• 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:
    The present invention relates to a method for assembling between a piece (1) of metallic material and a part (2) made of organic matrix composite material, which method comprises the following successive steps: a) a step of supplying said two parts ( 1, 2), each having a surface to be welded (11, 21), and which surface to be welded (21) of said composite part (2) is constituted, at least partially, by an exposed part (51) of at least a metal insert (5) which is partially embedded in said composite part (2), b) a step of positioning said weld surfaces (11, 21) opposite and at a distance from each other, and c) a high-speed projecting step of the soldering surface (11) of the metal part (1) on the surface to be welded (21) of the composite part (2), to obtain a high speed plating of said surfaces to be welded (11). , 21) one on the other and to obtain a welding between the expo part (51) of the metal insert (5) of the composite part (2) and the complementary part of the surface to be welded (11) of the metal part (1).
    公开号:FR3030329A1
    申请号:FR1462943
    申请日:2014-12-19
    公开日:2016-06-24
    发明作者:Guillaume Racineux；Didier Priem；Jean-Michel Lebrun；Yannick Amosse；Chady Khalil
    申请人:Faurecia Automotive Composites；Ecole Centrale de Nantes；
    IPC主号:
    专利说明:

    [0001] TECHNICAL FIELD TO WHICH THE INVENTION RELATES The present invention relates to the assembly between two parts, namely a part made of metallic material and a part made of composite material made of organic matrix.
    [0002] It relates in particular to a method for obtaining such an assembly, as well as an assembly consisting of the two assembled parts. TECHNOLOGICAL BACKGROUND In many areas, including transportation, multi-material structures are becoming more widespread in order to meet the increasing demands of users (particularly in terms of lighter structures, aesthetics and implementation of new technologies). features such as electrical isolation or damping). It is thus common to need to combine parts made of metallic material and parts made of organic matrix composite material. To ensure satisfactory rigidity of two assembled parts, it is often preferable to achieve intimate connections, generally obtained by welding. However, in practice, metal materials and organic matrix composite materials are not compatible with each other for the implementation of a heterogeneous welding. For this reason, the current technologies for the assembly of such materials are: - the mechanical assembly, for example the screwing or the riveting, and - the joining by adhesion, in particular by gluing. But the mechanical assembly technology has the particular disadvantage of generating a weight of the structure due to the connection elements reported. In addition, piercing the parts for the positioning of these connecting elements can generate areas of weakness, stress concentration or failure initiation. The assembly by gluing has the disadvantage of requiring a preparation of the surfaces, and also not to allow a reliable prediction of the long-term behavior of this bonding.
    [0003] In this context, there is a need for new technologies for the assembly between parts made of metallic material and parts made of organic matrix composite material.
    [0004] OBJECT OF THE INVENTION The present invention relates to a new assembly technology between a piece of metallic material (hereinafter referred to as a "metal part") and a part made of organic matrix composite material (hereinafter referred to as "composite part"). , which has the advantage of relying on a welding assembly. For this, the present invention provides for bringing a metal insert into the composite part, at the level of a surface to be welded, a part of which is arranged in an exposed manner so as to be assembled by a high-speed welding technique with a surface complementary to the metal part. The method according to the invention comprises the following successive steps: a) a step of supplying said two parts, which parts each comprise a surface intended to be welded with a surface complementary to the other part, and which surface to be welded of said part composite is constituted, at least partially, by an exposed portion of at least one metal insert which is partially embedded in said composite part, b) a step of positioning said weld surfaces opposite and at a distance from each other and c) a step of high-speed projection of the surface to be welded on the metal part to the surface to be welded of the composite part, to obtain a high speed plating of said surfaces to be welded to one another and to to obtain a welding between the exposed part of the metal insert of the composite part and the complementary part of the surface to be welded of the metal part. According to other advantageous characteristics, which can be taken in combination or independently: the composite part comprises a front face provided with the surface to be welded, and during the supply step, the metal insert of the composite part is flush of the front face of said composite part, or in the case of a laminated composite material formed of several plies, is located between said plies of said composite part and with cutting in the overlying folds to obtain the exposed part of the metal insert; for a composite part made of a thermoplastic material, the step of supplying the composite part comprises an operation of inclusion of the metal insert by heating and by pressure in said composite part; the metal insert has a thickness of between 0.1 and 3 mm; the metal insert and the metal part are made of a material chosen from steel and an aluminum alloy; the metal insert consists of a plate provided with through-holes or a solid plate; preferably, the metal insert consists of a plate provided with through orifices having a flared shape on the side of the exposed part, to increase the resistance to mechanical tearing of the metal insert in the composite part; at least a part of the unexposed surface of the metal insert, in contact with the composite material, is prepared, for example by shot blasting, so as to increase the contact surface between said metal insert and the constituent material of the composite part; the metal part comprises a part to be sprayed, a front surface of which constitutes the surface to be welded, and the projection step is obtained by means of a magnetic pulse which is applied to said part to be projected; in this case, possibly, the metal part is electrically non-conductive, and the part to be sprayed has a rear surface, opposite to the surface to be welded, which is covered with an electrically conductive material; - The projection step is carried out so as to obtain a progressive plating of the surfaces to be welded to one another, to ensure an expulsion of the oxides; in this case, preferably, said progressive plating is obtained by means of (i) at least one electrical insulating shim formed between the two parts and surrounding the part to be sprayed, or (ii) a part to project in shape a boss, or (iii) a fold on the edge of the metal part, intended to form said part to project.
