INTERIOR TRIM PART AND METHOD OF MANUFACTURING THE SAME
20170361782 · 2017-12-21
Inventors
Cpc classification
B32B2255/28
PERFORMING OPERATIONS; TRANSPORTING
B32B1/00
PERFORMING OPERATIONS; TRANSPORTING
C04B35/19
CHEMISTRY; METALLURGY
B32B27/06
PERFORMING OPERATIONS; TRANSPORTING
C23C28/00
CHEMISTRY; METALLURGY
C08J2400/00
CHEMISTRY; METALLURGY
B44C3/10
PERFORMING OPERATIONS; TRANSPORTING
B32B5/18
PERFORMING OPERATIONS; TRANSPORTING
B32B37/12
PERFORMING OPERATIONS; TRANSPORTING
B32B7/12
PERFORMING OPERATIONS; TRANSPORTING
B32B9/005
PERFORMING OPERATIONS; TRANSPORTING
B05D5/06
PERFORMING OPERATIONS; TRANSPORTING
C23C24/10
CHEMISTRY; METALLURGY
C08J5/12
CHEMISTRY; METALLURGY
B60R13/02
PERFORMING OPERATIONS; TRANSPORTING
B29C65/48
PERFORMING OPERATIONS; TRANSPORTING
B23K35/286
PERFORMING OPERATIONS; TRANSPORTING
B32B3/10
PERFORMING OPERATIONS; TRANSPORTING
B32B15/20
PERFORMING OPERATIONS; TRANSPORTING
B32B5/02
PERFORMING OPERATIONS; TRANSPORTING
C04B35/195
CHEMISTRY; METALLURGY
B32B15/14
PERFORMING OPERATIONS; TRANSPORTING
B32B2260/021
PERFORMING OPERATIONS; TRANSPORTING
B29C66/7422
PERFORMING OPERATIONS; TRANSPORTING
B23K35/0244
PERFORMING OPERATIONS; TRANSPORTING
International classification
B60R13/02
PERFORMING OPERATIONS; TRANSPORTING
B32B7/12
PERFORMING OPERATIONS; TRANSPORTING
C04B35/195
CHEMISTRY; METALLURGY
B29C65/48
PERFORMING OPERATIONS; TRANSPORTING
B32B9/00
PERFORMING OPERATIONS; TRANSPORTING
B29C65/00
PERFORMING OPERATIONS; TRANSPORTING
C04B35/19
CHEMISTRY; METALLURGY
C08J5/12
CHEMISTRY; METALLURGY
C04B35/622
CHEMISTRY; METALLURGY
Abstract
A process for producing an interior trim part (1) with a decorative layer situated on a first side (S1) thereof and forming a decorative pattern (M) for the interior of a motor vehicle, the process comprising the following steps: (a) formation of at least one cutout configuration (R), defined by a predetermined decorative pattern (M), in a protective layer (120) situated on a first side (S1), which is situated on a first surface (110a) of the shell-shaped base body (110) made of a metallic material, (b) deposition of sinterable decorative material on the first side (S1) in such a way that the decorative material, as an intermediate layer (150), covers at least the area in which the cutout configuration (R) defined by the decorative pattern (M) is formed in the protective layer (120), (c) laser-sintering of the intermediate layer (150) inside the at least one cutout configuration defined by the decorative pattern (M), (d) removal of the sinterable decorative material that is situated outside the at least one cutout configuration defined by the decorative pattern (M),
as well as an interior trim part (1).
Claims
1. A process for producing an interior trim part with a decorative layer situated on a first side thereof and forming a decorative pattern for the interior of a motor vehicle, the process comprising the following steps: (a) forming at least one cutout configuration, defined by a predetermined decorative pattern, in a protective layer situated on a first side, which is situated on a first surface of the shell-shaped base body made of a metallic material, (b) depositing a sinterable decorative material on the first side in such a way that the decorative material, as an intermediate layer, covers at least the area in which the cutout configuration defined by the decorative pattern is formed in the protective layer, (c) laser-sintering the intermediate layer inside the cutout configuration defined by the decorative pattern in order to produce at least one hardened portion of the intermediate layer situated inside said cutout configuration, (d) removing the sinterable decorative material that is situated outside the cutout configuration defined by the decorative pattern, so that the at least one hardened portion of the intermediate layer and the protective layer outside the latter form the decorative layer with the predetermined decorative pattern.
