AU2003236029A1 - Method and apparatus for recovering carbon and/or glass fibers from a composite material - Google Patents

Method and apparatus for recovering carbon and/or glass fibers from a composite material Download PDF

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Publication number
AU2003236029A1
AU2003236029A1 AU2003236029A AU2003236029A AU2003236029A1 AU 2003236029 A1 AU2003236029 A1 AU 2003236029A1 AU 2003236029 A AU2003236029 A AU 2003236029A AU 2003236029 A AU2003236029 A AU 2003236029A AU 2003236029 A1 AU2003236029 A1 AU 2003236029A1
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Australia
Prior art keywords
fibers
pyrolysis
upgrading
reactor
carbon
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AU2003236029A
Inventor
Tommaso Canelieri
Orazio Antonio Coriano'
Giacinto Cornacchia
Sergio Galvagno
Aldo Lucch
Sabrina Portofino
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Agenzia Nazionale per le Nuove Tecnologie lEnergia e lo Sviluppo Economico Sostenibile ENEA
Karborek Srl
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Enea Ente Per Le Nuove Tecnologie Lenergia E Lambiente
Agenzia Nazionale per le Nuove Tecnologie lEnergia e lo Sviluppo Economico Sostenibile ENEA
Karborek Srl
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Publication of AU2003236029A1 publication Critical patent/AU2003236029A1/en
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    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10GCRACKING HYDROCARBON OILS; PRODUCTION OF LIQUID HYDROCARBON MIXTURES, e.g. BY DESTRUCTIVE HYDROGENATION, OLIGOMERISATION, POLYMERISATION; RECOVERY OF HYDROCARBON OILS FROM OIL-SHALE, OIL-SAND, OR GASES; REFINING MIXTURES MAINLY CONSISTING OF HYDROCARBONS; REFORMING OF NAPHTHA; MINERAL WAXES
    • C10G1/00Production of liquid hydrocarbon mixtures from oil-shale, oil-sand, or non-melting solid carbonaceous or similar materials, e.g. wood, coal
    • C10G1/10Production of liquid hydrocarbon mixtures from oil-shale, oil-sand, or non-melting solid carbonaceous or similar materials, e.g. wood, coal from rubber or rubber waste
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B17/00Recovery of plastics or other constituents of waste material containing plastics
    • B29B17/02Separating plastics from other materials
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03CCHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
    • C03C25/00Surface treatment of fibres or filaments made from glass, minerals or slags
    • C03C25/002Thermal treatment
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10BDESTRUCTIVE DISTILLATION OF CARBONACEOUS MATERIALS FOR PRODUCTION OF GAS, COKE, TAR, OR SIMILAR MATERIALS
    • C10B47/00Destructive distillation of solid carbonaceous materials with indirect heating, e.g. by external combustion
    • C10B47/28Other processes
    • C10B47/30Other processes in rotary ovens or retorts
    • CCHEMISTRY; METALLURGY
    • C10PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10BDESTRUCTIVE DISTILLATION OF CARBONACEOUS MATERIALS FOR PRODUCTION OF GAS, COKE, TAR, OR SIMILAR MATERIALS
    • C10B53/00Destructive distillation, specially adapted for particular solid raw materials or solid raw materials in special form
    • C10B53/07Destructive distillation, specially adapted for particular solid raw materials or solid raw materials in special form of solid raw materials consisting of synthetic polymeric materials, e.g. tyres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B17/00Recovery of plastics or other constituents of waste material containing plastics
    • B29B17/0026Recovery of plastics or other constituents of waste material containing plastics by agglomeration or compacting
    • B29B17/0042Recovery of plastics or other constituents of waste material containing plastics by agglomeration or compacting for shaping parts, e.g. multilayered parts with at least one layer containing regenerated plastic
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B17/00Recovery of plastics or other constituents of waste material containing plastics
    • B29B17/04Disintegrating plastics, e.g. by milling
    • B29B2017/0424Specific disintegrating techniques; devices therefor
    • B29B2017/0496Pyrolysing the materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2707/00Use of elements other than metals for preformed parts, e.g. for inserts
    • B29K2707/04Carbon
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2709/00Use of inorganic materials not provided for in groups B29K2703/00 - B29K2707/00, for preformed parts, e.g. for inserts
