CN106810711B - A method of recycling carbon fiber from waste and old carbon fibre reinforced composite - Google Patents

A method of recycling carbon fiber from waste and old carbon fibre reinforced composite Download PDF

Info

Publication number
CN106810711B
CN106810711B CN201611247331.0A CN201611247331A CN106810711B CN 106810711 B CN106810711 B CN 106810711B CN 201611247331 A CN201611247331 A CN 201611247331A CN 106810711 B CN106810711 B CN 106810711B
Authority
CN
China
Prior art keywords
reinforced composite
fibre reinforced
carbon fibre
carbon fiber
carbon
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201611247331.0A
Other languages
Chinese (zh)
Other versions
CN106810711A (en
Inventor
梅生伟
吴磊
陈晓弢
薛小代
司杨
张韶红
陈来军
卢强
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tsinghua University
Qinghai University
Original Assignee
Tsinghua University
Qinghai University
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Tsinghua University, Qinghai University filed Critical Tsinghua University
Priority to CN201611247331.0A priority Critical patent/CN106810711B/en
Publication of CN106810711A publication Critical patent/CN106810711A/en
Application granted granted Critical
Publication of CN106810711B publication Critical patent/CN106810711B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J11/00Recovery or working-up of waste materials
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K7/00Use of ingredients characterised by shape
    • C08K7/02Fibres or whiskers
    • C08K7/04Fibres or whiskers inorganic
    • C08K7/06Elements

Abstract

The present invention relates to the recycling of carbon fibre material more particularly to a kind of methods that carbon fiber is recycled from waste and old carbon fibre reinforced composite.The method that carbon fiber is recycled from waste and old carbon fibre reinforced composite are as follows: after carbon fibre reinforced composite pretreatment, the heat treatment of 70~110min is carried out at 400~500 DEG C, gained solid product is carbon fiber after the recovery.The method of the invention simple process, step is few, low energy consumption, it is smooth to recycle obtained carbon fiber surface, it has excellent performance, purity is high, and substantially increases the rate of recovery, in waste and old carbon fibre reinforced composite field, especially there is important application and popularization value in the waste and old carbon fibre reinforced composite recycling field of retired aircraft.

