METHOD FOR PRODUCING A COMPOSITE MATERIAL PART, STEERING COLUMN SUPPORT AND LOWER SPACE CROSS MEMBER PRODUCED BY SUCH A METHOD
20200230897 ยท 2020-07-23
Assignee
Inventors
Cpc classification
H01M10/6556
ELECTRICITY
B29B11/16
PERFORMING OPERATIONS; TRANSPORTING
Y02E60/10
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B29C70/86
PERFORMING OPERATIONS; TRANSPORTING
B29C70/48
PERFORMING OPERATIONS; TRANSPORTING
H01M2220/20
ELECTRICITY
B62D29/04
PERFORMING OPERATIONS; TRANSPORTING
B29C70/086
PERFORMING OPERATIONS; TRANSPORTING
B62D25/14
PERFORMING OPERATIONS; TRANSPORTING
B29C70/543
PERFORMING OPERATIONS; TRANSPORTING
International classification
B29C70/48
PERFORMING OPERATIONS; TRANSPORTING
B29B11/16
PERFORMING OPERATIONS; TRANSPORTING
B29C70/08
PERFORMING OPERATIONS; TRANSPORTING
B29C70/38
PERFORMING OPERATIONS; TRANSPORTING
B29C70/54
PERFORMING OPERATIONS; TRANSPORTING
B62D25/14
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method for producing a part made of a composite material having an organic matrix and a fibrous reinforcement, the method comprising the following steps: a) automatically draping, either in a planar arrangement or shaped over a three-dimensional cavity, at least one lamination (30, 31) comprising at least a first and second different dry plies, at least partially stacked to form a dry, planar or three-dimensional preform, each ply being fibrous and the plies mutually differing in terms of their structure, their positioning on the preform, the fibres composing them and/or the geometry of the ply, wherein at least one ply is laid in a non-woven form and has a plurality of unidirectional fibre layers laid on top of each other with a different angular orientation of the fibres, and/or at least one ply is woven; b) thermoforming the preform, the thermoforming step taking place, when the preform has been draped in a planar arrangement in step a), in a three-dimensional cavity of a first mold to impart a three-dimensional shape thereto; and c) impregnating, with at least one polymer, the preform thus thermoformed inside a mold, the preform being moved, if it is draped in a planar arrangement in step a), from the first thermoforming mold to a second mold for the impregnation step.
Claims
1. A method for producing a part made of composite material having an organic matrix and fiber reinforcement for battery, said method comprising the following steps: a) automatically draping, either flat or shaped on a three-dimensional mold cavity, at least one layered structure comprising at least one first and one second different dry plies, at least partially superposed, so as to form a dry preform, either flat or three-dimensional, each ply being fibrous, the plies differing from one another in structure, positioning on the preform, the fibers of which they are constituted and/or the geometry of the ply, the positioning of the plies relative to one another being defined so as provide at least one zone, having a function, between the plies, b) thermoforming the preform, thermoforming being carried out, when it was draped flat in step a), in a three-dimensional cavity of a first mold in order to give it a three-dimensional shape, c) impregnating, within a mold, the preform thus thermoformed with at least one polymer, the preform being moved, in the case of draping flat in step a), from the first thermoforming mold to a second mold for impregnation.
2. The method as claimed in claim 1, each ply being in the form of a structure selected from the group consisting of a linear structure, a surface structure, or multidirectional.
3. The method as claimed in claim 1, comprising a step consisting of placing at least one core on at least one part of the layered structure, said at least one core, having a total external surface area less than that of at least one of the plies so that only certain predetermined zones of the layered structure are covered.
4. The method as claimed in claim 3, comprising the step of draping a second layered structure comprising at least one ply in order to cover the core and the layered structure at least partially.
5. The method as claimed in claim 1, in which said at least one zone having a function is a cavity for circulation of a fluid within the finished part and/or said at least one zone having a function being a cavity or a projection of suitable geometry, able to receive an element that is to be combined with the final part.
6. The method as claimed in claim 1, in which at least one ply of carbon-fiber fabric is used for supplying a function of conduction or dissipation of heat.
7. The method as claimed in claim 1, in which at least one sensor is inserted in the preform.
8. A battery comprising at least one part made of composite material produced by the method as claimed in claim 1, comprising at least one or projection of suitable geometry, able to receive at least one electric battery.
9. The battery according to claim 8, wherein said at least one zone having a function is a cavity for circulation of a fluid within the finished part in order to allow the cooling of the battery.
10. The battery according to claim 9, comprising at least one ply of carbon-fiber fabric for supplying a function of conduction or dissipation of heat,
11. The battery according to claim 10, wherein the carbon fibers are obtained from PAN (polyacrylonitrile) or from biosourced precursors.