    [0005] The present invention also relates to a composite material part, comprising a surface to be welded which is formed, at least partially, by an exposed portion of at least one metal insert partially embedded in said part made of organic matrix composite material.
    [0006] According to a particular embodiment of this piece of composite material, the metal insert has one-piece mounting lugs, a projecting portion of which resides on the side of the rear face of the composite part and is folded against said rear face of the composite part. The invention also relates to an assembly comprising a part made of metallic material and a part made of composite material, wherein together said composite part comprises at least one metal insert partially embedded in said composite part, which at least one metal insert comprises a part exposed on the surface of said composite part which is welded with a complementary part of the surface of the metal part. DETAILED DESCRIPTION OF THE INVENTION The present invention will be further illustrated, without being limited in any way, by the following description of various embodiments illustrated in the appended figures in which: FIG. 1 is a general schematic view of two parts assembled by welding; following the implementation of the assembly method according to the invention; - Figure 2 shows schematically and in section, the two main steps of the assembly method according to the invention, namely a positioning step (A) and a high speed projection step (B); - Figure 3 shows a first possible embodiment of a composite part according to the invention, comprising a metal insert flush with a front face of said composite part; FIG. 4 represents a second possible embodiment of the composite part according to the invention, in which this part is of the multi-ply type and the metal insert is attached between its folds, the overlying folds being cut to obtain the exposed portion of said metal insert; - Figure 5 shows, from above and in perspective, the surface to be welded of a composite part which is equipped with a metal insert consisting of a plate provided with a plurality of through holes; FIG. 6 schematically represents the composite part according to FIG. 5, seen according to a vertical sectional plane, the composite part according to FIG. 5; - Figure 7 shows schematically and in perspective, the surface to be welded of a composite part which is provided with a metal insert in the form of an elongate solid metal plate; - Figure 8 shows, schematically and in perspective, the surface to be welded of a composite part which is provided with several metal inserts juxtaposed and each in the form of a solid metal plate; FIG. 9 schematically illustrates, in two steps, an operation of inclusion of the metal insert, by heating and by pressure, in the thickness of a composite part; - Figure 10 schematically shows a first particular embodiment of the positioning and projection steps of the assembly method according to the invention, implementing an insulating shim system; - Figure 11 shows schematically a second particular embodiment of the positioning and projection steps of the assembly method according to the invention, wherein the part to be projected from the metal part is in the form of a boss; - Figure 12 schematically shows a third particular embodiment of the positioning and projection steps of the assembly method according to the invention, wherein the metal plate has a part to be projected in the form of a fold; FIG. 13 diagrammatically represents a fourth particular embodiment of the positioning and projection steps of the assembly method according to the invention, in the case of a composite part according to FIG. 4, the metal insert of which is reported between its folds; FIG. 14 diagrammatically represents another embodiment of the metal insert according to the invention, of the insert-to-staple type; FIG. 15 schematically illustrates, in two steps, an operation of inclusion of the metal insert according to FIG. 14, by heating and by pressure, in the thickness of a composite part. As represented in FIG. 1, the present invention thus proposes a new technology for the assembly between, on the one hand, a piece 1 made of metallic material and, on the other hand, a piece 2 made of organic matrix composite material, At the level of a welding zone 3. For the sake of simplification, these parts 1, 2 are again designated, respectively, under the names "metal part 1" and "composite part 2". in particular means a permanent connection, or not removable (subject to degradation or deterioration), between the two parts 1, 2 at the welding zone 3. By "assembly" means in particular a "welding" ensuring a continuity of the nature of the materials to be assembled. By "assembly" is advantageously meant a high speed plating assembly, preferably in the form of a magnetic pulse welding technique. The metal part 1 is advantageously made of a metallic material chosen from steel or an aluminum alloy. The metal part 1 is advantageously in the form of a plate, having a thickness of between 0.5 and 3 mm. This metal part 1 comprises in particular two opposite faces (FIGS. 1 and 2): a front face 1a intended to come opposite the composite part 2 and having a surface to be welded 11 to form part of the welding zone 3, and - a rear face 1b, opposite to said front face 1a. The composite part 2 is itself made of a material comprising: - a reinforcement, usually fibers, and - an organic matrix. The fibers of the reinforcement are characterized by their composition (metal, glass, polymer, carbon, vegetable, etc.), their length (short (0.1 to 1 mm), long (1 to 50 mm) or continuous (greater than 50 mm), and their arrangement (mat or woven) or multi-material NCF The continuous fibers may be arranged parallel to each other, for a unidirectional reinforcement, or at a predefined angle (45 ° for example relative to each other). to others) for multidirectional reinforcement, or in a random way: "NCF" or "Non Crimp Fabrics" means a multiaxial fabric which consists of several layers (or layers) unidirectional (UD), stitched together with a wire (usually PET).