Description

A method of recycling carbon fiber from waste and old carbon fibre reinforced composite
Technical field
The present invention relates to the recycling of carbon fibre material, more particularly to one kind to recycle from waste and old carbon fibre reinforced composite The method of carbon fiber.
Background technique
The great demand of China's retired aircraft in need of immediate treatment at present.Ended for the end of the year 2015, is flying in world wide Business aircraft is about 20000 framves, and China's commercial aircraft accounts for 4000 framves, because Air Passenger machine Years Of Service is generally 25-30, on Stating type gradually will scrap and be recycled.It can be seen that it is retired that processing will be present in the Chinese or even whole world in coming few decades The constant demand of aircraft.Carbon fiber (carbon fiber, abbreviation CF) is a kind of high intensity 95% or more of phosphorus content, height The new fiber materials of modulus fibre.Carbon fiber has many excellent performances, and the axial strength and modulus of carbon fiber are high, density Low, good corrosion resistance higher than performance, good electrical and thermal conductivity performance, electromagnetic wave shielding are good etc..
And as carbon fibre reinforced composite (the Carbon fiber for being applied to the military industry fields such as aircraft manufacturing Reinforced polymer composites, abbreviation CFRP) recycling can achieve save resource and the energy mesh 's.Composite material recovery technology is commercialized maximum obstruction and is the market demand scarcity of regrown material, high remanufacture The reduction of cost and regrown material performance.Currently, the composite material recovery technology of fibre reinforced includes the following three types: mechanical Recycling, recuperation of heat and chemical recovery.
As a kind of method for recycling carbon fibre material, recuperation of heat has with low power consuming, processing capacity is strong, the rate of recovery is high Etc. incomparable advantage, if but control the technological parameter of bad recuperation of heat method, can machinery to the carbon fiber being recovered to it is strong Degree damages.
Summary of the invention
In order to solve the above-mentioned technical problems, the present invention provides one kind to recycle carbon from waste and old carbon fibre reinforced composite The method of fiber, it may be assumed that after carbon fibre reinforced composite pretreatment, carry out 70~110min's at 400~500 DEG C Heat treatment, gained solid product is carbon fiber after the recovery.The carbon fiber surface light that the method for the invention recycles It is sliding, it has excellent performance, purity is high, and substantially increase the rate of recovery.
Preferably, the heat treatment is that 80~100min is heated at 420~470 DEG C.
It is furthermore preferred that the heat treatment is to heat 85~95min at 440~460 DEG C.
Further preferably, the heat treatment is to heat 90min at 450 DEG C.
Preferably, the pretreatment are as follows: after carbon fibre reinforced composite cutting, be put into dehydrated alcohol and impregnate It to remove surface impurity, then dries within 1.5~2.5 hours.
Further, the cutting are as follows: the carbon fibre reinforced composite is cut into the segment of 0.2m × 0.2m.
It is further, described that be put into time for impregnating in dehydrated alcohol be 2 hours.
Preferably, the mode of the heating is the heating of sunlight optically focused.
The present invention provides a kind of preferred embodiments for recycling carbon fiber comprising following steps:
(1) it pre-processes: it is small that the carbon fibre reinforced composite being cut into 0.15~0.25m × 0.15~0.25m Section, is put into dehydrated alcohol and impregnates 2~2.5 hours to remove surface impurity, then dry;
(2) heat: step (1) treated carbon fibre reinforced composite is poly- using sunlight at 450 DEG C Light heats 90min, and gained solid product is carbon fiber after the recovery.
The matrix of carbon fibre reinforced composite of the present invention is thermosetting resin.
Above-mentioned technical proposal of the invention has the advantages that the method for the invention simple process, and step is few, energy Consume low, the carbon fiber surface recycled is smooth, has excellent performance, purity is high, and substantially increase the rate of recovery.
Detailed description of the invention
Fig. 1 passes through recuperation of heat for the waste and old carbon fibre reinforced composite of the embodiment of the present invention at different temperatures and handles The TGA figure arrived;
Fig. 2 is at 450 DEG C, and the processing time is respectively the carbon that 60min (A), 90min (B) and 120min (C) are recycled afterwards The scanning electron microscope (SEM) photograph of fiber;
Fig. 3 is at 450 DEG C, and the processing time is the scanning electron microscope (SEM) photograph of the carbon fiber recycled after 90min.
Specific embodiment
Embodiments of the present invention are described in further detail with reference to the accompanying drawings and examples.Following embodiment is used for Illustrate the present invention, but cannot be used to limit the scope of the invention.
Waste and old carbon fibre reinforced composite used in the embodiment of the present invention derives from retired aircraft.
Embodiment 1
A method of it recycling carbon fiber from waste and old carbon fibre reinforced composite, includes the following steps:
(1) it pre-processes: the carbon fibre reinforced composite being cut into the segment of 0.2m × 0.2m, is put into dehydrated alcohol It is middle to impregnate 2 hours to remove surface impurity, then dry;
(2) heat: by step (1), treated that carbon fibre reinforced composite is put on sample treatment platform, 450 90min is heated using sunlight optically focused at DEG C, gained solid product is carbon fiber after the recovery.
Embodiment 2
A method of it recycling carbon fiber from waste and old carbon fibre reinforced composite, includes the following steps:
(1) it pre-processes: the carbon fibre reinforced composite being cut into the segment of 0.2m × 0.25m, is put into anhydrous second 2.5 hours are impregnated in alcohol to remove surface impurity, are then dried;
(2) heat: by step (1), treated that carbon fibre reinforced composite is put on sample treatment platform, 470 95min is heated using sunlight optically focused at DEG C, gained solid product is carbon fiber after the recovery.
Embodiment 3
A method of it recycling carbon fiber from waste and old carbon fibre reinforced composite, includes the following steps:
(1) it pre-processes: the carbon fibre reinforced composite being cut into the segment of 0.15m × 0.15m, is put into anhydrous second 1.5 hours are impregnated in alcohol to remove surface impurity, are then dried;
(2) heat: by step (1), treated that carbon fibre reinforced composite is put on sample treatment platform, 420 100min is heated using sunlight optically focused at DEG C, gained solid product is carbon fiber after the recovery.
As seen from Figure 1, carbon fibre reinforced composite is weightless in 344.1 DEG C of beginnings, and weightlessness is 1.86%.Work as heating Mass loss 16.80% when to 436.6 DEG C.When being continuously heating to 697.0 DEG C, residual qualities 75.42%.Illustrate the carbon fiber The pyrolysis temperature section for enhancing composite material is 344.1~436.6 DEG C.The quality for continuing carbon fiber after heating up is kept constant.
By Fig. 2, it can be seen that, the carbon fiber surface that heat treatment 60min is obtained has apparent buildup of resin, haircut mark in figure The resin of carbon fiber surface is shown;The carbon fiber surface obtained after heat treatment 90min is smooth;And it is obtained after handling 120min Carbon fiber surface there is apparent dent (shown in circle), illustrate that with this condition, carbon fiber surface has been destroyed.
By Fig. 3, it can be seen that, the carbon fiber surface obtained after 450 DEG C of processing 90min is smooth, and diameter is 7 μm.
In conclusion the present invention handles 90min at 450 DEG C with the technique that light thermal method recycles carbon fibre reinforced composite The excellent properties of carbon fiber can be retained.
Comparative example 1
A method of recycling carbon fiber, substantially the same manner as Example 1, area from waste and old carbon fibre reinforced composite Be not only that: the heat treatment of step (2) is to heat 120min using sunlight optically focused at 350 DEG C.Treated, and carbon fiber increases Strong composite material surface has a large amount of buildup of resin, does not thoroughly remove the resin of wrap carbon fiber, multiple in fibre reinforced There was only a small amount of carbon fiber in condensation material surface.
Comparative example 2
A method of recycling carbon fiber, substantially the same manner as Example 1, area from waste and old carbon fibre reinforced composite Be not only that: the heat treatment of step (2) is to heat 60min using sunlight optically focused at 450 DEG C.The carbon fiber obtained after processing Surface is smooth, but the resin being present in composite material does not have completely burnout, does not reach recycling carbon fiber material completely The purpose of material.
Comparative example 3
A method of recycling carbon fiber, substantially the same manner as Example 1, area from waste and old carbon fibre reinforced composite Be not only that: the heat treatment of step (2) is to heat 60min using sunlight optically focused at 600 DEG C.The carbon fiber obtained after processing There is apparent dent in surface, illustrates that with this condition, carbon fiber surface has been destroyed, the carbon fiber of recycling loses original The structure come, has no practical application value.
The embodiment of the present invention is given for the purpose of illustration and description, and is not exhaustively or by this to send out It is bright to be limited to disclosed form.Many modifications and variations are obvious for the ordinary skill in the art.Choosing Selecting and describe embodiment is and to make those skilled in the art to more preferably illustrate the principle of the present invention and practical application It will be appreciated that the present invention is to design various embodiments suitable for specific applications with various modifications.