2. The process according to claim 1, wherein the formation of the cutout configuration in the protective layer defined by a predetermined decorative pattern is produced by vaporization of the material of the protective layer according to a predetermined pattern.
3. The process according to claim 1, wherein the sinterable decorative material contains a mineral substance.
4. The process according to claim 1, wherein a dispersion of sinterable decorative material takes place when sinterable decorative material is deposited on the first side.
5. The process according to claim 1, wherein the sinterable decorative material is deposited on the first side in powder form.
6. The process according to claim 1, wherein the base body is formed from or comprises aluminum or an aluminum alloy.
7. The process according to claim 1, wherein an application of a plastic reinforcement takes place on the second surface of the base body, wherein the application of the plastic reinforcement takes place in particular by adhesive bonding thereof and an adhesive layer is applied between the second surface of the base body and the plastic reinforcement.
8. The process according to claim 1, wherein an application of a plastic reinforcement takes place on the second surface of the base body, wherein, by back-molding of the base body at the second surface thereof, the plastic reinforcement is applied thereon.
9. An interior trim part, comprising: a shell-shaped base body made of a metallic material, a protective layer, which is situated on a first surface of the shell-shaped base body, wherein at least one cutout configuration defining a decorative pattern is formed in the protective layer, and a decorative material layer made of a sintered material, which at least partially fills the cutout configuration in the protective layer.
10. The interior trim part according to claim 9, wherein the material of the decorative material layer is a mineral material.
Description
[0038] Embodiments of the invention are described below with the aid of the appended figures, in which:
[0039]
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[0044]
[0045]
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[0050] According to the process according to the invention, an interior trim part 1 with a decorative layer situated at a first side S1 thereof and forming a decorative pattern M is produced for the interior of a motor vehicle. The interior trim part can for example be a door panel for application on the side of the vehicle door facing the interior, an instrument panel or an armrest.
[0051] A shell-shaped base body 110 made of a metallic material, which extends in a planar manner, is used for interior trim part 1 produced according to the process according to the invention. The planar extension of base body 110 is constituted by first surface 110a and a second surface 110b situated opposite to first surface 110a. First surface 110a is situated at a first side S1 of base body 110. A first side S1 and a second side S2 of interior trim part 1 are defined for the subsequent description, wherein first surface 110a is situated facing first side S1 and second surface 110b is situated facing second side S2. Shell-shaped base body 110 preferably has in its main area the shape of interior trim part 1 to be produced, apart from further layers to be deposited on base body 110 in the production of interior trim part 1. If need be, base body 110 can however also be further shaped or processed.
[0052] The base body 110 can have a thickness between 0.1 mm and 10 mm, preferably up to 5.0 mm and in particular a thickness between 0.1 mm and 2.0 mm. The base body 110 is formed from a metallic material or comprises a metallic material. In particular, provision can be made such that base body 110 is formed from or comprises aluminium or an aluminium alloy.
[0053] A protective layer 120 is situated on first surface 110a of shell-shaped base body 110. Provision can be made such that protective layer 120 extends over entire first surface 110a. Provision can also be made such that protective layer 120 extends only over a part, i.e. in sections, over first surface 110a. The material of base body 110 can be a metal, in particular aluminium or at least in part an oxide of a metal and in particular aluminium oxide. Base body 110 can be formed from or comprises a basic body and a surface layer covering the latter, wherein the material basic body is made of metal and in particular aluminium and the surface layer is made of an oxide of a metal and, when the material basic body is formed from aluminium, of an aluminium oxide. In particular, provision can be made such that the surface layer constitutes surface 110a. The surface layer can cover the basic body in sections or completely.
[0054] The protective layer is formed from or comprises plastic, e.g. is formed from or comprises a UV hardened lacquer of urethane acrylate.
[0055] A further step can optionally be provided, wherein a plastic reinforcement 130 is applied as a layer and in particular in a planar manner on second surface 110b of shell-shaped base body 110 for the formation of intermediate product Z1. Alternatively, provision can for example be made such that a rib-shaped plastic reinforcement 130 is applied to second surface 110b of shell-shaped base body 110. According to an embodiment, provision can be made such that plastic reinforcement 130 only partially covers second surface 110b. In the state shown in FIG. 3, plastic reinforcement 130 is applied as a layer and in a planar manner to second surface 110b of base body 110.
