Method in which a vehicle interior trim part with a decor layer comprising paper layers is produced
10131128 ยท 2018-11-20
Assignee
Inventors
Cpc classification
B32B1/00
PERFORMING OPERATIONS; TRANSPORTING
Y10T156/1044
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
B32B37/10
PERFORMING OPERATIONS; TRANSPORTING
B29L2031/30
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B29C70/78
PERFORMING OPERATIONS; TRANSPORTING
B29C45/14336
PERFORMING OPERATIONS; TRANSPORTING
B32B29/005
PERFORMING OPERATIONS; TRANSPORTING
B32B2272/00
PERFORMING OPERATIONS; TRANSPORTING
B29C2793/00
PERFORMING OPERATIONS; TRANSPORTING
B29C44/1228
PERFORMING OPERATIONS; TRANSPORTING
B32B7/12
PERFORMING OPERATIONS; TRANSPORTING
B29C2037/0042
PERFORMING OPERATIONS; TRANSPORTING
B32B3/18
PERFORMING OPERATIONS; TRANSPORTING
B32B38/0004
PERFORMING OPERATIONS; TRANSPORTING
Y10T156/1041
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
B29C45/1418
PERFORMING OPERATIONS; TRANSPORTING
B32B5/245
PERFORMING OPERATIONS; TRANSPORTING
B29C70/686
PERFORMING OPERATIONS; TRANSPORTING
Y10T156/1075
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
B29C43/003
PERFORMING OPERATIONS; TRANSPORTING
B32B29/002
PERFORMING OPERATIONS; TRANSPORTING
B26D3/00
PERFORMING OPERATIONS; TRANSPORTING
B32B2307/546
PERFORMING OPERATIONS; TRANSPORTING
B32B29/02
PERFORMING OPERATIONS; TRANSPORTING
International classification
B32B37/02
PERFORMING OPERATIONS; TRANSPORTING
B32B37/10
PERFORMING OPERATIONS; TRANSPORTING
B29C43/00
PERFORMING OPERATIONS; TRANSPORTING
B32B7/12
PERFORMING OPERATIONS; TRANSPORTING
B29C45/14
PERFORMING OPERATIONS; TRANSPORTING
B26D3/00
PERFORMING OPERATIONS; TRANSPORTING
B32B38/00
PERFORMING OPERATIONS; TRANSPORTING
B32B38/10
PERFORMING OPERATIONS; TRANSPORTING
B32B38/04
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method in which an interior trim part for a vehicle is produced. The method includes the steps of providing a block of material comprising a plurality of paper layers connected to each other by at least one resin, cutting the block into slices, wherein a cutting plane has an angle between 5 and 85 in relation to layer planes of the paper layers, providing a flexible support layer and applying at least one of the slices to the flexible support layer to obtain a flexible composite layer, and providing a rigid carrier and applying the flexible composite layer directly or indirectly to the carrier.
Claims
1. Method in which an interior trim part for a vehicle is produced, comprising the steps: providing a block of material comprising a plurality of paper layers connected to each other by at least one resin; cutting the block into slices along a cutting plane that has an angle between 5 and 85 in relation to layer planes of the paper layers, wherein the block is cut with a cutting tool, wherein the cutting tool cuts each paper layer by contacting the paper layer on a first side, then passes through the paper layer and leaves the paper layer again on a second side, wherein the first side of each of the paper layers has a surface normal facing out of the slice to be cut; providing a flexible support layer and applying at least one of the slices to the flexible support layer to obtain a flexible composite layer; and providing a rigid carrier and applying the flexible composite layer directly or indirectly to the carrier.
2. Method according to claim 1, wherein the block of material provided comprises a content of resin which is higher than 10 wt % of a total weight of the block of material and/or a content of cellulose, lignin or a mixture thereof which is lower than 90 wt % of a total weight of the block of material.
3. Method according to claim 1, wherein the flexible composite layer is laminated onto the rigid carrier.
4. Method according to claim 1, wherein the carrier is provided and connected to the flexible composite layer in one integral step.
5. Method according to claim 4, wherein the carrier is provided and connected to the flexible composite layer by back injecting a plastic material into a mold and into contact with the composite layer.
6. Method according to claim 1, further comprising the step of smoothing a surface of the slices.
7. Method according to claim 1, wherein the slice cut from the block of material is smoothed after it has been applied to the flexible support layer.