    [0007] For example, a biaxial NCF material + 45 ° / -45 ° is a fabric composed of two UD plies: the first ply is composed of UD at + 45 ° and the second ply is composed of UD at -45 °. There are also 0 ° / 90 ° biaxial NCF materials or 0 ° / + 45 ° / -45 ° triaxial NCF materials. This composite material can still be laminated, formed of several folds (not shown). By "fold" is commonly meant the semi-composite product (fibers plus matrix) presented in quasi-two-dimensional form; we still hear a thickness composed of wicks or "tapes" parallel, linked by the matrix.
    [0008] The organic matrix is advantageously chosen from thermosetting materials and thermoplastic materials. By "thermosetting material" is meant, in particular: - unsaturated polyester resins (UP), which are generally used with glass fibers, - epoxy resins (EP), which are generally used with carbon fibers, - resins vinylester, - polyurethane resins, - phenolic resins (PF), - thermosetting polyimide resins (PI) and polybismaleimides (BMI). By "thermoplastic material" is meant in particular: polypropylene, polyamide, polyetherimide (PEI), polyphenylene sulphide (PPS) and polyphenylene ether-ketone ( PEEK). On its side also, the composite part 2 is advantageously in the form of a plate, having a thickness of between 0.5 and 10 mm. This composite part 2 comprises in particular two opposite faces (FIGS. 1 and 2): a front face 2 intended to come opposite the metal part 1 and having a surface to be welded 21 to form part of the welding zone 3 and a rear face 2b opposite said front face 2a. According to the invention, the surface to be welded 11 of the metal part 1 is intended to be assembled, by a high speed projection technique, with the surface to be welded 21 of the composite part 2.
    [0009] For this, as illustrated in FIG. 2, the method according to the invention comprises the following successive steps: a step of supplying the two parts 1, 2 to be assembled, a step of positioning the surfaces to be welded. , opposite and at a distance from each other (part A of FIG. 2), and - a step of high speed projection of the surface to be welded 11 of the metal part 1 onto the surface to be welded 21 of the composite part 2, to obtain the welding zone 3 (part B of FIG. 2). To obtain such an assembly (even though the respective materials are incompatible for a connection by welding), the composite part 2 provided comprises at least one metal insert 5 which is partially embedded at its welding surface 21 (Figure 2). During the high speed projection step, the surface to be welded 11 of the metal part 1 is thus pressed at high speed onto the surface to be welded 21 of the composite part 2, thereby causing a welding phenomenon between the metal insert 5 of the composite part 2 and a complementary part of the surface to be welded 11 of the metal part 1. This provides a bonding by welding, without adding material, between the metal insert 5 and the metal part 1 (corresponding to a continuity of matter between them).
    [0010] The metal insert 5 is therefore housed in the composite part 2, at the level of the area where it is desired to assemble the metal part 1. For this reason, depending on the case, the metal insert 5 can be placed at a distance from the edge of the composite panel 2, but also along this edge. The metal insert 5, and its implantation in the composite part 2, are described in more detail below with reference to FIGS. 2 to 9. In this case, the metal insert 5 is implanted in the composite part 2 of so as to have an exposed portion 51 which is stripped at its weld surface 21 (Figure 2 - Part A in particular). By "exposed portion" is thus meant a portion of the surface of the metal insert 5 which is directly accessible at the surface to be welded 21 of the composite part 2. In particular, this exposed portion 51 of the metal insert 5 must not be covered by the composite material, in particular by the organic matrix. The metal insert 5 is made of a material which is chosen according to the material constituting the metal part 1 to be assembled. In particular, this material is chosen to allow a dynamic plating welding technique between the exposed portion 51 of the metal insert 5 and the surface to be welded 11 of the metal part 1. For example, this metal insert 5 can be made of steel or aluminum alloy when the metal part 1 is made of aluminum alloy.