[0056] Plastic reinforcement 130 can serve to stabilise and in particular to increase the strength of shell-shaped base body 110.
[0057] Plastic reinforcement 130 can for example be constituted as a layer, which covers second surface 110b in a planar manner or covers a main area thereof. Plastic reinforcement 130 can also be formed from a plurality of strips.
[0058] The plastic reinforcement can be a plastic with or without additives and for example a thermoplastic or a foam. The plastic reinforcement can also be a fibre-reinforced plastic.
[0059] The application of plastic reinforcement 130 to second surface 110b can take place by adhesive bonding.
[0060] According to the invention, a process step represented in
[0061] In the embodiment shown in
A cutout portion arises by the planar removal of material of protective layer 120 up to first surface 110a of base body 110. Provision can in particular be made such that the surface-portion configuration of surface 110a laid bare by cutout configuration R is the surface of the surface layer made of an oxide of a metal and, in the case of the formation of the material basic body from aluminium, of an aluminium oxide.
[0062] The planar removal can take place by vaporisation of the material of the protective layer in a predetermined decorative pattern. Vaporisation of the material of the protective layer is preferred, because with this process step it can be ensured in a particularly reliable manner that no residual material will remain on the surface of the base body inside the cutout configuration. The material is preferably vaporised with a laser. Vaporisation is understood here also to mean sublimation or ablation or a combination of sublimation and ablation. The cross-sectional representation shown in
[0063] Cutout configuration R—viewed in cross-section along the extension thereof—is formed in particular by lateral faces RS, which are each formed from protective layer 120 and which lie facing one another, and a bottom face RB which border cutout RA open towards first side S1. Bottom face RB is formed by a portion of first surface 110a (
[0064]
[0065] According to the invention, provision is made such that a deposition of sinterable material as a decorative-material intermediate layer 150 on first side S1 takes place in a subsequent step, in such a way that decorative material D as intermediate layer 150 at least covers the area in which cutout configuration R defined by decorative pattern M is formed in protective layer 120.
[0066] In particular, provision can be made such that a deposition of a dispersion of sinterable decorative material as a decorative-material intermediate layer 150 at first side S1 takes place in a subsequent step, in such a way that the dispersion as an intermediate layer 150 at least covers the area in which cutout configuration R defined by decorative pattern M is formed in protective layer 120.
[0067] Provision can be made such that intermediate product Z3 with base body 110, with mineral intermediate layer 150 and with plastic reinforcement 130 lies on a workpiece holding fixture H.
[0068] In this process step, provision can be made such that the sinterable decorative material is present in powder form and is introduced in powder form into cutout configuration R.
[0069] Alternatively, provision can be made such that the sinterable decorative material is present and deposited as a dispersion, e.g. as a binder dissolved in a solvent with decorative material in powder form introduced into the latter. A spraying device 155 is shown in this regard in
[0070] The decorative material is sinterable in particular inasmuch as it can be hardened by heat input, in particular by means of a laser beam. Provision can be made such that base body 110 or plastic reinforcement 130 is held and fixed by a holding fixture H.
[0071] Layer 150 of decorative material comprises an outer surface 150a facing first side S1 and can be deposited relatively thinly. The thickness of the deposited layer can in particular lie in the range between 1 and 500 μm especially—viewed in the extension of intermediate product Z3—outside cutout configuration R. In particular, the thickness of the deposited layer can lie between 20 and 100 μm.
[0072] The decorative material, in particular the powdery decorative material, can comprise one or more of the following components or can comprise each of them respectively: ceramic powder, plastic, moulding sand, metal powder, polyurethane for example in particle form or in droplet form.
[0073] Furthermore, provision can be made such that the decorative material is deposited by spraying or by mechanical deposition.
[0074] In a further step, laser sintering of this decorative-material intermediate layer 150 takes place by means of at least one laser jet L1 of a laser device L (
[0075] The same laser is preferably used for the sintering as for the removal of the protective layer material. A resolution of better than 30 μm can be achieved by this process step.
[0076] In a further process step, removal of non-hardened portions 190 (