zone 8), on a diameter substantially equivalent to the radius of the turns 5A, 6A. In the case where the two composite materials are of different natures, one chooses the highest transformation temperature of the two, so that the two materials are transformed together. The magnetic field 7 is maintained for a defined time in order to obtain a sufficient transformation of the contact walls. Once the magnetic field 7 is stopped, the assembly 21 is kept in contact by the contact pressure applying members 10 until it has sufficiently cooled down. Thus, the device 1 further comprises cooling means 23 (FIG. 1). In a preferred embodiment, the cooling means 23 comprise a set of channels for circulating a fluid, such as water or air, on the assembly 21, as illustrated by an arrow 24 on the Figure 1. Cooling is achieved when the temperature of the assembly 21 has fallen below the crystallization temperature of the composite materials. In this case, the welding between the two parts 2 and 3 composite materials is performed and the contact pressure, become unnecessary, is stopped. In a first embodiment of the invention, the assembly 21 is held stationary during welding in the bifacial inductor 19. In addition, in a second embodiment of the invention, the device 1 further comprises displacement means 22, which are able to move the assembly 21 between the coils, as represented by an arrow 16 in FIG. 3. The assembly 21 is subjected to a translation in the zone 8 where the magnetic field 7 is homogeneous . The speed of movement of the assembly 21 (generated by the displacement means 22) is adjusted so that the exposure time to the magnetic field 7 (between the coils) is sufficient to reach the transformation temperature of the composite materials, and thus to obtain the welding of the parts 2 and 3. In this second embodiment, a production line makes it possible to produce the assembled parts 2 and 3 by circulating them in an assembly between the two coils. The magnetic field 7 is applied with parameters defined according to the nature of the ferromagnetic material, particle size or grid. In a preferred embodiment, the frequencies are high (of the order of the MHz), as well as the powers (the magnetic field 7 is greater than 5000 A / m). High frequencies (1 MHz to 10 MHz) provide heating of multiple magnetic domains in particles that are favorable to the hysteresis effect. In addition, a high magnetic field, greater than 5000 A / m, allows better control of heating through the Curie temperature. In addition, these inductive parameters initiate hysteresis heating and limit heating by circulation of induced currents. It will be noted that the device according to the invention makes it possible to weld complex geometries of simple shape or presenting a double curvature, or which comprise variations of thickness.
    权利要求:
    Claims (10)
    [0001]
    REVENDICATIONS1. A method of induction welding of at least two composite material parts (2, 3) comprising carbon fibers embedded in a resin and oriented along a main direction belonging to a main plane (Pp), said method comprising the following steps: a) forming at least one field absorber (4) configured to absorb a magnetic field (7) and comprising a ferromagnetic material; b) forming an assembly (21) comprising the parts (2, 3) to be welded and said at least one field absorber (4) arranged at the contact walls of the parts (2, 3); and c) generating, for a predefined duration, a homogeneous alternating magnetic field (7) in the assembly (21) using a bifacial inductor (19), in a direction of incidence (DB), so as to heat the contact walls of the assembly to a so-called process temperature, characterized in that the method further comprises a step of inclining at least one of the following: (21) and the bifacial inductor (19), so as to orient the direction of incidence (DB) of the magnetic field (7) relative to the main plane (Pp) by an angle other than 90 ° and different from a zero angle.
    [0002]
    2. Method according to claim 1, characterized in that it comprises a step of applying a contact pressure (9) on the assembly (21).
    [0003]
    3. Method according to claim 2, characterized in that it comprises an additional step, subsequent to step c) and of cooling the assembly (21) while maintaining the contact pressure (9), after a stop of generating the magnetic field (7) in the assembly (21).
    [0004]
    4. Method according to any one of the preceding claims, characterized in that the process temperature is defined between a transformation temperature of the resin and a temperature above this resin conversion temperature of at least 50 ° C.
    [0005]
    5. Method according to any one of the preceding claims, characterized in that in step c), the assembly (21) is displaced relative to the bifacial inductor (19) at a speed of displacement, the duration generating the magnetic field (7) in the assembly (21) being controlled as a function of the traveling speed.
    [0006]
    6. Induction welding device of at least two pieces (2, 3) of composite materials comprising carbon fibers embedded in a resin and oriented in a main direction belonging to a main plane (Pp), the device (1) comprising at least one heating unit (18) provided with at least one bifacial inductor (19) comprising two walls (5, 6) spaced apart and distributed on either side of a support (25) on which is disposed, in use, an assembly (21) comprising the parts (2, 3) to be welded and a field absorber (4), the field absorber (4) being configured to absorb a magnetic field (7) and comprising a ferromagnetic material, the field absorber (4) being arranged at the contact walls of the two parts (2, 3) to be welded, so as to heat them to a so-called process temperature, the device (1) comprising, also , generating means (16) and means (15) for adapting a current rectifier for use in generating a homogeneous magnetic field (7) between the two walls (5, 6) of the bifacial inductor (19), characterized in that the device (1) further comprises tilting means (27) at least one of the following: the assembly (21) and the bifacial inductor (19), so as to orient the direction of incidence (DB) of the magnetic field (7) relative to the main plane (Pp) at an angle different from 90 ° and different from a null angle.
    [0007]
    7. Device according to claim 6, characterized in that each wall of the bifacial inductor (19) comprises a Helmholtz coil.
    [0008]
    8. Device according to one of claims 6 and 7, characterized in that the field absorber (4) comprises a ferromagnetic grid embedded in a film of composite material compatible with those of the parts (2, 3) to be welded, and forming an interface element (20).
    [0009]
    9. Device according to one of claims 6 and 7, characterized in that the field absorber (4) comprises ferromagnetic particles embedded in a film of composite material compatible with those of the parts (2, 3) to be welded, and forming an interface element (20).
    [0010]
    10. Device according to one of claims 6 and 7, characterized in that the field absorber (4) comprises ferromagnetic particles embedded in the contact wall of at least one of said parts (2, 3).
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    同族专利:
    公开号 | 公开日
    EP2907651A1|2015-08-19|
    EP2907651B1|2018-05-23|
    US20150231869A1|2015-08-20|
    US9770892B2|2017-09-26|
    FR3017562B1|2016-03-11|
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    FR3083734B1|2018-07-16|2021-12-24|Arkema France|INDUCTION WELDING PROCESS FOR PARTS BASED ON THERMOPLASTIC MATERIAL|
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    法律状态:
    2015-02-19| PLFP| Fee payment|Year of fee payment: 2 |
    2016-02-18| PLFP| Fee payment|Year of fee payment: 3 |
    2017-02-17| PLFP| Fee payment|Year of fee payment: 4 |
    2018-02-23| PLFP| Fee payment|Year of fee payment: 5 |
    2019-10-25| ST| Notification of lapse|Effective date: 20191006 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1451293A|FR3017562B1|2014-02-18|2014-02-18|METHOD AND DEVICE FOR INDUCTION WELDING OF PARTS IN COMPOSITE MATERIALS.|FR1451293A| FR3017562B1|2014-02-18|2014-02-18|METHOD AND DEVICE FOR INDUCTION WELDING OF PARTS IN COMPOSITE MATERIALS.|
    EP15151123.5A| EP2907651B1|2014-02-18|2015-01-14|Method and device for induction welding of parts made of composite materials|
    US14/623,143| US9770892B2|2014-02-18|2015-02-16|Induction welding process and device for parts made of composite materials|
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