8. Method according to claim 7, wherein the slice of the block of material is smoothed after the composite layer has been applied to the carrier.
9. Method according to claim 1, wherein the block of material is cut into slices which comprise a thickness of less than 2 mm.
10. Method according to claim 9, wherein the thickness is less than 1.5 mm.
11. Method according to claim 10, wherein the thickness is less than 1 mm.
12. Method according to claim 1, wherein the block of material is provided by soaking multiple paper layers with resin and pressing the multiple paper layers together.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The invention is further described in connection with the figures of which:
(2)
(3)
(4)
(5)
(6)
(7)
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DETAILED DESCRIPTION OF THE ILLUSTRATED EMBODIMENT(S)
(9)
(10) Although in
(11) A block of material produced as described above in connection with
(12) In
(13) In a subsequent step of the method, the block of material is cut into slices.
(14)
(15) After slicing, the slices 8, 9, which are very fragile, are applied to a flexible support layer 10. In this embodiment, the slices 8, 9 are laminated to the flexible support layer 10; however, other methods for applying the slices to the flexible support layer could be used instead. In order to laminate the slice of material onto the support layer, a hot melt polyurethane can be applied to the slice of material, and the latter can be heated to 120 C. and pressed against the support layer with a pressure of 5 bar. Without the flexible support layer, the fragility of the slices 8, 9 would render them not usable in vehicle interior trim parts. However, a composite layer 11 formed from the flexible support layer 10 and the slice of material 8 is less fragile and can be bent into a desired shape.
(16) The flexible composite layer 11 comprising the slice of material of
(17) In a further method step, the flexible composite layer 11 is attached to a rigid carrier to form a vehicle interior trim part. In a first embodiment of this method step, the flexible composite layer 11 is introduced into a press 12 comprising an upper die 13 and a lower die 14. The dies 13, 14 have a shape corresponding to a desired shape of a vehicle interior trim part to be produced. In addition to the flexible composite layer 11, a rigid carrier 15 and, optionally, an intermediate layer 16 are introduced into the press 12. The press 12 with the flexible composite layer 11, the rigid carrier 15 and the intermediate layer 16 is shown in
(18) In an alternative embodiment (not shown), the flexible composite layer 11 may be applied directly onto the rigid carrier 15 without an intermediate layer 16 in between.
(19) According to a further embodiment of the method, the flexible composite layer 11 as well as the rigid carrier 15 are introduced into a foaming tool 17 such that a cavity 18 is formed between the flexible composite layer 11 and the rigid carrier 15. Into this cavity 18 a foaming material may be introduced in order to form a foam layer. The foam layer hardens and connects the flexible composite layer 11 to the rigid carrier 15. The foaming tool 17 with the flexible composite layer 11 and the rigid carrier is shown in
(20) In a further embodiment of the method, the flexible composite layer 11 is introduced into a mold 19 for injection molding such that a cavity 20 is delimited by the mold 19 and the flexible composite layer 11. A plastic material is injected into the cavity 20. The plastic material, after hardening, forms a rigid carrier. The plastic material may be hot at the time it is injected into the cavity 20. The heat of the plastic material may soften the flexible composite layer 11 and thus may ease the deformation of the latter into the desired final shape. The mould 19 for injection molding together with the flexible composite layer is shown in
(21) With help of
(22) In the top right part of
(23) By contrast, advancing the second saw 23 in direction 24 would possibly provide an undesirable result. The surface normal 27 of the first side 25 faces towards the inside of the slice of material 8. If the saw 23 is bent by a force caused by the contact with the first side 25, the saw 23 possibly damages the slice 8. Therefore, the cutting direction is preferably chosen such that the surface normal 27 of the first side 26 faces out of the slice 8 to be produced.
(24) While both situations, cutting in the direction 24 or in the direction 23 is possible, a preferred embodiment is cutting in the direction 24. This is illustrated by angle between the cutting plane along direction 24 and a layer plane of paper 4, where is around 10 in the shown embodiment. The angle in this embodiment is defined as the angle between the cutting plane and the paper plane in a clockwise direction, when the cutting direction is from the right to the left and in a counter-clockwise direction, when the cutting direction is from the left to the right. It can be easily seen that shown angle , between the cutting plane and the layer plane of the paper when cutting along direction 24 (from right to left) is measured clockwise. Cutting from direction 23 corresponds to a counter-clockwise angle of around 170 when keeping the orientation of the paper layers 4 and 4, but cutting from left to right.