    • B29K2709/08Glass
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P20/00Technologies relating to chemical industry
    • Y02P20/141Feedstock
    • Y02P20/143Feedstock the feedstock being recycled material, e.g. plastics
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02WCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO WASTEWATER TREATMENT OR WASTE MANAGEMENT
    • Y02W30/00Technologies for solid waste management
    • Y02W30/50Reuse, recycling or recovery technologies
    • Y02W30/62Plastics recycling; Rubber recycling

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Thermal Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Environmental & Geological Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Wood Science & Technology (AREA)
  • Separation, Recovery Or Treatment Of Waste Materials Containing Plastics (AREA)

Description

WO 03/089212 PCT/IT03/00247 METHOD AND APPARATUS FOR RECOVERING CARBON AND/OR GLASS FIBERS FROM A COMPOSITE MATERIAL The present invention substantially relates to a method aimed at recovering carbon and/or glass fibers from composite materials in polymeric matrix (also known as FRP: Fiber Reinforced Plastics), coming from 5 different industrial processing stages and/or from manufacts at end of life, by means of a pyrolysis thermal treatment and of a subsequent cleaning treatment from residues, the latter being called "upgrading". 10 The involved commodity field is that of the production of second raw materials derived from industrial waste with particular attention to the mechanical die. Carbon, glass, etc. fibers are the material which 15 is wanted to be recovered from the scraps and from the industrial production waste, with a combined process of pyrolysis and subsequent upgrading of the fibers. Currently, CFRP scraps and waste are sent to dump and they represent a cost both for the firms producing 20 the waste and for the community. In fact carbon fibers, or CF, are not recovered from CFRP. The analysis of the state of art has pointed out that the results obtained with other recovery methods have not achieved conditions so as to justify the 25 industrial use thereof due to problems connected to the quality of the obtained products, to the cost of the WO 03/089212 PCT/IT03100247 2 processes or to the industrial applicability of the processes themselves. One of the main problems met in the recycle processes of carbon fibers (CF) is the separation 5 thereof from resins or from the plastic matrix in general. In fact, the separation process usually results to be uneconomical. Up to now, the dissolution of resin in chemical solvents has been the most advantageous technique 10 experimented for this purpose. However, the solvent containing the dissolved resin creates serious risks for the environment especially if the solvent quantity used for this process is high. Furthermore, this process does not allow is recovering carbon fibers from the composite materials which have already undergone the whole processing, that is the reticulation process and resin cure up to the end product. The recovery of the reinforcing fibers of the 20 composite materials -according to the invention allows to industrially reutilize, pursuant to European Community and national rules, a more and more huge waste flow, which otherwise would be destined to be confined into dump. 25 By way of information, in table 1 the consumptions in Europe of carbon fibers or CF are listed. Table 1 Consumptions of carbon fibers in Europe (Source: AKZO NOBEL FIBERS S .r.L.) 1995 1996 1997 1998 Consumption ton/year 1700 2000 2200 2700 WO 03/089212 PCT/IT03100247 3 Currently the production of carbon fibers is represented by 95% by the "3000 high-toughness filament" type, the selling price thereof fluctuates between 51.50 and 77.50 Euro/kg, according to 5 quantities. CF physical-mechanical features are considerably better than the ones of the materials used nowadays (nylon, glass fibers, etc.) to produce fabrics and tapes of unidirectional fibers. 