Manufacturing method of a component of automotive vehicle equipment and associated component of equipment
11001017 · 2021-05-11
Assignee
Inventors
Cpc classification
B29C70/545
PERFORMING OPERATIONS; TRANSPORTING
B29C70/46
PERFORMING OPERATIONS; TRANSPORTING
B29L2031/30
PERFORMING OPERATIONS; TRANSPORTING
International classification
B29C70/54
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A manufacturing method for an automotive vehicle component that includes the steps of: arranging at least a first skin capable of solidifying on a first half-mold of a mold; closing a second half-mold of the mold to form the first skin; then solidifying the first skin in the molding cavity defined between the first half-mold and the second half-mold. The second half-mold has a piercing element with at least one point-shaped end, and the method includes piercing by the piercing element of at least one through-hole in the first skin before solidification of the first skin.
Claims
1. A method of manufacturing a component of automotive vehicle equipment, the method comprising: arranging at least a first skin capable of solidifying on a first half-mold of a mold; closing a second half-mold of the mold to shape the first skin in a molding cavity defined between the first-half mold and the second-half mold; solidifying the shaped first skin in the molding cavity, the second half-mold comprising a piercing element having at least one point-shaped end, wherein the method comprises piercing by the piercing element of a through-hole at least in the first skin before the solidification of the first skin; and piercing an additional hole through a second skin and a spacer in an additional mold, wherein the shaped first skin is arranged on the spacer so that the additional hole faces the through hole.
2. A method according to claim 1, wherein the first skin comprises a matrix of polymer and fibers embedded in the matrix, wherein the matrix is fluid during the through-hole piercing, and wherein the matrix solidifies around the piercing element after the through-hole piercing.
3. A method according to claim 2, wherein the piercing element displaces the fibers contained in the matrix at a periphery of the piercing element.
4. A method according to claim 3, wherein the following steps are performed after the step of piercing the first skin: introducing the spacer and second skin between a first additional half-mold and a second additional half-mold of the additional mold, wherein the second additional half-mold is provided with an additional piercing element in the shape of a point, piercing the additional hole through the second skin and the spacer by the additional piercing element; and assembling the first skin on a first face of the spacer located opposite a second face of the spacer on which the second skin is attached, wherein the additional hole extends opposite the through hole.
5. A method according to claim 2, wherein the following steps are performed after the step of piercing the first skin: introducing the spacer and second skin between a first additional half-mold and a second additional half-mold of the additional mold, wherein the second additional half-mold is provided with an additional piercing element in the shape of a point, piercing the additional hole through the second skin and the spacer by the additional piercing element; and assembling the first skin on a first face of the spacer located opposite a second face of the spacer on which the second skin is attached, wherein the additional hole extends opposite the through hole.
6. A method according to claim 1, wherein the spacer is a honeycomb spacer, wherein the first skin is arranged on a first face of the honeycomb spacer during the piercing in the additional mold, and wherein a piercing element of a second additional half-mold of the additional mold passes through the spacer and into the through hole during the additional hole piercing step.
7. A method according to claim 6, wherein the second skin is arranged on a second face of the spacer, and wherein the piercing element of the second additional half-mold pierces the second skin before piercing the spacer during the additional hole piercing step.
8. A method according to claim 1, wherein the following steps are performed after the step of piercing the first skin: introducing the spacer and second skin between a first additional half-mold and a second additional half-mold of the additional mold, wherein the second additional half-mold is provided with an additional piercing element in the shape of a point, piercing the additional hole through the second skin and the spacer by the additional piercing element; and assembling the first skin on a first face of the spacer located opposite a second face of the spacer on which the second skin is attached, wherein the additional hole extends opposite the through hole.
9. A method according to claim 1, comprising placing an insert in the through hole.
10. A method according to claim 9, wherein the insert is a socket.
11. A method according to claim 9, wherein the spacer is a honeycomb spacer and wherein the insert is mounted through the through hole and the additional hole.
12. A method according to claim 11, wherein the insert comprises at least one outer retaining protuberance of the insert inserted into the spacer and/or in the first skin.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The invention will be better understood upon reading the description which follows, given solely by way of nonlimiting example and with reference to the appended drawings, in which:
(2)
(3)
(4)
(5)
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(9)
DETAILED DESCRIPTION OF THE ILLUSTRATED EMBODIMENTS
(10)
(11) The component of automotive vehicle equipment 10 comprises a composite panel 12, and a fixing element 14 that is mounted in the composite panel 12.