Claims (9)

1. a kind of method for recycling carbon fiber from waste and old carbon fibre reinforced composite, which is characterized in that by the carbon fiber After enhancing composite material pretreatment, the heat treatment of 85~95min is carried out at 440~460 DEG C, gained solid product is back Carbon fiber after receipts;
The mode of the heating is the heating of sunlight optically focused;
The pretreatment are as follows: after carbon fibre reinforced composite cutting, it is small to be put into immersion 1.5~2.5 in dehydrated alcohol When to remove surface impurity, then dry.
2. the method according to claim 1, wherein the heat treatment is to heat 90min at 450 DEG C.
3. the method according to claim 1, wherein the cutting are as follows: by the carbon fibre reinforced composite It is cut into 0.15~0.25m × 0.15~0.25m segment.
4. method according to claim 1 or 3, which is characterized in that it is described be put into time for being impregnated in dehydrated alcohol be 2~ 2.5 hour.
5. described in any item methods according to claim 1~3, which comprises the steps of:
(1) it pre-processes: the carbon fibre reinforced composite being cut into 0.15~0.25m × 0.15~0.25m segment, is put Enter to impregnate 2~2.5 hours in dehydrated alcohol to remove surface impurity, then dries;
(2) heat: step (1) treated carbon fibre reinforced composite is added at 450 DEG C using sunlight optically focused Hot 90min, gained solid product are carbon fiber after the recovery.
6. according to the method described in claim 4, it is characterized by comprising the following steps:
(1) it pre-processes: the carbon fibre reinforced composite being cut into 0.15~0.25m × 0.15~0.25m segment, is put Enter to impregnate 2~2.5 hours in dehydrated alcohol to remove surface impurity, then dries;
(2) heat: step (1) treated carbon fibre reinforced composite is added at 450 DEG C using sunlight optically focused Hot 90min, gained solid product are carbon fiber after the recovery.
7. according to claim 1~3 or 6 described in any item methods, which is characterized in that the carbon fibre reinforced composite Matrix is thermosetting resin.
8. according to the method described in claim 4, it is characterized in that, the matrix of the carbon fibre reinforced composite is thermosetting property Resin.
9. according to the method described in claim 5, it is characterized in that, the matrix of the carbon fibre reinforced composite is thermosetting property Resin.
CN201611247331.0A 2016-12-29 2016-12-29 A method of recycling carbon fiber from waste and old carbon fibre reinforced composite Active CN106810711B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611247331.0A CN106810711B (en) 2016-12-29 2016-12-29 A method of recycling carbon fiber from waste and old carbon fibre reinforced composite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611247331.0A CN106810711B (en) 2016-12-29 2016-12-29 A method of recycling carbon fiber from waste and old carbon fibre reinforced composite

Publications (2)

Publication Number Publication Date
CN106810711A CN106810711A (en) 2017-06-09
CN106810711B true CN106810711B (en) 2019-09-20