10 In fact carbon fibers have a tensile strength ten times greater than high-resistant steels and also the other mechanical features such as compressive strength, flexural strength, torsional strength, * etc. are considerably higher than the other materials for is mechanical constructions. The rolled sections produced with CF are among the most advanced manufacts used in modern technologies. The density of these new materials is less than a half of light alloys and it is about five times smaller than steels, even if at the same 20 time it provides a much higher resistance. It is then evident that practically all construction materials can be replaced by composite materials, when hardness superficial features and/or a particular resistance to high temperatures are not required, to great advantage 25 to the considerable decrease in weight, the mechanical features of the manufact being the same. Nevertheless, the CF high market price strongly limits the use thereof in conventional uses. The increase in the CFRP utilization in 30 aeronautical, automotive, nautical, etc. industry determines a considerable increase in production waste WO 03/089212 PCT/IT03100247 4 and scraps, which currently have as end destination the dump disposal with considerable additional costs for the industry. To exactly understand the extent of the CR 5 utilization in this field, it has to be noted that the quantity of carbon fibers used to construct an aeroplane varies from 13 to 20% of the aircraft weight: this quantity is constantly increasing. The more and more considerable use of CF has 10 further determined, during the years, a set of obsolete means destined to scrapping, which, in turn, cause disposal problems. It is therefore the main object of the present invention to provide a method for recovering carbon 15 fibers from composite materials reinforced with resins, also called CFRP, aimed at reutilizing the same in the production of manufacts having mechanical features very similar to the manufacts produced with "virgin" carbon fibers. 20 This has been achieved, according to the present invention, by providing a method wherein the composite materials therefrom the reinforcing fibers have to be recovered, undergo a heat treatment which sets carbon and/or glass fibers free from the resinous matrix and 25 allows the recovery and the reutilization thereof for all the conventional applications wherein "virgin" carbon or glass fibers are used. The treatment steps are a pyrolysis of the material to decompose the resinous matrix and an "upgrading" step of the 30 recovered fibers, wherein the recycled fibers are cleaned from the carbon residues of the first step in WO 03/089212 PCT/IT03100247 5 order to allow the reutilization thereof to produce new composite materials. It is also an object of the present invention a plant for carrying out said process. 5 A better understanding of the invention will occur with the following detailed description and by referring to the figures which illustrate, by way of example and not for limitative purposes, a preferred embodiment for the carbon fibers. 10 In the drawings: Figures 1, 2 and 3 show the starting materials utilized to feed the plant performing the treatment thereof according to the method sofar described; figures 4 and 5 respectively show stereomicroscope 15 and optical microscope photos of fibers impregnated with epoxy resin; figures 7 and 8 respectively show optical microscope photo and SEM image of the solid residue after the pyrolysis treatment; 20 figure 9 shows the microanalysis performed on the fibers of figures 7 and 8; figures 10 and 11 show the SEM image of the reinforcing fibers recovered after the upgrading step; figure 12 is a block diagram underlining the main 25 steps of the developed process, either in continuous (or flow) and in batch; and figure 13 is a block diagram of the implemented plant. . The process according to the invention 30 substantially comprises two subsequent steps, pirolysis and upgrading, which take place preferably in WO 03/089212 PCT/IT03100247 6 consecutive way inside a reactor: the material pyrolysis to decompose the resinous matrix by setting free the fibers and the upgrading to clean the recycled fibers from carbon residues of the preceding step. S The upgrading is performed by supplying a reactive gas flow to the reactor: the main upgrading gases are
CO