12. The method according to claim 5, wherein said at least one zone having a function is a cavity or a projection of suitable geometry able to receive an element that is to be combined with the final part, wherein the cavity or cavities are sites of the male or female type for receiving batteries.
13. The method according to claim 12, wherein the cavities comprise 30 to 50 cells approximately vertically for a battery with a length of one meter.
14. The battery according to claim 8, wherein said at least one zone having a function is a cavity for circulation of a fluid within the finished part in order to allow the cooling of the battery.
15. The method according to claim 6, wherein the carbon fibers are obtained from PAN (polyacrylonitrile) or from biosourced precursors.
16. The method according to claim 13, wherein at least one ply of precursor fabric that has undergone a carbonization step is used.
Description
FIGURES
[0107] The invention may be better understood on reading the description given hereunder, of nonlimiting embodiment examples of the invention, and on examining the appended drawing, in which:
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DETAILED DESCRIPTION
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[0131] The steering column support 1, in this example, is made of composite material having an organic matrix, according to the method of production described below.
[0132] The column support 1 comprises an upper part 2 made of composite material having an organic matrix, in this example having a sandwich structure at least partially, configured for holding the steering column C at the front 3. As can be seen in
[0133] The support 1 also comprises, in the prolongation of part 7, in this example, a lower part 8 in the approximate shape of a curved cross, arranged for carrying the pedal bracket, as can be seen in
[0134] The drawing also shows a windshield recess lower crossmember 5 according to an embodiment example, shown in
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[0136] Moreover, compared to assemblies made from metal parts, a smaller number of parts is required to fulfill the same functions.
[0137] The windshield recess lower crossmember 5 is made of a composite material having an organic matrix, in this example partially as a sandwich structure incorporating one or more cores on some or all of its length. As can be seen in
[0138] As can also be seen in
[0139] For its part, the lower part 8 is fixed to the metal bulkhead T of the vehicle, as shown in particular in
[0140] In this example, the windshield recess lower crossmember 5 has a fixing part 15 with a sandwich structure matching the shape of the column support 1 at the back 4 of its upper part 2. This fixing part 15 is approximately vertical. The windshield recess lower crossmember 5 further comprises an approximately horizontal upper part 19, in the prolongation of the flat portion 6 of the upper part 2, as well as a reinforced portion with a sandwich structure 22 extending downwards at the back under the vehicle's windshield. The various parts are fixed and assembled according to the arrows in
[0141] As illustrated in
[0142] Another example of a support 1 and a windshield recess lower crossmember 5 is illustrated in
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[0145] Step b), also illustrated in
[0146] Step c) consists of placement, on a predetermined part of the surface of the layered structure consisting of plies 30 and 31, of a core 32 of foamed polyethylene terephthalate. The core or cores 32 may be glued on the layered structure.
[0147] If the core is not made of foamed PET or if there is no core, this will still be within the scope of the invention. Any other material suitable for the method may be used, including a metal insert, for example made from formed or cast sheets, so as to have a function appropriate to the application: material for damping, strength, sound or heat insulation, conductive or insulating material for example.
[0148] The next step d) consists of flat draping of a second layered structure once again comprising a deformable dry ply 33 corresponding to ply 31, at least in shape.
[0149] In a step e), a deformable dry ply 34, identical at least in shape to ply 30, is draped flat, forming the second layered structure with ply 33. The relative flexibility of the core does not interfere with the draping of these plies 33 and 34. According to a variant embodiment, the plies 33 and 34 making up the second layered structure are stabilized on the preform by thermal activation of a polymer, for example a thermoplastic polymer, dusted on said plies, or by spraying of glue.
[0150] In this step e), it can clearly be seen that one part, in the present case the upper part 2 of the column support 1, is made as a sandwich structure whereas the other part, namely the lower part 8 of the column support 1, is made in one piece with the upper part 2 but without the core and therefore the sandwich structure.
[0151] In this example the plies 30, 31, 33 and 34 are advantageously nonwoven plies of NCF, with a weight selected so as to obtain the desired stiffness without multiplying the number of plies required. For example, a ply in NCF, used for making the column support 1 or for any other part produced by the method according to the invention, comprises a first layer of carbon fibers oriented at +45, a second layer of aramid fibers oriented at 0, and a third layer of carbon fibers oriented at 45, without this example being limiting or exhaustive. Thus, the nature of the fibers that are draped is adapted to meet the needs of mechanical durability with respect to stresses during use of the part made and the requirements in an exceptional stress situation, such as in the case of an impact or penetration of a foreign body. If the preform comprises for example glass fibers, carbon fibers, kevlar fibers or natural fibers, among others, this will still be within the scope of the invention.
