CN103642170A - Preparation method for carbon fiber composite material - Google Patents
Preparation method for carbon fiber composite material Download PDFInfo
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- CN103642170A CN103642170A CN201310598537.8A CN201310598537A CN103642170A CN 103642170 A CN103642170 A CN 103642170A CN 201310598537 A CN201310598537 A CN 201310598537A CN 103642170 A CN103642170 A CN 103642170A
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Abstract
The invention relates to a preparation method for a carbon fiber composite material. The main preparation steps include: material selection, material mixing, carbon fiber prefabrication, impregnation, heat treatment, and curing. The carbon fiber composite material involved in the invention has the advantages of excellent tensile strength and breaking elongation, easy large area integral molding, and stable molding.
Description
Technical field
The present invention relates to a kind of preparation method of matrix material, relate in particular to a kind of preparation method of carbon-fibre composite.
Background technology
The appearance of carbon-fibre composite, has improved thermal expansivity, fracture toughness property, impelling strength, electrical property, the magnetic property of single metal material greatly, thereby is widely used in the sophisticated technology industries such as military project, space flight.But in the performances such as conventional its tensile strength of CB/PVC material and elongation at break, go back Shortcomings, overall performance is had to larger impact.
Summary of the invention
For above-mentioned the deficiencies in the prior art, the invention provides a kind of carbon-fibre composite, this carbon-fibre composite has good tensile strength and elongation at break, easily big area global formation, stable molding.Concrete technical scheme is:
The present invention adopts following steps to prepare carbon-fibre composite:
(1) by parts by weight, be that the viscose fiber of 50 ~ 60 parts, the rayon fibers that parts by weight are 25 ~ 30 parts, the pitch that parts by weight are 15 ~ 20 parts pass through dry mixed, then by batch mixing wire drawing, in air, heat, temperature maintains 200 ℃ ~ 300 ℃ and continues 50 minutes, then in inert atmosphere, be heated to 1200 ℃, maintain 20 minutes, then in inert atmosphere, be heated to 2500 ℃, maintain 15 seconds;
(2) carbon fiber making is immersed to the steeping vat of filling epoxy resin by transmission mechanism; Dipping time is controlled at 10s ~ 20s;
(3) then the carbon fiber having flooded is sent in heating unit and is cured, be 10min ~ 20min set time, and solidification value is 120 ℃;
(4) after epoxy resin cure, send out heating unit, take out goods.
Preferred version, described rare gas element is high pure nitrogen.
Preferred version, described heating unit is infrared-ray oven.
The carbon-fibre composite that the present invention can make through above-mentioned steps, this matrix material has good tensile strength and elongation at break, easily big area global formation, stable molding.
Embodiment
Below by embodiment, the invention will be further described:
Embodiment 1: by parts by weight, be the viscose fiber of 50 parts, parts by weight are the rayon fibers of 30 parts, parts by weight are that the pitch of 20 parts passes through dry mixed, then by batch mixing wire drawing, in air, heat, temperature maintains 200 ℃ and continues 50 minutes, then in inert atmosphere, be heated to 1200 ℃, maintain 20 minutes, in inert atmosphere, be heated to again 2500 ℃, maintain 15 seconds, the carbon fiber making is immersed to the steeping vat of filling epoxy resin by transmission mechanism, dipping time is controlled at 10s, then the carbon fiber having flooded is sent in heating unit and is cured, be 10min set time, solidification value is 120 ℃, after epoxy resin cure, send out heating unit, take out goods.
Embodiment 2: by parts by weight, be the viscose fiber of 60 parts, parts by weight are the rayon fibers of 25 parts, parts by weight are that the pitch of 15 parts passes through dry mixed, then by batch mixing wire drawing, in air, heat, temperature maintains 300 ℃ and continues 50 minutes, then in inert atmosphere, be heated to 1200 ℃, maintain 20 minutes, in inert atmosphere, be heated to again 2500 ℃, maintain 15 seconds, the carbon fiber making is immersed to the steeping vat of filling epoxy resin by transmission mechanism, dipping time is controlled at 20s, then the carbon fiber having flooded is sent in heating unit and is cured, be 20min set time, solidification value is 120 ℃, after epoxy resin cure, send out heating unit, take out goods.