(12) The composite panel 12 has a “sandwich” type structure, comprising a first face 16 and an opposite second face 18.
(13) More specifically, the composite panel 12 comprises a first skin 20 and a second skin 22, respectively defining the first face 16 and the second face 18 of the composite panel 12. The composite panel 12 further comprises a spacer 23 interposed between the two skins 20, 22.
(14) More particularly, the first skin 20 is fixed on a first face 24 of the spacer 23, and the second skin 22 is fixed on a second face 25 opposite the first face 24 of the spacer 23.
(15) The spacer 23 is preferably based on a cellular or honeycomb structure. Thus, the spacer 23 has a plurality of walls 26 that are substantially perpendicular to the faces 16, 18 of the panel 12. The walls 26 define central spaces with a closed contour forming the honeycomb. The honeycomb defines, for example, polygonal meshes, in particular hexagonal meshes.
(16) The spacer 23 is advantageously made of a light material, such as paper or cardboard. The density of the spacer 23 is preferably less than 1500 g/m.sup.2 and is substantially between 200 g/m.sup.2 and 1200 g/m.sup.2.
(17) Each skin 20, 22 has a greater density, and preferably a lower thickness, with respect to the density and the thickness of the spacer 23.
(18) Each skin 20, 22 comprises reinforcing fibers 28 bonded to one another by a polymer matrix 30. The reinforcing fibers 28 are, for example, chosen from carbon fibers, ceramic fibers such as glass fibers, or even cellulosic fibers of natural origin such as flax fiber, hemp, kenaf or jute.
(19) According to a first embodiment, the polymer matrix 30 is a thermosetting matrix, notably comprising one or more unsaturated polyesters.
(20) According to a second embodiment, the polymer matrix 30 is a thermoplastic matrix, comprising, in particular, one or more materials chosen from polyamides (PA), polyethylenes (PE), polypropylenes (PP) and polyesters such as poly(ethylene terephthalate) (PET).
(21) In the embodiment of
(22) The fixing element 14 is arranged along an axis 32 through the first skin 20, the spacer 23 and the second skin 22. In the component of automotive vehicle equipment 10 visible in
(23) The fixing element 14 is inserted into a through hole 34 formed through the first skin 20, the spacer 23 and the second skin 22.
(24) In this example, the fixing element 14 is a socket that is advantageously threaded and designed to receive an insert on the composite panel 12.
(25)
(26) The first half-mold 40 and the second half-mold 42 are movable relative to each other between an open position for assembling/disassembling the two half-molds and a closed molding position.
(27) The first half-mold 40 has a first molding face 46. It defines an orifice 48 which opens into the first face 46.
(28) The second half mold 42 has a second molding face 50 opposite the first face 46. It comprises a piercing element 52 fixed on the second face 50 facing the orifice 48. The piercing element 52 protrudes from the second face 50.
(29) The piercing element 52 is designed to be received in the orifice 48 in the closed molding position.
(30) In this position, the piercing element 52 is able to pierce at least the first skin 20. Advantageously, the piercing element 52 is able to pierce the first skin 20, the spacer 23, and the second skin 22.
(31) The piercing element 52 has, for example, the form of a point at its free end 54.
(32) The piercing element 52 here has a body of circular shape. In a variant, the body of the piercing element 52 has a slot shape, to provide a quarter-turn type fixing.
(33)
(34) The piercing member 52 has pierced the first skin 20, the second skin 22, and the spacer 23. At least a portion of the piercing member 52 enters the orifice 48.
(35) The manufacturing process of a component 10 will now be described according to a first embodiment which concerns thermoplastic matrices.
(36) First, a mold 38 as described above is provided and is placed in the open position.
(37) The first skin 20 is heated in a heating station to bring the matrix 30 into a fluid state, as shown in
(38) Then, the first skin 20 is deposited on the first face 46 of the first half-mold 40.
(39) Then, the spacer 23 is placed on the first skin 20, while the first face 24 of the spacer 23 is placed in contact with the first skin 20.
(40) The second skin 22 is heated in the heating station to bring the matrix 30 into the fluid state. The second skin 22 is then disposed on the second face 25 of the spacer 23.
(41) In a variant, the two skins 20, 22 and the spacer 23 previously superimposed are assembled and then placed between two heating plates in order to simultaneously heat the two skins 20, 22 and thus cause the fusion of the reinforcing fibers 28.