2 , air, oxygen, vapour; they can be used on their own or mixed, even with other gases. It has to be noted that the distinction between 10 the two steps, pyrolysis and upgrading, is purely formal, since the same can take place without interruption: for example, by utilizing air as process gas, it is obtained that, during heating of the composite material, the fibers undergo the upgrading 15 while the process advances. In other words, pyrolysis and upgrading take place at the same time, since whereas some fibers undergo pyrolysis, some others are subjected to upgrading and this without interrupting the process nor adding reaction gas. 20 Advantageously, the method can be extended to any other kind of composite material formed by fibers in polymeric matrixes. As it will seen better hereinafter, the process conditions of the first and of the second step (process 25 temperature, gas flow, residence time, upgrading gas) vary with the starting material. The recovered fibers can be used for preparing manufacts, by utilizing them as such (sheets or fiber fragments) or after trimming the same. 30 It is to be noted that the pyrolysis process, which itself has been a well known process for many WO 03/089212 PCT/IT03100247 7 years, has never been applied in significant way to scraps and CFRP waste for the recovery of carbon fibers. According to the invention, to make possible this application it has been necessary to set up the 5 geometrical parameters and the management mode of the plant as well as the parameters conditioning the kinetics of the process itself. The pyrolysis, which as already said is the first step of the method which is described (figure 12), 10 consists in the thermal degradation process performed in absence of oxygen, by means of indirect heating. The material supplied to the reactor undergoes a thermal cracking, by resolving into one solid and one volatile component. is The volatile fraction can undergo cooling and partial condensation by producing one liquid fraction and one incondensable gaseous faction. The application of the pyrolysis process to CFRP leads to the following products: 20 - gaseous fraction, mainly constituted by hydrogen, methane, ethylene, ethane and carbon oxydes; - oily fraction, constituted by organic substances condensable at room temperature and pressure; - solid fraction, constituted by the recovered carbon 25 fibers coated with the residue coming from the resin cracking. Percentages and compositions of the above mentioned fractions depend upon conditions thereunder the process is performed and mainly upon: 30 - temperature of the material in the pyrolysis reactor; WO 03/089212 PCT/IT03100247 8 - working pressure; - contact time; - presence or not of catalysts. Table 2 shows the commodity composition typical 5 for CFRPs; tables 3 and 4 respectively show the immediate and average elementary analysis for CFRPs, whereas figure 6 shows the qualitative microanalysis of the resin present on starting fibers: it is to be noted the presence of 0, S and Cl in the resin. The presence 10 of Au is determined by the metalization of the sample. Tab. 2 - CFRP commodity analysis. CFRP components Chemical composition weight % Carbon fibers Carbon 54 Resin C,H,N,S,O, ecc.'a)('b 36 Antiadherent film C, H * 10 (a) percentages are calculated by comprising metals, 15 catalysts and cross-linking agents added in the preparation processes of resins and films; (b) sometimes in the resins small quantities of Cl and Br (about 0.5t) may be present due to the resin precursors (es. epichlorohydrin for epoxy resins) or to antiknock 20 compounds. Tab. 3 - CFRP immediate analysis. Humidity(%) Volatiles (%) Fixed carbon (%) Ashes (%) 0,07 32,28 66,45 1,2 Tab. 4 - Average elementary analysis for CFRP Element Percenlage C 80,8 H 2,7 N 6,5 S 1,5 O (by difference)) 7,3 Ashes 1,2 WO 03/089212 PCT/IT03100247 9 (c)it is to be noted that the organic 0 percentage is calculated by difference and therefore it comprises possible existing halogens. 5 During the first step of the process the material supplied to the plant is treated then at temperatures ranging from 250 to 700 0 C and with a residence time of a few hours. The residence time depends upon the reactor 10 geometry, upon the 02 percentage and upon the temperature. It is important to underline that, from the implementation point of view, the pyrolysis reactor and the upgrading reactor can coincide, that is they can be constituted by the same reactor wherein both 15 steps occur. The process environment is guaranteed either by pyrolysis gases developing in the reactor or by a nitrogen flow, utilized as conveying gas of the produced vapours. 20 The weight percentages of the products obtained by pyrolysis of CFRP composite materials at a process temperature of 550 0 C are the following, on the average: - 60+70% solid residue, containing recovered carbon fibers, deposited carbon, inert feedstocks and 25 metals; - 10+30% oily fraction; - 10+20% gas. Gas, mainly constituted by light hydrocarbons, has a lower calorific power equal (or net heat value) to 30 about 8,000 kcal/Nm3. It can be utilized as fuel and it helps heating the pyrolysis reactor so as to amortize process costs.
