PLANAR COMPOSITE MATERIAL
20200238659 ยท 2020-07-30
Assignee
Inventors
Cpc classification
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
D04H1/46
TEXTILES; PAPER
Y10T428/24132
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
B29C70/506
PERFORMING OPERATIONS; TRANSPORTING
B32B27/12
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B5/08
PERFORMING OPERATIONS; TRANSPORTING
B32B38/0012
PERFORMING OPERATIONS; TRANSPORTING
B32B2262/14
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/24091
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
B32B5/10
PERFORMING OPERATIONS; TRANSPORTING
B29C51/145
PERFORMING OPERATIONS; TRANSPORTING
B29C70/02
PERFORMING OPERATIONS; TRANSPORTING
B32B2262/106
PERFORMING OPERATIONS; TRANSPORTING
B32B5/12
PERFORMING OPERATIONS; TRANSPORTING
B32B2250/40
PERFORMING OPERATIONS; TRANSPORTING
B29C70/24
PERFORMING OPERATIONS; TRANSPORTING
B32B2262/02
PERFORMING OPERATIONS; TRANSPORTING
B32B5/06
PERFORMING OPERATIONS; TRANSPORTING
International classification
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B5/08
PERFORMING OPERATIONS; TRANSPORTING
B32B5/10
PERFORMING OPERATIONS; TRANSPORTING
B32B27/28
PERFORMING OPERATIONS; TRANSPORTING
B32B5/12
PERFORMING OPERATIONS; TRANSPORTING
B32B38/00
PERFORMING OPERATIONS; TRANSPORTING
B29C70/50
PERFORMING OPERATIONS; TRANSPORTING
B32B5/06
PERFORMING OPERATIONS; TRANSPORTING
B32B5/02
PERFORMING OPERATIONS; TRANSPORTING
D04H1/46
TEXTILES; PAPER
B29C70/24
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A sheetlike composite material including at least one layer A of a nonwoven thermoplastic fiber web or a thermoplastic film, and at least two unidirectional oriented-fiber layers B and B, the layers B and B having a bidirectional fiber orientation. The layers are not only needled but also stitched to one another.
Claims
1. A method for producing three-dimensional components, or planar semifinished products with a thickness of 0.5 to 5 mm, comprising: (I) for the three-dimensional components, heat pressing in a mold, a thermoformable composite material comprising a) at least one layer A comprising A1 a fiber nonwoven comprising 40 to 100 wt.-% thermoplastic fibers and 60 to 0 wt.-% reinforcing fibers, or comprising, A2 a thermoplastic film, and b) at least two unidirectionally oriented fiber layers B and B comprising parallel reinforcing fiber bundles, wherein at least two layers B and B have different fiber orientations relative to at least one other B or B layer prior to stitching and needling, wherein all layers are stitched together and subsequently needled, the thermoformable composite material being formed by: a) continuously merging together at least one fiber nonwoven layer A1 produced by a carding, airlay or spunbound nonwoven process, with at least two unidirectionally oriented fiber layers B and B, at least one layer B and one layer B having different fiber orientations relative to each other and subsequently stitching the layers to each other and thereafter needling the layers; or: b) continuously merging together at least one thermoplastic film layer A2 with the at least two unidirectionally oriented fiber layers B and B, at least one layer B and one layer B having different fiber orientations relative to each other, stitching the layers to each other and thereafter needling the layers, and (II) for the planar semifinished product, heat pressing in a double band press a thermoformable composite material comprising a) at least one layer A comprising A1 a fiber nonwoven comprising 40 to 100 wt.-% thermoplastic fibers and 60 to 0 wt.-% reinforcing fibers, or comprising, A2 a thermoplastic film, and b) at least two unidirectionally oriented fiber layers B and B comprising parallel reinforcing fiber bundles, wherein at least two layers B and B have different fiber orientations relative to at least one other B or B layer prior to stitching and needling, wherein all layers are both stitched together and also subsequently needled, the thermoformable composite material being formed by: a) continuously merging together at least one fiber nonwoven layer A1 produced by a carding, airlay or spunbound nonwoven process, with at least two unidirectionally oriented fiber layers B and B, at least one layer B and one layer B having different fiber orientations relative to each other and subsequently stitching the layers to each other and thereafter needling the layers; or: b) continuously merging together at least one thermoplastic film layer A2 with at least two unidirectionally oriented fiber layers B and B, at least one layer B and one layer B having different fiber orientations relative to each other, stitching the layers to each other and thereafter needling the layers.