Comparison of test results:
Table 1: the physicochemical property cartogram of two embodiment
? | Tensile strength/MPa | Elongation at break/% | Flexural strength/MPa |
CB/PVC | 61.8 | 87.36 | 101.65 |
Embodiment 1 | 72.66 | 120.33 | 105.62 |
Embodiment 2 | 71.84 | 118.83 | 103.22 |
Claims (4)
1. the preparation method of a carbon-fibre composite, it is characterized in that: viscose fiber, rayon fibers, pitch are passed through to dry mixed, then by batch mixing wire drawing, in air, heat, then in inert atmosphere, heat, in inert atmosphere, heat under certain condition again, the carbon fiber making is immersed to the steeping vat of filling epoxy resin by transmission mechanism, then the carbon fiber having flooded is sent in heating unit and is cured, after epoxy resin cure, send out heating unit, take out goods.
2. a preparation method for carbon-fibre composite, is characterized in that: concrete steps are,
(1) carbon fiber preparation: according to parts by weight, the viscose fiber of 50 ~ 60 parts, the rayon fibers of 25 ~ 30 parts, the pitch of 15 ~ 20 parts pass through dry mixed, then by batch mixing wire drawing, in air, heat, temperature maintains 200 ℃ ~ 300 ℃ and continues 50 minutes, then in inert atmosphere, is heated to 1200 ℃, maintains 20 minutes, in inert atmosphere, be heated to again 2500 ℃, maintain 15 seconds;
(2) carbon fiber making is immersed to the steeping vat of filling epoxy resin by transmission mechanism; Dipping time is controlled at 10s ~ 20s;
(3) then the carbon fiber having flooded is sent in heating unit and is cured, be 10min ~ 20min set time, and solidification value is 120 ℃;
(4) after epoxy resin cure, send out heating unit, take out goods.
3. the preparation method of a kind of carbon-fibre composite according to claim 1, is characterized in that: described rare gas element high pure nitrogen.
4. the preparation method of a kind of carbon-fibre composite according to claim 1, is characterized in that: described heating unit is infrared-ray oven.
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CN201310598537.8A CN103642170A (en) | 2013-11-25 | 2013-11-25 | Preparation method for carbon fiber composite material |
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CN201310598537.8A CN103642170A (en) | 2013-11-25 | 2013-11-25 | Preparation method for carbon fiber composite material |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105220274A (en) * | 2015-11-09 | 2016-01-06 | 沈阳化工大学 | The preparation method of the brilliant material of a kind of asphalt base carbon fiber carbon |
CN105236838A (en) * | 2015-10-09 | 2016-01-13 | 中复神鹰碳纤维有限责任公司 | Reinforced concrete and preparation method thereof |
Citations (4)
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CN101423650A (en) * | 2008-11-27 | 2009-05-06 | 中国科学院山西煤炭化学研究所 | High interlaminar shear strength epoxy resin base composite material and preparation method thereof |
CN102060555A (en) * | 2010-11-24 | 2011-05-18 | 西安超码科技有限公司 | Method for manufacturing high-strength carbon/carbon hot-press die |
CN102675886A (en) * | 2012-05-07 | 2012-09-19 | 湖北大学 | Fiber-reinforced epoxy asphalt material and preparation method thereof |
CN103193495A (en) * | 2013-03-01 | 2013-07-10 | 辽阳金谷碳纤维科技有限公司 | Production method of insulation materials used for crystal pulling furnace |
-
2013
- 2013-11-25 CN CN201310598537.8A patent/CN103642170A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
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CN101423650A (en) * | 2008-11-27 | 2009-05-06 | 中国科学院山西煤炭化学研究所 | High interlaminar shear strength epoxy resin base composite material and preparation method thereof |
CN102060555A (en) * | 2010-11-24 | 2011-05-18 | 西安超码科技有限公司 | Method for manufacturing high-strength carbon/carbon hot-press die |
CN102675886A (en) * | 2012-05-07 | 2012-09-19 | 湖北大学 | Fiber-reinforced epoxy asphalt material and preparation method thereof |
CN103193495A (en) * | 2013-03-01 | 2013-07-10 | 辽阳金谷碳纤维科技有限公司 | Production method of insulation materials used for crystal pulling furnace |
Non-Patent Citations (1)
Title |
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杨延风等: "碳纤维复丝的拉伸性能", 《理化检验-物理分册》 * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105236838A (en) * | 2015-10-09 | 2016-01-13 | 中复神鹰碳纤维有限责任公司 | Reinforced concrete and preparation method thereof |
CN105220274A (en) * | 2015-11-09 | 2016-01-06 | 沈阳化工大学 | The preparation method of the brilliant material of a kind of asphalt base carbon fiber carbon |
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Application publication date: 20140319 |