WO 03/089212 PCT/IT03/00247 10 The oily residue, which has a calorific power around 10,000 Kcal/kg, is constituted by aromatic, aliphatic components and by olefines; even such fraction can be utilized to supply energy to the S process. For the objects here described, the preferred solution consists in utilizing the pyrolysis vapours as such, without condensation, to supply energy to the process. 10 The solid residue is constituted by recovered carbon fibers and by charcoal which will be removed during the upgrading procedure of fibers. The content in ashes is almost exclusively constituted by inert feedstocks and by metals, added as is catalysts utilized during the manufacturing processes of the composite materials. It has to be noted that the weight percentage of the solid fraction differs by about 10% from the quantity of fibers existing in the original composite 20 material, as shown by data of the commodity analysis: this 10% represents the carbon residue generated by the thermal cracking of the resin (the decomposition of the polyethylene film does not produce appreciable quantities of solid residue). 25 Figures 7 and 8 show the solid residue after the pyrolysis treatment: the fibers are coated with a layer of material. The performed microanalysis, shown in figure 9, has pointed out that this material is very rich in carbon and it has appreciable quantities of 0, 30 S and Cl. The material is surely a char due to cracking of WO 03/089212 PCT/IT03/00247 11 the resin, wherein o, S and Cl were previously present. The presence of carbon residue on fibers causes a great change in their properties, by making them hard, stiff and fragile and then it prevents the reuse s thereof. JImpregnation tests of fibers with epoxy resins to obtain again the starting manufacts have demonstrated that apart from influencing the processability of fibers:,, the carbon residue strongly limits the adhesion 10 of fiber with the resin, causing to obtain inferior manufacts. The second part of the process performs indeed the "improirement" (upgrading) of recovered fibers, by implementing the removal of the carbon residue. 15 The upgrading step is consecutive to the pyrolysis step and it preferably takes place without any operation of cooling, opening and discharging of the reactor. The upgrading process could also be made either in parallel to the pyrolysis analysis or 20 subsequently, otherwise with a combined pyrolysis/upgrading process in a single step. The upgrading is carried out by supplying to the reactor a flow of reactive gas (such as for example
CO
2 , air, oxygen, vapour and mixtures of the same 25 gases) so as to remove from fibers the carbon deposits without damaging the fibers themselves. The process temperature, the gas flow and the residence time (which shows contact time of fibers with gas at the process temperature) vary according to the 30 utilized process gas. For example, by using air in mixture with nitrogen WO 03/089212 PCT/IT03/00247 12 in 30:70 proportion (02 percentage in the gaseous flow equal to 6%) at a temperature of 500+7000C with a residence time of gas in the reactor equal to about ten minutes, the residence time for the upgrading on the s average results.to be 2+3 hours. Figures 10 and 11 show the SEM image of recovered CF: as it can be seen, fibers are clean and well distinct one from the other. Table 5 shows the results of the elementary 10 analysis performed on recovered CF. Tables 6 and 7 respectively show the results of traction tests performed on virgin carbon fibers and on the ones recovered under different process conditions and the properties percentage loss. 15 Tab, 5 - Elementary analysis on recovered CF Element Percentage C 92,01 H 0,10 N 6,65 S 0 Ashes 1,2 Tab. 6 - Mechar ical tests on recovered fibers: calculation of u(N/mm 2 ) 20 breaking load Fiber length (mm) Sample 1=50 1-25 1=10 White 3302.3 36512 4556.8 A500 2873 3435.3 4065.8 A550 2711.6 2928.6 3519.1 A600 24282 2818 3223.6 WO 03/089212 PCT/IT03/00247 13 Tab. 7 - % loss in breaking load of fiber samples with respect to WHITE Fiber length (mm) Avrage Sample 1=50 1=25 1=10 value A500 13.0 5.9 10.8 9.9 A550 17.9 19.8 22.8 202 A600 26.5 22.8 29.3 262 The recovered fibers can be used for preparing manufacts, by using them as such (sheets or fiber fragments) or after trimming the same. 5 In the first case, fibers are used in the original form of fabric, by re-impregnating them with resin and by processing them, or by crumbling them and producing a casual scattering of the same on a resin layer, the MAT (non-woven fabric), which can be then processed. 