2. The method of claim 1, wherein a three-dimensional component is produced, comprising: heat pressing in a mold a thermoformable composite material comprising a) at least one layer A comprising A1 a fiber nonwoven comprising 40 to 100 wt.-% thermoplastic fibers and 60 to 0 wt.-% reinforcing fibers, or comprising, A2 a thermoplastic film, and b) at least two unidirectionally oriented fiber layers B and B comprising parallel reinforcing fiber bundles, wherein at least two layers B and B have different fiber orientations relative to at least one other B or B layer prior to stitching and needling, wherein all layers are both stitched together and also subsequently needled, the thermoformable composite material being formed by: a) continuously merging together at least one fiber nonwoven layer A1 produced by a carding, airlay or spunbound nonwoven process, with at least two unidirectionally oriented fiber layers B and B, at least one layer B and one layer B having different fiber orientations relative to each other and subsequently stitching the layers to each other and thereafter needling the layers; or: b) continuously merging together at least one thermoplastic film layer A2 with the at least two unidirectionally oriented fiber layers B and B, at least one layer B and one layer B having different fiber orientations relative to each other, stitching the layers to each other and thereafter needling the layers.
3. The method of claim 1, wherein a planar semifinished product with a thickness of 0.5 to 5 mm is produced, comprising heat pressing in a double band press a thermoformable composite material, comprising a) at least one layer A comprising A1 a fiber nonwoven comprising 40 to 100 wt.-% thermoplastic fibers and 60 to 0 wt.-% reinforcing fibers, or comprising, A2 a thermoplastic film, and b) at least two unidirectionally oriented fiber layers B and B comprising parallel reinforcing fiber bundles, wherein at least two layers B and B have different fiber orientations relative to at least one other B or B layer prior to stitching and needling, wherein all layers are both stitched together and also subsequently needled, the thermoformable composite material being formed by: a) continuously merging together at least one fiber nonwoven layer A1 produced by a carding, airlay or spunbound nonwoven process, with at least two unidirectionally oriented fiber layers B and B, at least one layer B and one layer B having different fiber orientations relative to each other and subsequently stitching the layers to each other and thereafter needling the layers; or: b) continuously merging together at least one thermoplastic foil layer A2 with at least two unidirectionally oriented fiber layers B and B, at least one layer B and one layer B having different fiber orientations relative to each other, stitching the layers to each other and thereafter needling the layers.
4. The method of claim 2, wherein the thermoformable composite material has a layer arrangement of B-A-B or B-A-B-A-B.
5. The method of claim 3, wherein the thermoformable composite material has a layer arrangement of B-A-B or B-A-B-A-B.
6. The method of claim 2, wherein the fiber orientation of the layers B and B with respect to a reference direction of the thermoformable composite material is 0/90, 30/30, 45/45 or 60/60.
7. The method of claim 3, wherein the fiber orientation of the layers B and B with respect to a reference direction of the thermoformable composite material is 0/90, 30/30, 45/45 or 60/60.
8. The method claim 2, wherein the areal weights of the individual layers of the thermoformable composite material each are 20 to 1,000 g/m.sup.2.
9. The method of claim 3, wherein the areal weights of the individual layers of the thermoformable composite material each are 20 to 1,000 g/m.sup.2.
10. The method of claim 2, wherein the areal weights of the individual layers of the thermoformable composite material each are 150 to 3,000 g/m.sup.2.
11. The method of claim 3, wherein the areal weights of the individual layers of the thermoformable composite material each are 150 to 3,000 g/m.sup.2.
12. The method of claim 2, wherein the total amount of reinforcing fibers in the of the thermoformable composite material is 20 to 80 wt.-%, based on the total weight of the thermoformable composite material.
13. The method of claim 3, wherein the total amount of reinforcing fibers in the thermoformable composite material is 20 to 80 wt.-%, based on the total weight of the thermoformable composite material.
14. The method of claim 2, wherein the layers are merged to form an arrangement B-A1-B or B-A1-B-A1-B.
15. The method of claim 3, wherein the layers are merged to form an arrangement B-A1-B or B-A1-B-A1-B.
16. The method of claim 2, wherein the layers are merged to form an arrangement B-A2-B or B-A2-B-A2-B.
17. The method of claim 3, wherein the layers are merged to form an arrangement B-A2-B or B-A2-B-A2-B.
18. The method of claim 2, wherein the layers are merged to form an arrangement such that a thermoplastic film A2 is present on at least one side of the thermoformable composite material.
19. The method of claim 3, wherein the layers are merged to form an arrangement such that a thermoplastic film A2 is present on at least one side of the thermoformable composite material.
20. The method of claim 14, wherein a further layer, A2 is present, on one or both outsides of the B-A1-B or B-A1-B-A1-B layers.
21. The method of claim 15, wherein a further layer, A2 is present, on one or both outsides of the B-A1-B or B-A1-B-A1-B layers.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0014]
[0015]
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
[0016] The term thermoplastic as generally known in the technical field is to be understood in such manner that the corresponding materials can be melted and thermoplastically molded under conventional processing conditions.
[0017] According to an advantageous embodiment the fiber nonwoven of the layer A contains up to 50 wt.-% reinforcing fibers. According to another advantageous embodiment the fiber nonwoven of the layer A contains no reinforcing fibers and is, therefore, only made of thermoplastic fibers. According to a further advantageous embodiment the layer A is made of a thermoplastic foil.
[0018] Bidirectional in the context with two oriented fiber layers B and B means that the longitudinal axis of the oriented fiber layer B is not parallel to the longitudinal axis of the oriented fiber layer B.
[0019] Further objects of the invention are processes for producing such composite materials. There are two variants therefor:
[0020] In the first variant, initially the fiber nonwoven-layer(s) A are produced according to the carding, airlay or spunbound nonwoven process or according to so-called paper making process, and subsequently the oriented fiber layers B and B, which are bidirectionally aligned to each other, are continuously joined together with the layer(s) A. The layers are subsequently stitched to each other and thereafter needled.
[0021] In the second variant, the thermoplastic foil(s) of the layer A and the oriented fiber layers of the layers B and B, which are bidirectionally aligned to each other, are continuously joined, stitched to each other and are thereafter needled.
[0022] Preferred layer arrangements are B-A-B and B-A-B-A-B. Further arrangements with a plurality of up to 20 layers are possible. It is preferred that always a fiber nonwoven or a thermoplastic foil layer A is arranged between two oriented layers B or B. For specific applications, an arrangement in which one layer A is arranged at the outside is also possible.
[0023] The fiber orientation of the layers B or B is bidirectional, and preferred orientations are 0/90, 30/30, 45/45 and 60/60 with respect to a reference direction in the layer arrangement such as, for example, its longitudinal axis L. Accordingly, the acute angle between the respective fiber directions is preferably 60 or 90. Thereby, the layers are preferably arranged symmetrically.
[0024]
[0025] The areal weights of the individual layers are preferably between 20 to 1,000 g/m.sup.2, particularly between 30 to 1,000 g/m.sup.2, more particularly between 150 and 300 g/m.sup.2. The individual oriented fiber layers may also have different areal weights. The areal weights are to be selected in such manner that the portion of the total reinforcing fibers in the composite material is preferably 20 to 80 wt.-%, more preferably 30 to 70 wt.-% and most preferably about 60 wt.-%.
[0026] Preferred reinforcing fibers are glass fibers and carbon fibers; but also aramide fibers, basalt fibers, natural fibers, and fibers from higher melting polymers, as well as hybrid fibers, for example from glass fibers and polypropylene fibers, are suitable. Preferably, the fiber types are in each case the same in the individual layers. The reinforcing fibers of the oriented fiber layer are preferably present as fiber bundle with a titer between 300 and 4,800 tex.
[0027] Preferred thermoplastics in the fiber nonwoven or in the thermoplastic foil are polypropylene and meltable polyamides, particularly aliphatic polyamides; in addition, other thermoplastics such as polyester, polyether sulfone, polyether ketones and polyether imide are also suitable. Polyether ketones stand out particularly by a good heat resistance. Composite materials having a particularly good flowability can be obtained if the thermoplastic is polypropylene with a melt flow index (melt flow index, MFI) (230 C., 2.16 kg) between 10 and 400, particularly at about 120 g/10 min. The thermoplastics for producing the fiber nonwoven of the layer A can be provided in many different dimensions and geometries.
[0028] The individual layers of the composite material are both stitched to each other and also needled.
[0029] Upon stitching, the fiber bundles of the oriented fiber layer are connected to each other by means of a stitching thread which forms meshes. Thereby, the reinforcing fibers are fixed in their parallel orientation. Suitable stitching threads can be made of glass, polypropylene, polyamide, and also of PET or polyether ketones. Acetate and viscose threads can also be used.
[0030] Preferably, the stitching threads are made of the same thermoplastic as the thermoplastic fibers or the thermoplastic foil of the layer A, that is, preferably also of polypropylene or polyamide.
[0031]
[0032] Upon needling, as already explained, the fiber bundles are opened and the fibers are partially broken. Moreover, thermoplastic fibers are drawn out of the nonwoven into the oriented fiber layer by the barbs of the needles. The same happens also upon needling the thermoplastic foil, where fragments or threads are torn out of the foil and drawn into the oriented fiber layer by the barbs. The needling can be carried out on conventional needling looms with felting needles. The number of needle stitches may vary between 5 and 100 per cm.sup.2, particularly between 20 and 40 punctures per cm.sup.2.
[0033] All this has the result that by the subsequent hot pressing the thermoplastic melt penetrates from the fiber nonwoven or from the thermoplastic foil into the oriented fiber layers and can impregnate the same uniformly. If the stitching thread consists of the same thermoplast, it will also melt during the hot pressing; thereafter it is no longer needed.
[0034] Due to the fact that the fiber bundles are additionally stitched to each other, they keep their orientation upon needling, and because by the needling also the oriented fiber layer is connected to the fiber nonwoven layer or to the thermoplastic foil, there is also no risk for the layers to slip out of position during the transport and the subsequent processing.
[0035] At temperatures above the softening range of the thermoplastic the planar composite materials of the present invention can be directly pressed in molds to form three-dimensional components, or they can be consolidated by means of heat pressing, for example, in a double band press, to planar semifinished products, preferably with a thickness of 0.5 to 5 mm.
[0036] While embodiments of the invention have been illustrated and described, it is not intended that these embodiments illustrate and describe all possible forms of the invention. Rather, the words used in the specification are words of description rather than limitation, and it is understood that various changes may be made without departing from the spirit and scope of the invention.