Family

ID=59109509

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611247331.0A Active CN106810711B (en) 2016-12-29 2016-12-29 A method of recycling carbon fiber from waste and old carbon fibre reinforced composite

Country Status (1)

Country Link
CN (1) CN106810711B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019153217A1 (en) * 2018-02-09 2019-08-15 深圳大学 Method for recovering high-performance carbon fiber from inorganic cementing material
CN111196879A (en) * 2018-11-19 2020-05-26 航天特种材料及工艺技术研究所 Method for recovering carbon fibers from carbon fiber reinforced thermosetting resin-based composite material
CN111004401A (en) * 2019-12-04 2020-04-14 安徽旭升新材料有限公司 Carbon fiber-PA 66 composite material for shoe sole and processing method thereof
CN114618874B (en) * 2022-04-01 2023-04-11 四川优比贝柠科技有限公司 Secondary recovery process for waste of thermal insulation material

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103665427A (en) * 2013-12-11 2014-03-26 上海交通大学 Method for recovering carbon fiber by cracking waste carbon fiber composite material
CN103665430A (en) * 2013-11-21 2014-03-26 上海交通大学 Thermolysis separation method for resin and carbon fibers in waste carbon fiber composite material
CN103897213A (en) * 2014-04-10 2014-07-02 合肥工业大学 Recovery method of carbon-fiber reinforced resin-base composite material with pretreatment modes

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5292408A (en) * 1990-06-19 1994-03-08 Osaka Gas Company Limited Pitch-based high-modulus carbon fibers and method of producing same

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103665430A (en) * 2013-11-21 2014-03-26 上海交通大学 Thermolysis separation method for resin and carbon fibers in waste carbon fiber composite material
CN103665427A (en) * 2013-12-11 2014-03-26 上海交通大学 Method for recovering carbon fiber by cracking waste carbon fiber composite material
CN103897213A (en) * 2014-04-10 2014-07-02 合肥工业大学 Recovery method of carbon-fiber reinforced resin-base composite material with pretreatment modes

Also Published As

Publication number Publication date
CN106810711A (en) 2017-06-09

Similar Documents

Publication Publication Date Title
CN106810711B (en) A method of recycling carbon fiber from waste and old carbon fibre reinforced composite
Lester et al. Microwave heating as a means for carbon fibre recovery from polymer composites: a technical feasibility study
Oliveux et al. Current status of recycling of fibre reinforced polymers: Review of technologies, reuse and resulting properties
Velmurugan et al. Statistical analysis of mechanical properties of wood dust filled Jute fiber based hybrid composites under cryogenic atmosphere using Grey-Taguchi method
Longana et al. Multiple closed loop recycling of carbon fibre composites with the HiPerDiF (High Performance Discontinuous Fibre) method
Yan et al. Recycling of carbon fibers in epoxy resin composites using supercritical 1-propanol
Dauguet et al. Recycling of CFRP for high value applications: Effect of sizing removal and environmental analysis of the SuperCritical Fluid Solvolysis
Cai et al. Interfacial adhesion of recycled carbon fibers to polypropylene resin: Effect of superheated steam on the surface chemical state of carbon fiber
CN103333360B (en) Reinforcement mode based high-performance fiber reinforced resin based composite material recovery method
Kim et al. A low energy recycling technique of carbon fibers-reinforced epoxy matrix composites
Relvas et al. Characterization of physical, mechanical and chemical properties of quiscal fibres: the influence of atmospheric DBD plasma treatment
CN105408079A (en) Process of producing thermoplastic-fiber composite and fan blades formed therefrom
Zöllner et al. Thermal resistance of carbon fibres/carbon fibre reinforced polymers under stationary atmospheric conditions and varying exposure times
JP2008044999A (en) Process for producing prepreg excellent in uniformity
Shen et al. A study on the characteristics and thermal properties of modified regenerated carbon fiber reinforced thermoplastic composite recycled from waste wind turbine blade spar
Sun et al. Weak layer exfoliation and an attempt for modification in anodic oxidation of PAN-based carbon fiber
Sarmah et al. Recycle and reuse of continuous carbon fibers from thermoset composites using Joule heating
US11945931B1 (en) Recyclable nano composite as well as preparation method and application thereof
CN104179001A (en) Preparation method of carbon cloth with wet chemical modified surface
Ehlert et al. Interaction of ZnO nanowires with carbon fibers for hierarchical composites with high interfacial strength
CN105196651A (en) Multi-dimensional fiber high-performance friction material and preparation method thereof
JP2011093758A (en) Carbonaceous material
CN108467511A (en) The recovery method of carbon fiber in a kind of discarded carbon carbon composite
Parsons Reinforcing fibres
CN106750506A (en) A kind of method that two-step thermal processing reclaims carbon fiber

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant