US2015030804A1PendingUtilityA1

Sheetlike composite material

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Assignee: QUADRANT PLASTIC COMPOSITES AGPriority: Feb 8, 2012Filed: Feb 8, 2013Published: Jan 29, 2015
Est. expiryFeb 8, 2032(~5.6 yrs left)· nominal 20-yr term from priority
Inventors:Burak Baser
B32B 2038/008B32B 2262/0253B32B 38/0012B32B 5/022D04H 1/46B32B 27/08B32B 2250/03B32B 2305/08B32B 2250/05B32B 2262/106B32B 27/32B32B 2250/04B32B 5/12B32B 27/285B32B 5/10B32B 2262/101B32B 5/06B32B 2262/0261B32B 27/34B32B 2250/40B32B 5/26B29C 51/145B29C 39/203B29C 70/28B29C 43/305D04H 1/48B29C 70/02Y10T428/24091B32B 27/12B29C 70/24B32B 2262/14B29C 70/506Y10T156/1044B32B 27/288B32B 2262/02B32B 5/08Y10T428/24132
57
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Claims

Abstract

A sheetlike composite material including at least one layer A of a nonwoven thermoplastic fibre web or a thermoplastic film, and at least two unidirectional oriented-fibre layers B and B′, the layers B and B′ having a bidirectional fibre orientation. The layers are not only needled but also stitched to one another.

Claims

exact text as granted — not AI-modified
1 .- 15 . (canceled) 
     
     
         16 . A planar composite material comprising
 a) at least one layer A made of a fiber nonwoven consisting of 40 to 100 wt.-% thermoplastic fibers and 60 to 0 wt.-% reinforcing fibers, or of a thermoplastic foil, 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 a bidirectional fiber orientation,   
       wherein the layers are both stitched to each other and also needled. 
     
     
         17 . The composite material of  claim 16 , wherein a layer arrangement is B-A-B′ or B-A-B′-A-B. 
     
     
         18 . The composite material of  claim 16 , wherein the fiber orientation of the layers B and B′ with respect to a reference direction of the composite material is 0°/90°, 30°/−30°, 45°/−45° or 60°/−60°. 
     
     
         19 . The composite material of  claim 16 , the areal weights of the individual layers each are 20 to 1,000 g/m 2 . 
     
     
         20 . The composite material of  claim 16 , the areal weights of the individual layers each are 30 to 1,000 g/m 2 . 
     
     
         21 . The composite material of  claim 16 , the areal weights of the individual layers each are 150 to 3,000 g/m 2 . 
     
     
         22 . The composite material of  claim 16 , wherein the total amount of reinforcing fibers in the composite material is 20 to 80 wt.-%, based on the total weight of the composite material. 
     
     
         23 . The composite material of  claim 16 , wherein the reinforcing fibers comprise glass fibers or carbon fibers. 
     
     
         24 . The composite material of  claim 16 , wherein the thermoplastic fibers or the thermoplastic foil of the layer A comprise polypropylene. 
     
     
         25 . The composite material of  claim 24 , wherein threads used for stitching comprise polypropylene. 
     
     
         26 . The composite material of  claim 16 , wherein the thermoplastic fibers or the thermoplastic foil of the layer A comprise polyamide. 
     
     
         27 . The composite material of  claim 26 , wherein the threads used for stitching comprise polyamide. 
     
     
         28 . The composite material of  claim 16 , wherein the thermoplastic fibers or the thermoplastic foil of the layer A comprise polyether ketone. 
     
     
         29 . The composite material of  claim 28 , the threads used for stitching comprise polyether ketone. 
     
     
         30 . A method for producing a composite material of  claim 16 , comprising:
 a) fiber nonwoven layer(s) A produced by a carding, airlay or spunbound nonwoven process are provided, and oriented fiber layers B and B′ are continuously merged together with the fiber nonwoven layer(s) A, and subsequently the layers are stitched to each other and thereafter needled; or   b) thermoplastic foil(s) of the layer(s) A and the oriented fiber layers B and B′ are continuously merged together, the layers are stitched to each other, and thereafter needled.   
     
     
         31 . A process for producing three-dimensional components comprising heat pressing a composite material of  claim 16  in a mold. 
     
     
         32 . A process for producing a planar semifinished product with a thickness of 0.5 to 5 mm comprising of heat pressing a composite material of  claim 16  in a double band press. 
     
     
         33 . A planar heat-moldable semi-finished product comprising a molding having a thickness of 0.5 to 5 mm prepared by thermally consolidating a composite material of  claim 16  in a double band press.

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