    [0011] Without limitation, other possible combinations of materials are: - Aluminum-aluminum, - Aluminum-copper - Aluminum-magnesium - Aluminum-titanium - Copper-copper - Copper-steel - Copper-bronze - Nickel-titanium - Nickel The steel insert 5, for example in the form of a plate or a plate, comprises: an outer face 53 intended to form the exposed part 51 of the metal insert 5; inner face 54 opposite, embedded in the material of the composite part 2, and - a peripheral contour 55, embedded in the material of the composite part 2.
    [0012] For example, this metal insert has a thickness of between 0.1 and 3 mm. As shown in Part A of Figure 2, but also in Figures 3 and 4, the metal insert 5 is embedded in the thickness of the composite part 2; it extends over only a part of its thickness.
    [0013] In particular, as illustrated in FIG. 3, the metal insert 5 is flush with the front face 2a of the composite part 2. In this case, the outside face 53 of the metal insert 5 and the front face 2a of the part composite 2 extend in the same plane, or at least approximately in the same plane.
    [0014] Alternatively, as shown in FIG. 4, the metal insert 5 can be attached between the folds (not shown) of the composite part 2. A cutout 25 is then formed in the overlying folds with respect to the outer face 53 of the metal insert 5, so as to obtain the exposed portion 51 of the metal insert 5 corresponding to the surface to be welded 21 of the composite part 2. To optimize its cohesion with the composite material, the surface of the The metal insert 5 in contact with this composite material, called the "unexposed surface", can be prepared so as to obtain an irregular surface. By "unexposed surface" is meant in particular the internal face 54 and / or the peripheral contour 55 of the metal insert 5. For example, shot blasting may be applied to this unexposed surface of the metal insert 5, so as to increase the contact area between the matrix of the composite part 2 and the metal insert 5. Moreover, the metal insert 5 may consist of a solid part or a perforated part.
    [0015] For example, as illustrated in FIGS. 5 and 6, the metal insert 5 is provided with a plurality of through orifices 56, opening at its outer 53 and inner 54 faces. Each of these through orifices 56 is delimited by a contour 561 which has a flared shape from the inner surface 54 to the outer surface 53 (Figure 6), for example a generally frustoconical or truncated pyramid shape. These through orifices 56 are advantageously filled by the material constituting the composite part 2 (organic matrix and optionally the fibers) so as to increase the resistance to mechanical tearing of the metal insert 5 provided on the composite part 2. The percentage orifice 56 is adapted according to the expected compromise between, on the one hand, the resistance by welding between the metal insert 5 and the metal part 1 and, on the other hand, the maintenance of the metal insert 5 in the composite material. A solid plate consists, for its part, in a plate devoid of the through orifices as described above in relation to FIGS. 5 and 6. The metal insulator (s) 5 of the surface to be welded 21 may be in various shapes and sizes, depending in particular on the desired assembly. FIG. 7 represents a first embodiment in which the metal insert 5 of the surface to be welded 21 has an elongated shape, here of generally rectangular shape.
    [0016] Its exposed portion 51 thus also consists of an elongate strip of generally rectangular shape, to obtain a continuous welding zone 3. For example, as an indication, the metal insert 5 has a length of between 10 and 100 mm and a width of between 10 and 30 mm. FIG. 8 shows yet another embodiment in which the surface to be welded 21 of the composite part 2 consists of the exposed part 51 of a group of juxtaposed metal inserts 5 (in this case three in number), to form a spot welding area.
    [0017] Each metal insert 5 here has a general square or rectangular shape; its exposed portion 51 thus also consists of a square or rectangular shape. For example, as an indication, each metal insert 5 has a length of between 20 and 40 mm and a width of between 20 and 40 mm. The composite part 2, with its added metal insert 5, can be obtained by any suitable method. For example, as shown in FIG. 9, the composite part 2 can be obtained during an operation of inclusion of the metal insert 5 by heating and by pressure within a heating press 6. A such a method is possible in the case of a composite part 2 made of a thermoplastic material. Such an inclusion operation consists in: - depositing a composite part 2, devoid of metal insert 5, on a fixed part 61 of the heating press 6, - depositing the metal insert 5 on the front face 2a of the part composite 2, at its surface to be welded 21 (part A of Figure 9), - to apply a pressure with heating through a movable heating jaw 62 of the heating press 6, so as to heat the insert 5 and to embed it in the composite plate 2 (part B of FIG. 9). In particular, the metal insert 5 is heated to a temperature which is a function of the melting temperature of the matrix of the composite part 2. More specifically, this metal insert 5 is brought to a temperature equal to or greater than this temperature fusion. For example, the metal insert 5 is heated to a temperature of 260 ° C, with the application of a pressure of 27 bar, for an extruded polyamide matrix 6.6.