10 Obviously, the procedure and preparation conditions vary according to the type of resin, or plastic material, used for preparing composite materials. Hereinafter, by way of example, the description of 15 a method used for preparing rolled sections based upon recovered carbon fibers with an epoxy resin is shown. The manufacts have been prepared starting from sheets or fragments of carbon fibers, as obtained after recovery and cleaning treatment; samples have been 20 obtained by means of impregnation in epoxy resin and subsequent polymerization and cure. A relative composition of fibers and resin of about 3/2 has been used (60% of weight by fibers, 40% of weight by resin): such composition has been 25 calculated starting from the densities of components and it allows obtaining an end manufact with a density in fiber volume equal to about 50%, WO 03/089212 PCT/IT03/00247 14 The preparation can be schematized as follows: A) Preparation of matrix The matrix has been prepared by making epoxy resin to react in stoichiometric quantities with the cross 5 linking agent (72% resin, 18% cross-linking agent) , at room temperature and until obtaining a homogeneous product. B) Preparation of preimpregnated Weighed quantities of matrix have been spread on io subsequent sheets of crossed fibers, so as to obtain a 4-layer rolled section, 10ox100 mm in size. The manufact, coated with an antiadherent film, has been firstly inserted into vacuum stove, at a pressure of 0.1 atm (to allow removing volatile substances from the is reaction environment) and then cold subjected to the pressure of some atmospheres, to uniformly impregnate the fibers with resin and to discharge threrefrom the exceeding quantity. The so-obtained preimpregnated material has been kept into refrigerator to prevent 20 resin reticulation. C) Cure and post-cure of the manufact The sample, set free from the antiadherent film, has been placed between two steel mirror plates and subjected to the cure thermal treatment, carried out 25 under press, at the temperature of 70 0 C for 2 hours, at the pressure of 6+8 atm. The preparation has ended with the post-cure treatment, performed in stove at the temperature of 140 0 C for 2 hours. By referring to the block diagram of figure 13 the 30 implemented plant provides the following main sections: 1) reaction section, wherein the pyrolysis and WO 03/089212 PCT/IT03/00247 15 upgrading steps take place in sequence; 2) fume-treating section, optional for the process, wherein the pyrolysis and upgrading vapours are treated in order to allow the discharge into 5 atmosphere of cleaned gases, as well as the cogeneration. The fume-treating section may comprise: - a "quenching" subsection (optional) , for separating the condensable fraction from the pyrolysis vapours; o - a "scrubbing" subsection (optional) , for washing the process gases from the acid components (e.g. HCl,
H
2 S, etc.); - an oxidation subsection, wherein the process gases undergo the complete oxidation to CO 2 and H 2 0 and is which provides the energy for the process; - a discharge subsection wherein the combustion fumes are cleaned and then discharged by a chimney. By using then the guidelines previously shown, summarized in figure 13, the process can be applied 20 indifferently in plants implemented for operating in batch or flow. The process for the recovery of fibers according to the present invention has been experimented by using a "CRFP" pilot plant designed and manufactured to 25 develop the treatment Figure 14 is a simplified process diagram of the implemented plant. The main procedures of the processing are: 1) Reactor loading; 30 2) material pyrolysis; 3) upgrading; WO 03/089212 PCT/IT03/00247 16 4) cooling and discharge. In this case, as there has been already a chance to mention, the two steps take place in sequence in the same reactor. 5 The statement that the distinction between the two steps is to be considered purely formal, is confirmed by the fact that they can take place also without an evident separation; for example, it is possible to provide a "flow" plant wherein a fluid bed exploiting io air as process gas is utilized as reactor: in such case, fibers will be supplied from the bottom in the same direction of gas. Therefore, it is possible to implement a heating gradient from the bottom upwards, so that in the low area of the reactor the first is pyrolysis step takes place (in this case temperature is low and air does not react) ; as the gas gradually transports fibers in areas with higher temperature, the upgrading reaction begins to be thermodinamically promoted, which then, upon leaving the reactor, 20 completes the fiber recovery process. Another possible solution, wherein different areas of a same reactor are used to make the "flow" process to occur, is to utilize a conveyor belt for transportation, or a "drop-in" system of the material, 25 always in the same direction .of the process gas, but in opposite direction to the heater vector, so as to implement the conditions mentioned above. However, the flow process can be implemented by simply following the diagram of figure 12 and by 30 utilizing for the pyrolysis and upgrading steps two rotating-drum reactors, in series one to the other, or WO 03/089212 PCT/IT03/00247 17 any other technology usually utilized to carry out thermotreating processes. Advantageously, it is also possible to utilize the same plant as described in figure 14 to carry out the s "flow" process, by implementing other two reactors which utilize the same section of treating vapours and fumes; in this case the three reactors will be operated alternatively, so that when the reactor 1 is in the process step, the reactor 2 is in the loading and 10 heating step and the reactor 3. is in the cooling and discharging step. At this point, it is interesting to examine in more details the conditions of the upgrading step. What follows refers to the upgrading step of is fibers performed under ideal conditions (in laboratory, by neglecting problems due to scattering or reactor geometry) by utilizing oxygen as upgrading gas. The used oxygen is that of the air, enriched during some tests (as it will be seen later) with 20 technical oxygen. Although hereinafter carbon fibers are referred to, the same considerations can be extended to glass, kevlar, etc. fibers. Table Al shows the dependence of cleaning time 25 upon process temperature by utilizing air as upgrading gas.
WO 03/089212 PCT/IT03/00247 18 Table Al Sample Cleaning time (min.) Temperature ("C) 1 60 500 2 20 550 3 10 600 4 2 700 Other tests have been performed under the same conditions as above highlighted, by utilizing a flow of air enriched with oxygen to increase the quantity of 5 reactive agent, the flows being the same. Table A2 relates to the dependance of cleaning time upon process temperature by utilizing air enriched with oxygen (02 end content 45%) as upgrading gas. 10_ _Table A2 Sample Cleaning time (min.) Temperature ("C) 5 180 400 6 90 450 7 20 500 Table A3 shows the dependance of cleaning time upon the 02 percentage present in the gaseous flow at the temperature of 500 0 C. Table A3 Sample Cleaning time (min.) % 02 8 60 20 9 50 25 10 40 30 11 25 37 12 20 45 15 By examining the features of the treated fibers, it has been noted that an increase in the oxygen percentage in the gaseous flow, even if it leads to a decrease in the cleaning time, attacks fibers in an eccessive way, by determining the weakening thereof in WO 03/089212 PCT/IT03/00247 19 some places. Therefore, the use of air (not enriched) guarantees a more controlled, even if slower, reaction. Based upon the data shown in tables Al+A3 it has 5 been chosen to utilize an operating temperature of about 500+600 0 C in air, to be experimented then on pilot scale. However, it is to be underlined that data refer to ideal conditions, that is experiments carried out in 10 single layer and on small samples (absence of scattering phenomena due to the sample mass and to the reactor geometry). What has been said can be extended to upgrading processes which use different reactive gases such as is C0 2 , steam and others, used on their own or in mixture, able to remove the residual charcoal from the pyrolysis process of fibers by reaction. It has to be highlighted that the optimum process conditions (process temperature, residence time, speed 20 of gaseous flow, etc.) vary with the used gas and the type and quantity of treated material. For example, it is known that the conversion reaction of coal with CO 2 is much slower than the one with oxygen and it takes place in significant way from 800 0 C upwards. 25 A process utilizing carbon dioxide as upgrading gas has the drawback of longer residence time of the material in contact with gas, higher temperatures (therefore higher energy consumption), but it involves a more controlled attack of the reagent (less 30 aggressive) and then less damage to fibers. Similar remarks can be made for steam or gas WO 03/089212 PCT/IT03/00247 20 mixtures. The use of the method sofar described involves several advantages: - possibility of recovering carbon and glass fibers 5 from composite materials of the same reinforced with epoxy resins (FRP), coming from scraps and waste produced in different industrial processing steps and from manufacts at end of life; the recovered fibers can be reutilized in the production of 10 manufacts with mechanical features very similar to the ones produced with "virgin" carbon fibers; - potential economic saving due to missed conferring to dump of scraps and waste produced in different industrial processing steps and from manufacts at is end of life; - availability of a "source" of carbon, glass, etc. fibers, to manufacture composite materials, also in countries where the production of such fibers does not exist; 20 - possibility of obtaining carbon fibers with considerable reduced costs and with mechanical properties similar to "virgin" fibers; - the lower cost of recovered fibers compared to "virgin" fibers makes possible the use thereof for 25 new applications, up to now not considered for the high price of the "new" material. - the recovered fibers can be reutilized as such in the manufacturing process of new composite materials or they can be trimmed and reutilized to produce MAT 30 (unwoven fabric), by utilizing fibers distributed randomly on a layer or to produce felts.
