Nonwoven laminate
US-12152326-B1 · Nov 26, 2024 · US
US9643380B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9643380-B2 |
| Application number | US-201214233090-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 1, 2012 |
| Priority date | Jul 12, 2012 |
| Publication date | May 9, 2017 |
| Grant date | May 9, 2017 |
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A carbon fiber reinforced composite material including at least two carbon fiber fabrics and a thermoplastic resin, wherein each of the at least two carbon fiber fabrics is formed of an opened yarn obtained by opening a carbon fiber bundle, and the thermoplastic resin is impregnated with the at least two carbon fiber fabrics in a solidified state such that the carbon fiber reinforced composite material is formed integrally as a whole. Also disclosed is a method for producing the carbon fiber reinforced composite material.
Opening claim text (preview).
The invention claimed is: 1. A method for producing a carbon fibre reinforced composite material, the method comprising: a step of carrying out thermal pressing of a laminate comprising (a) at least two carbon fibre fabrics of an opened yarn obtained by opening a carbon fibre bundle and (b) a foam of a thermoplastic resin between the at least two carbon fibre fabrics wherein the foam of the thermoplastic resin melts to form a molten thermoplastic resin and the molten thermoplastic resin is impregnated into the at least two carbon fibre fabrics; and a step of solidifying the molten thermoplastic resin that has been penetrated into the two carbon fibre fabrics to form the carbon fibre reinforced composite material; wherein the foam of the thermoplastic resin is a closed-cell foam; and in the thermal pressing step, the foam of the thermoplastic resin exhibits a spring effect to promote penetration of the molten thermoplastic resin into the two carbon fibre fabrics and removal of voids. 2. The method according to claim 1 , wherein a film of a thermoplastic resin is disposed on at least one face of the carbon fibre fabric. 3. The method according to claim 1 , wherein the laminate is formed of at least 5 layers of, in the order from one face, the film of the thermoplastic resin, the carbon fibre fabric, the foam of the thermoplastic resin, the carbon fibre fabric and the film of the thermoplastic resin. 4. The method according to claim 1 , wherein the laminate is formed of only 7 layers of, in the order from one face, the film of the thermoplastic resin, the carbon fibre fabric, the film of the thermoplastic resin, the foam of the thermoplastic resin, the film of the thermoplastic resin, the carbon fibre fabric and the film of the thermoplastic resin. 5. The method according to claim 2 , wherein a thermoplastic resin of the foam of the thermoplastic resin and a thermoplastic resin of the film of the thermoplastic resin are of the same kind. 6. The method according to claim 1 , wherein all thermoplastic resins contained in the carbon fibre reinforced composite material are of the same kind. 7. The method according to claim 1 , wherein a maximum height (Rmax) thereof is 12.0 μm or less, a ten-point mean roughness (Rz) thereof is 6.0 μm or less, a flexural modulus thereof is 25 GPa or more, a flexural strength is 170 MPa or more and a thickness thereof is 0.5 mm or less. 8. The method according to claim 1 , wherein the solidified thermoplastic resin is substantially in non-foamy state. 9. The method of claim 1 , wherein the thermoplastic resin is polyamide (Nylon 6) or polyethylene. 10. The method of claim 1 , wherein the thermoplastic resin foam in the laminate has a thickness of from 1.5 mm to 2.3 mm prior to step of carrying out the thermal pressing, and wherein the carbon fibre reinforced composite material has a thickness of from 0.2 to 0.5 mm.
Web or sheet containing structurally defined element or component · CPC title
Elastic · CPC title
comprising polycarbonates · CPC title
Carbon fibres, e.g. graphite fibres · CPC title
next to a fibrous or filamentary layer · CPC title
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