    [0018] This assembly could also be obtained by any other method of assembly, for example by sewing (the metal insert 5 is sewn with the pre-impregnated fabrics before consolidation). Starting from such a composite part 2 with its metal insert 5, as described above, the step of relative positioning of the two parts 1, 2 is implemented so that the surfaces to be welded 11, 21 extend. facing one another and at a distance advantageously between 0.5 and 1.5 mm. The high-speed projecting step is implemented in such a way as to obtain a high-speed plating of the surfaces to be welded 11, 21 on each other and to obtain a weld between the exposed portion 51 of the metal insert 5 of the composite part 2 and the complementary part of the surface to be welded 11 of the metal part 1. By "high speed" is meant in particular a speed of between 150 m / s and 400 m / s.
    [0019] This projection step is advantageously carried out by means of a pulse which is applied to a projecting part 15 of the metal part 1. In this case, this projecting part comprises two opposite surfaces: a front surface 151, corresponding to the surface to be welded 11 of the metal part 1 and situated on the side of its front face 1a, and - a rear surface 152, opposite the weld surface 11 mentioned above and located on the side of the rear face 1b of the metal part 1. A projection force is thus applied on this part to be projected 15, in a direction extending from its rear surface 152 towards its front surface 151 and in a direction directed towards the surface to be welded 21 of the composite part 2 The projection step is advantageously obtained by means of magnetic pulse projection means 7.
    [0020] A welding cycle, conventional in itself, can be summarized by the following 6 steps: a charger is powered by an electrical energy network; the electrical energy is then stored in capacitors in the form of electrostatic energy, the stored energy being gradually increased via the charging voltage controlled by an energy control unit; when the fixed threshold of the charging voltage is reached, a spark gap (or discharger) discharges the electrostatic energy of the capacitors very rapidly into an inductor 71 (during this discharge, whose duration is of the order of a hundred or so ps, extremely high electric currents of the order of several hundred kA are generated); the circulation of this high current through the inductor 71 very abruptly generates a magnetic induction field in the coil; there is a transformation of electrostatic energy into magnetic energy; the magnetic field thus created can have a large amplitude (of the order of several tens of tesla); it is highly variable over time, so generates in the metal part 1 to weld induced currents also called "Foucault currents"; the interaction between the primary magnetic field created by the coil and the currents induced in the metal part 1 generates significant forces of magnetic origin, forces acting mechanically on the metal part 1 in which the eddy currents flow; these magnetic forces very abruptly transform the magnetic energy into mechanical energy acting radially on the part to be projected 15 of the metal part 1, the latter is then propelled onto the composite part 2 held fixed. This projection phenomenon is thus the consequence of an extremely fast transfer of energy, the power of this process being of the order of several hundred megawatts, but for very short durations. This process is practically adiabatic and there is no real heat transfer: the welding between the metal insert 5 and the metal part 1 is performed "cold". Indeed, the materials do not reach more than 30 ° C. There is therefore no heat affected area in the composite material that does not lose its properties. The magnetic pulse welding process is also a "Solid State" type welding process, which means that the material is not melted during the welding cycle.
    [0021] In the case of an electrically non-conductive metal part, the rear surface 152 of the part to be sprayed 15 is then advantageously covered with an electrically conductive material forming a "pusher", for example made of aluminum alloy, so as to obtain the desired projection.
    [0022] Alternatively, it may be envisaged to use any other suitable technique to produce a projection at high speed, for example by means of a mechanical action or by means of a laser shock. In the various cases, under the effect of the propulsive force, the part to be sprayed is deformed so that its surface to be welded is pressed at high speed against the surface to be welded of the composite part. high speed then generates a welding phenomenon between the exposed portion 51 of the metal insert 5 of the composite part 2 and the complementary part of the surface to be welded 11 of the metal part 1. This gives a multi-material assembly, comprising a part 1 made of metallic material and a part 2 made of organic matrix composite material, wherein said composite part 2 comprises a metal insert 5 partially embedded in said composite part 2, which metal insert 5 has an exposed portion 51 on the surface 2a of said composite part 2 which is welded with a complementary part of the surface 11 of the metal part 1. Various embodiments can be envisaged to obtain this positioning and this projection, as described in more detail below with reference to FIGS. 10 to 13. In these various embodiments, the projection step is advantageously implemented so as to obtain a progressive plating of the surfaces to be welded 11, 21 one on the other, to ensure an expulsion of the oxides.
    [0023] By "progressive plating" is meant in particular a contact of the surfaces to be welded which begins with a point, then which extends on a line, before spreading until all the surface is in contact (welding surface). According to a first embodiment illustrated in FIG. 10, the parts to be welded 1, 2 are attached remotely from one another by means of a system of electrical insulating shims 8 distributed around the periphery of the surfaces to be welded. 11, 21 (Figure 10 - Part A). The front faces 1a, 2a of the two parts 1, 2, and their surfaces to be welded 11, 21 respectively, are then separated by a distance equal to the height of the shims 8 reported.
    [0024] The projection step will thus propel at high speed the part to be projected 15 of the metal part 1, in the direction of the surface to be welded 21 of the composite part 2, in the space separating their respective front faces 1a, 2a ( Figure 10- Part B).
    [0025] The part to be sprayed thus presents, in the end, a convex arrangement with respect to the front face la of the metal part 1. According to another embodiment illustrated in FIG. 11, the part to be projected 15 of the metal part 1 is initially has the form of a boss which is concave at the surface to be welded 11 (protruding at the rear face lb of the metal part 1) (Figure 11 - Part A). The boss is in particular arranged so as to maintain a distance of between 0.5 and 1.5 mm between its weldable surface 11 and the surface to be welded 21 of the composite part 2. The projection step will thus propel high speed the part to be projected 15 of the metal part 1, boss-shaped, towards the surface to be welded 21 of the composite part 2 (Figure 11 - part B). The projecting part 15 thus has, in the end, a planar or substantially plane arrangement with respect to the metal part 1 (FIG. 11 - part B).
    [0026] According to a third embodiment illustrated in part A of FIG. 12, the part to be projected 15 of the metal part 1 consists of a folding of this metal plate 1, forming an angle with the surface to be welded 21 of the composite part 2 The metal part 1 thus comprises: - a rear part 16, covering the rear face 2b of the composite part 2, - a lateral part 17, matching the edge of the composite part 2, and - a front part, extending in facing the front face 2a of the composite part 2 and forming a fold intended to constitute the part to be sprayed 15. The projection step will thus propel at high speed the projecting part 15 of the metal part 1, shaped fold in the direction of the welding surface 21 of the composite part 2 (Figure 12 - Part B).
    [0027] The composite part 2 is thus ultimately sandwiched between the rear portion 16 and the front portion 17 of the metal part 1 (Figure 12 - Part B). According to a fourth embodiment illustrated in FIG. 13, the composite part 2 of FIG. 4 (with the metal insert 5 inserted between the folds of said composite part 2) and a flat metal part 1 are attached to each other on the other (Figure 13 - part A). The front faces 1a, 2a of the two parts 1, 2 are supported on one another, and their respective surfaces to be welded 11, 21 are then separated by a distance equal to the height of the overlying folds by relative to the outer face 53 of the metal insert 5. This height still corresponds to the height of the cutout 25 formed in the overlying folds above. The projection step will thus propel at high speed the part to be projected 15 of the metal part 1, in the direction of the surface to be welded 21 of the composite part 2, in the space separating their weld surfaces 11, 21 respectively ( Figure 13 - Part B). The part to be sprayed thus has, in the end, a convex arrangement with respect to the front face la of the metal part 1, extending within the cutout 25. In this case, the distance between the surfaces to be welded 11, 21 allows direct welding, without the use of insulators or pads. FIG. 14 diagrammatically represents another embodiment of the metal insert 5 according to the invention, of the insert-to-staple type, in order to optimize its cohesion with the composite material. Such a metal insert 5, similar to that described above in relation to FIGS. 2 to 9, also comprises one-piece mounting tabs 57 which are distributed at its peripheral contour 55 (in particular of these long sides) and which extend on the side of its inner face 54.
    [0028] The metal insert 5 advantageously comprises through holes 56 as developed above in relation to FIGS. 5 and 6. The one-piece mounting tabs 57 facing each other (connected to the two long sides) are here divergent with respect to one another. , deviating from the metal insert 5.
    [0029] These mounting lugs 57 are also flexible, so as to be folded during the mounting of the metal insert 5 on the composite part 2. In this respect, FIG. 15 schematically represents an operation of inclusion of the metal insert 5 according to FIG. 14, by heating and by pressure, in the thickness of a composite part 2, this according to a method similar to that described above in relation to FIG. 9. Such a method is possible in the case of a composite part 2 made of a thermoplastic material. Such an inclusion operation consists in: - depositing a composite part 2, devoid of metal insert 5, on a fixed part 61 of the heating press 6, - depositing the metal insert 5 on the front face 2a of the part composite 2, at its surface to be welded 21 (part A of Figure 15), - to apply a pressure with heating through a movable heating jaw 62 of the heating press 6, so as to heat the insert 5 Again, the metal insert 5 is heated to a temperature which is a function of the melting temperature of the matrix. In this last step, the one-piece mounting tabs 57 penetrate the thickness of the composite part 2 to emerge on the side of its rear face 2, until the outer face 53 of the metal insert 5 extends in the plane, or at least approximately in the plane, of the front face 2a of the composite part 2. The projecting portion 571 of these one-piece mounting brackets 57 (protruding from the side of the rear face 2b of the composite part 2) are then folded against the rear face 2b of the composite part 2, advantageously by means of a shape adapted to the fixed part 61 of the heating press 6. In general, the present invention has the advantage of allowing an effective assembly between a metal part and a composite part, without affecting their respective properties. This technical solution has the further advantage of allowing the implementation of conventional means, usually used for assembling two metal parts together.