(42) Then, the mold 38 is moved to its closed position. The height of the cavity 44 of the mold 38 between the first half-mold 40 and the second half-mold 42 decreases, wherein the first half-mold 40 and the second half-mold 42 come closer to each other.
(43) The piercing element 52 comes into contact with the second skin 22 and pierces the second skin 22 as it moves with the second half-mold 42.
(44) As the closure of the mold 38 continues, the piercing element 52 completely pierces the second skin 22. As a result, a through hole 34 is formed in the second skin 22.
(45) The piercing element 52 then pierces the spacer 23 and then the first skin 20.
(46) The matrix 30 of the first skin 20 has a fluid state during piercing. As shown in
(47) This avoids embrittlement of the periphery of the hole during its piercing which would be caused by cutting the reinforcing fibers contained in the matrix.
(48) When the mold reaches its closed position, the through hole 34 extends over the entire height of the composite panel 12 and opens through the first face 14 and the second face 25.
(49) The piercing element 52 thus pierces the entire composite panel 12.
(50) In this position, the piercing element 52 enters the orifice 48 of the first half-mold 40. The second half-mold 42 is in direct contact with the second skin 22.
(51) Then, the first skin 20 and the second skin 22 cool in the mold 38. The matrix 30 of each skin 20, 22 solidifies during cooling, and the fibers 28 contained in the matrix 30 are frozen in position in the solidified matrix 30.
(52) After solidification of the first skin 20 and the second skin 22, the mold returns to its open position. The piercing member 52 is withdrawn from the through hole 34, and the panel 12 with the through hole 34 is then removed from the mold 38.
(53) After opening of the mold 38, a retaining insert 56 is mounted in the hole 34 pierced by the piercing element 52.
(54) The retaining insert 56 is, for example, a socket.
(55)
(56) The retaining insert 56 is hollow, and engages around the piercing element 52 before piercing. Internally, it has a shape that is complementary to the shape of the piercing element 52.
(57) The retaining insert 56 advantageously has an outer surface defining notches 57 to lock in translation along the axis 32 in the through hole 34. For example, between the notches 57, the insert 56 comprises at least one external retaining protuberance 58 of the retaining insert 56 inserting into the spacer 23 and/or the first skin 20 and/or the second skin 22 during piercing.
(58) The retaining insert 56 is advantageously internally threaded in order to allow direct screwing of the screws in the through hole 34. As a variant, it has a device for snap-fitting.
(59) The retaining insert 56 is, for example, made by the injection of a plastic material, for example polypropylene (PP) or polyamide (PA) that is rigid enough to allow efficient screwing.
(60) Once the skins have solidified, the solidified skins 20, 22 keep the retaining insert 56 locked in position. The retaining insert 56 remains in the through hole 34 after removal of the piercing element 52.
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(64) The spacer 23 previously glued to ensure perfect adhesion to the skins 20, 22 is placed on the second skin 20. The glue is preferably a glue that is activated at the crosslinking temperature of the resin.
(65) The additional piercing element 66 is designed to pierce an additional hole 68 through the second skin 22 and the spacer 23. It is arranged to face the through hole 34 of the first skin 20.
(66) The piercing method of the first skin 20 is performed in the mold 38 in a manner similar to that described above and will not be repeated here.
(67) Again, since the piercing member 52 acts before the resin is cured, the reinforcing fibers 28 are free to move. The piercing element 52, therefore, spreads them apart without damaging them. Once the resin is crosslinked, the reinforcing fibers 28 are fixed around the piercing element 52 constituting the periphery of the hole. Moreover, as the reinforcing fibers 28 have been pushed aside, they constitute a denser zone and act as a peripheral stiffener.
(68) After piercing, the first skin 20 with the through hole 34 is assembled on a first face 24 of the spacer 23, wherein the first face 24 is located opposite a second face 25 of the spacer 23. The second skin 22 is fixed on the second face 25 of the spacer 23.
(69) The additional hole 68 extends opposite the through hole 34 in the finished component 10.
(70) In a variant, the piercing element 52 is removable and the orifice 48 is able to be filled in order to use the mold 38 without piercing the composite panel 12.
(71) When using at least some embodiments of the invention described above, the weakening of the composite panels due to the cutting of the fibers during their manufacture is greatly reduced. In particular, the perimeter of the openings is not weakened by piercing. Everything ensures good mechanical strength of a part manufactured according to the invention.