[0152] In a step f), at least one seam 35 of the plies is produced, so as to keep the two layers together. The seam 35, preferably in zigzag, may follow the contour of the core or cores so as to allow separation of the layers on either side of the core or cores, reinforcing this separation zone against peeling. As a variant or additionally, the seam 35 may constitute one or more lines of folding of the preform. The location of the seam 35 is determined for example by experience or by simulation. The seam may be produced by a seaming system bonding the plies together to fix their position. Such a system may have two needles or one curved needle. In both cases, a buffer zone is provided under the preform for receiving the needles. The speed of producing the seam may be about 1400 stitches/min, or about 10 cm/s.
[0153] In a variant embodiment that is not shown, the seam or seams under most stress are covered with bands of unidirectional fibers, for example of carbon fibers, in order to reinforce them. The fibers of said bands are oriented approximately parallel to the general direction of progression of the seams that they cover.
[0154] A flat dry preform 36 is then obtained. As illustrated in
[0155] The thermoformed preform 37 thus obtained is then moved into a second mold, not visible in the figures, in which it is impregnated with at least one polymer in order to produce the part, shown in
[0156] The polymer used for impregnation may be a thermosetting or thermoplastic resin.
[0157] According to an embodiment example that is not illustrated, the second mold comprises two parts and sealing means so that, when the mold is closed, said two parts define a sealed cavity in which the dry preform is located. The mold comprises means for vacuuming said cavity, and according to one embodiment example, means for heating each part of the mold. According to various embodiment examples, the two parts of the mold are heated by circulation of a fluid, by electric resistances or by induction. When the preform is under vacuum in the mold cavity, channels allow a polymer to be injected into the preform, so as to impregnate it. This injection is carried out at a temperature appropriate to the polymer used. Injection may be carried out at high pressure, for example of about 30 bar, and at high temperature, notably between 120 C. and 180 C. The mold may be made of metal, notably steel. According to one embodiment example, polymers of different nature are injected into the upper part and into the lower part of the mold and/or in specific zones of the upper and/or lower parts, in order to confer suitable properties on the part as a function of the stressing to which it is subjected.
[0158] After consolidating the part 1 by solidification of the polymer when it is a thermoplastic polymer or by baking the polymer when it is a thermosetting polymer, the part 1 is removed from the mold. Simple deburring, not machining, may be carried out to finish the part 1.
[0159] With such a method, the rate for production of one part may be less, in cumulative time, than 200 s, the steps of draping and of impregnation, notably injection, each requiring 90 s.
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[0161] An installation D for carrying out the method in
[0162] A robot R1 performs the flat draping automatically. A second robot R2, visible in
[0163] In the third zone 47, besides a robot R3 arranged for moving the thermoformed preforms to the third zone 47, tooling O including the mold for impregnation, notably by injection, of polymer into the preform is shown. In this example the tooling is an injection device such as a press.
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[0165] The method for producing the latter is illustrated in
[0166] In step m), second plies 52, constituting reinforcement, are positioned on certain zones of the first ply 51. These plies 52 are for example made of carbon fiber cloth.
[0167] Then, in step n), cores 53, numbering two in this example, are positioned on a part of the first layered structure 51, in the present case on plies 52.
[0168] In step o), a second layered structure 54, comprising in this example a deformable dry ply of NCF, is produced automatically using the rollers S. It should be noted that plies 52 were also deposited beforehand above the cores 53, as can be seen in this step o).
[0169] A preforming step, or thermoforming step, at low pressure, of the order of 1 bar, and at low temperature, below 100 C., is carried out after step o), in a simple mold, for example of aluminum or of composite material having an organic matrix, or of resin, or some other.
[0170] The three-dimensional preform 55 obtained is shown in perspective in
[0171] In the step illustrated in
[0172] It should be noted that the features described above for the preform, the materials used, the steps of the method as well as the tooling, with respect to
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[0174] An example of tooling that may be used for mold draping is shown in
[0175] With the complete installation illustrated in
[0176] The method, the steps of which are illustrated in
[0177] In particular, such a method may allow high-rate production of any complex parts made of composite material having an organic matrix that may comprise at least one part having a sandwich structure, whether intended for the automotive sector, aeronautical sector or other industrial sectors.
[0178] Other parts produced using the method of the invention are illustrated in
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[0182] It should be noted that the steps of the method according to the invention for producing the preform or preforms may be carried out independently of the final step of impregnation with a polymer in order to produce the part. The dry preforms may be stored in a stack to save storage space. The final step of the method may be carried out subsequently after a time lapse that may be for example from 1 h up to a year. As a variant, all the steps of the method may be carried out successively, without delay, i.e. in less than about 1 h, notably of the order of some minutes at most.