    权利要求:
    Claims (14)
    [0001]
    1. A method for assembling a piece (1) of metallic material and a part (2) made of organic matrix composite material, which method comprises the following successive steps: a) a step supplying said two pieces (1,
    [0002]
    2), which parts (1, 2) each have a surface (11, 21) to be welded with a complementary surface (11, 21) of the other part (1, 2), and which surface to be welded (21). ) of said composite part (2) is constituted, at least partially, by an exposed part (51) of at least one metal insert (5) partially embedded in said composite part (2), b) a positioning step said welding surfaces (11, 21) facing each other at a distance from one another, and c) a step of high speed projection of the surface to be welded (11) of the metal part (1) onto the surface soldering (21) of the composite part (2), to obtain a high-speed plating of said weld surfaces (11, 21) one on the other and to obtain a weld between the exposed portion (51) of the metal insert (5) of the composite part (2) and the complementary part of the surface to be welded (11) of the metal part (1). 2. Assembly method according to claim 1, characterized in that the composite part (2) comprises a front face (2a) provided with the surface to be welded (21), and in that, during the supply step , the metal insert (5) of the composite part (2) is: - flush with the front face (2a) of said composite part (2), or - in the case of a composite material formed of several plies between said plies of said composite part (2) and with a cutout (25) in the overlying folds to obtain the exposed part (51) of the metal insert (5).
    [0003]
    3. Assembly method according to any one of claims 1 or 2, for a composite part (2) made of a thermoplastic material, characterized in that the step of providing the piececomposite (2) comprises an operation of inclusion of the metal insert (5), by heating and pressure, in said composite part (2).
    [0004]
    4. Assembly method according to any one of claims 1 to 3, characterized in that the metal insert (5) is made of steel or aluminum alloy, and in that said metal part (1) is made of steel or aluminum alloy.
    [0005]
    5. Assembly method according to any one of claims 1 to 4, characterized in that the metal insert (5) consists of a plate provided with through orifices (56) or a solid plate.
    [0006]
    6. A method of assembly according to claim 5, characterized in that the metal insert (5) consists of a plate provided with through holes (56) having a flared shape on the side of the exposed portion (51) reported in the composite part (2) so that the composite material fills at least a portion of said through holes (56).
    [0007]
    7. Assembly method according to any one of claims 1 to 6, characterized in that at least a portion of the unexposed surface (54, 55) of the metal insert (5), in contact with the composite material, is prepared so as to increase the contact surface between said metal insert (5) and the constituent material of the composite part (2).
    [0008]
    8. A method of assembly according to any one of claims 1 to 7, characterized in that the metal part (1) comprises a portion to be sprayed (15), a front surface (151) constitutes the surface to be welded (11). , and in that the projection step is obtained by means of a magnetic pulse which is applied to said projection part (15).
    [0009]
    9. Assembly method according to claim 8, characterized in that the metal part (1) is non-conductive electrical, and in that the part to project (15) has a rear surface (152), opposite the surface solder (11), which is covered with an electrically conductive material.
    [0010]
    10. The assembly method according to any one of claims 1 to 9, characterized in that the projection step is carried out so as to obtain a progressive plating of the surfaces to be welded (11, 21) one on the other, to ensure the expulsion of the oxides.
    [0011]
    11. An assembly method according to claim 10, characterized in that said progressive plating is obtained by means of: - at least one electrical insulating wedge (8) formed between the two parts (1, 2) and surrounding the part to projecting (15), or - a projection part (15) in the form of a boss, or - a folding on the edge of the metal part (1), intended to form said projection part (15).
    [0012]
    12. Part made of organic matrix composite material, for carrying out the assembly method according to any one of the preceding claims, comprising a surface to be welded (21) which is formed, at least partially, by an exposed part ( 51) of at least one metal insert (5) partially embedded in said composite part (2).
    [0013]
    13. Part made of organic matrix composite material according to claim 12, characterized in that the metal insert (5) comprises one-piece mounting lugs (57), a protruding part (571) of which resides on the side of the rear face (2b). ) of the composite part (2) and is folded against said rear face (2b) of said composite part (2).
