Manufacturing method for fibre-reinforced resin substrate or resin molded article, and plasticizing exhauster used in manufacturing method
US-2016001510-A1 · Jan 7, 2016 · US
US10507612B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10507612-B2 |
| Application number | US-201615260459-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 9, 2016 |
| Priority date | Mar 11, 2014 |
| Publication date | Dec 17, 2019 |
| Grant date | Dec 17, 2019 |
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Disclosed is a composite material including a black pigment, carbon fibers, and a resin, wherein marking is applied with a laser having a wavelength of 100 to 2,000 nm on the composite material having 1) an area proportion of the carbon fibers in its topmost surface layer of 10 to 90%, 2) a proportion of the black pigment contained in the composite material of 0.2 to 20% by mass, and 3) an average fiber length of the carbon fibers of 1 mm or more.
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The invention claimed is: 1. A method of applying laser marking on a composite material comprising a black pigment, carbon fibers, and a resin, and having the following 1) to 3): 1) an area proportion of the carbon fibers in a topmost surface layer of the material from 10 to 90%, 2) a proportion of the black pigment contained in the composite material from 0.2 to 20% by mass, and 3) an average fiber length of the carbon fibers from 1 to 100 mm, wherein the laser marking is applied using a YVO 4 laser having a wavelength from 100 to 2,000 nm, an output density from 1.0 (mW/μm 2 ) to 30 (mW/μm 2 ), and an irradiation energy per pulse from 1000×10 −5 (mWs) to 50,000×10 −5 (mWs). 2. The method of applying laser marking according to claim 1 , wherein the wavelength is 300 to 600 nm. 3. The method of applying laser marking according to claim 1 , wherein the area proportion of the carbon fibers in the topmost surface layer is 20 to 60%. 4. The method of applying laser marking according to claim 1 , wherein the resin contained in the composite material is a thermoplastic resin. 5. The method of applying laser marking according to claim 1 , wherein a volume fraction (Vf) of the carbon fibers contained in the composite material is 10 to 65%. 6. The method of applying laser marking according to claim 1 , wherein the black pigment is carbon black. 7. The method of applying laser marking according to claim 1 , wherein the laser marking is applied using a laser having an output density from 3.0 (mW/μm 2 ) to 20 (mW/μm 2 ). 8. The method of applying laser marking according to claim 1 , wherein the wavelength is 1,000 to 1,200 nm. 9. The method of applying laser marking according to claim 1 , wherein the irradiation energy per pulse is from 1500×10 −5 (mWs) to 10,000×10 −5 (mWs). 10. The method of applying laser marking according to claim 1 , wherein the laser marking is applied using a laser beam having a beam diameter from 10 to 40 μm. 11. A method of producing a composite material having laser marking applied thereon by using the method of applying laser marking set forth in claim 1 . 12. The method of producing a composite material according to claim 11 , wherein the wavelength is 300 to 600 nm. 13. The method of producing a composite material according to claim 11 , wherein the area proportion of the carbon fibers in the topmost surface layer is 20 to 60%. 14. The method of producing a composite material according to claim 11 , wherein the resin contained in the composite material is a thermoplastic resin. 15. The method of producing a composite material according to claim 11 , wherein a volume fraction (Vf) of the carbon fibers contained in the composite material is 10 to 65%. 16. The method of producing a composite material according to claim 11 , wherein the black pigment is carbon black. 17. The method of producing a composite material according to claim 11 , wherein the wavelength is 1,000 to 1,200 nm.
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