    [0014]
    14. Assembly comprising a part (1) made of metal material and a part (2) made of organic matrix composite material, resulting from an assembly process according to any one of claims 1 to 13, wherein said part composite (2) comprises at least one metal insert (5) partially embedded in said composite part (2), which at least one metal insert (5) has an exposed portion (51) on the surface (2a) of said composite part (2). ) which is welded with a complementary part of the surface (11) of the metal part (1).
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    同族专利:
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    US10611094B2|2020-04-07|
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    CN107530822A|2018-01-02|
    EP3233364B1|2019-09-11|
    WO2016097656A1|2016-06-23|
    US20180050496A1|2018-02-22|
    CN107530822B|2020-04-03|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US20040155030A1|2002-12-24|2004-08-12|Jim Schmidt|Method for joining vehicle frame components|
    DE102006024604A1|2006-05-26|2007-11-29|Bayerische Motoren Werke Ag|Fiber composite component|
    DE102011106700A1|2011-07-06|2012-03-08|Daimler Ag|Component for motor vehicle, has insert part sectionally held in fiber reinforced plastic e.g. thermoplastic, from which component is made, where component is weldable with metallic sheet by interposition of insert part with metallic sheet|
    FR2998210A1|2012-11-20|2014-05-23|Plastic Omnium Cie|ASSEMBLY OF A METAL INSERT AND A MATERIAL COMPOSITE TABLE, METHOD FOR INCORPORATING SUCH AN INSERT IN SUCH A TABLET AND PART OBTAINED BY MOLDING SUCH A TABLET|
    DE1911940A1|1969-03-10|1970-09-24|Hoehn Jakob|Method for mounting panels on substrates, and nailable holders for carrying out the method|
    DE69612925T2|1995-03-10|2002-03-28|Nippon Petrochemicals Co Ltd|METAL / PLASTIC COMPOSITE PLATE, FLOATING ACTUATOR THEREFOR, AND METHOD FOR THEIR PRODUCTION|
    DE10125559A1|2001-05-23|2002-11-28|Basf Ag|Composite component manufacturing method, involves compression of a punched edge on a metal component into a plastic component to form a connection|
    DE102011055993B3|2011-12-02|2013-03-21|Benteler Automobiltechnik Gmbh|Automotive chassis component|
    US9553296B1|2012-03-23|2017-01-24|Greatbatch Ltd.|Magnetic pulse welding in medical power manufacturing|KR101807039B1|2016-04-28|2017-12-08|현대자동차 주식회사|Composites having insert steel for welding|
    FR3065663B1|2017-04-28|2019-06-28|Faurecia Automotive Composites|METHOD OF ASSEMBLING TWO PIECES OF DIFFERENT MATERIALS AND ASSEMBLY ARISING FROM THE ASSEMBLY PROCESS|
    KR20190041306A|2017-10-12|2019-04-22|주식회사 엘지화학|Manufacturing method of different material joint body|
    US10369748B2|2017-10-26|2019-08-06|Battelle Memorial Institute|Friction stirring interlocking of dissimilar materials|
    法律状态:
    2015-12-08| PLFP| Fee payment|Year of fee payment: 2 |
    2016-06-24| PLSC| Publication of the preliminary search report|Effective date: 20160624 |
    2016-10-14| PLFP| Fee payment|Year of fee payment: 3 |
    2017-11-21| PLFP| Fee payment|Year of fee payment: 4 |
    2019-11-20| PLFP| Fee payment|Year of fee payment: 6 |
    2020-11-20| PLFP| Fee payment|Year of fee payment: 7 |
    2021-11-18| PLFP| Fee payment|Year of fee payment: 8 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1462943A|FR3030329B1|2014-12-19|2014-12-19|PROCESS FOR ASSEMBLING BETWEEN A METAL MATERIAL PART AND A COMPOSITE MATRIX PART WITH ORGANIC MATRIX|FR1462943A| FR3030329B1|2014-12-19|2014-12-19|PROCESS FOR ASSEMBLING BETWEEN A METAL MATERIAL PART AND A COMPOSITE MATRIX PART WITH ORGANIC MATRIX|
    PCT/FR2015/053654| WO2016097656A1|2014-12-19|2015-12-18|Assembly method between a part made of metal material and a part made of organic matrix composite material; corresponding parts made of organic matrix composite material and assembly|
    CN201580069575.1A| CN107530822B|2014-12-19|2015-12-18|Method for assembling metal material part and organic matrix composite material part|
    US15/537,556| US10611094B2|2014-12-19|2015-12-18|Assembly method between a part made of metal material and a part made of organic matrix composite material; corresponding parts made of organic matrix composite material and assembly|
    EP15823690.1A| EP3233364B1|2014-12-19|2015-12-18|Assembly method between a part made of metal material and a part made of organic matrix composite material; corresponding assembly|
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