WO 03/089212 PCT/IT03/00247 21 The present invention has been described and illustrated in a preferred embodiment thereof, but it is clear that any person skilled in the art could apply modifications and/or replacements equivalent from the s technical and/or operating point of view, however comprised within the protective scope of the present industrial invention.

Claims (14)

1. Method for recovering reinforcing fibers from composite materials of the same in polymeric matrixes (also known as FRP: Fiber Reinforced Plastics), coming 5 from different industrial processing stages and/or from manufacts at end of life, characterized in that the composite materials therefrom the reinforcing fibers have to be recovered undergo a thermal treatment in two steps apt to set free the reinforcing fibers (for 10 example of carbon and/or glass) from the plastic matrix by allowing the recovery and reuse thereof for all the conventional applications wherein "virgin" reinforcing fibers are utilized; said two steps of the treatment respectively being a pyrolysis of the material apt to is decompose the plastic matrix by setting free the fibers, followed by an "upgrading" step of the recovering fibers, wherein the recycled fibers are cleaned from carbon residue of the pyrolysis step in order to allow the reuse thereof for manufacturing new 20 composite materials.
2. Method according to claim 1, characterized in that said two subsequent steps, pyrolysis and upgrading, take place in consecutive way inside a reactor. 25
3. Method according to the preceding claim, characterized in that the upgrading step is performed by supplying to the reactor a flow of reactive gas suitable to react with the carbon residue of pyrolysis, such as for example carbon dioxide, air, oxygen, 30 vapour, which are utilized on their own or in mixture in any percentage, also with other gases. WO 03/089212 PCT/IT03/00247 23
4. Method according to anyone of the preceding claims, chararacterized in that the pyrolysis step is performed by thermally degrading the composite material to be treated in absence of oxygen, so that the s material supplied to the reactor undergo a thermal cracking, by resolving into one solid and one volatile component.
5. Method according to anyone of the preceding claims, chararacterized in that during the pyrolysis 10 step the material is treated at temperatures ranging between 250-750 0 C and with a residence time of some hours, depending upon the typology of the material to be treated, the geometry of the reactor, the temperature, and all other process conditions. 15
6. Method according to anyone of the preceding claims, chararacterized in that the process environment is guaranteed either by the same pyrolysis gases developing into the reactor and by the use of a flow of an inertization gas, utilized also as conveying gas of 20 the produced vapours.
7. Method according to the preceding claim, characterized in that the process vapours are utilized as fuel and contribute to heat the reactor so as to amortize process costs. 25
8. Method according to claim 2, characterized in that the upgrading step preferably occurs without any cooling, opening and discharge procedure of the reactor.
9. Method according to anyone of the preceding 30 claims, chararacterized in that the treated materials are scraps and processing waste and manufacts at end of WO 03/089212 PCT/IT03/00247 24 life of FRP and they are processed without any pretreatment.
10. Method according to the preceding claims, characterized in that the recovered fibers are reused 5 as such in the manufacturing process of new composite materials, or they are trimmed and utilized to produce MAT (non-woven fabric), by utilizing fibers distributed randomly on a layer or to produce felts.
11. Plant for the recovery of reinforcing fibers 10 from the composite materials of the same in polymeric matrixes (also known as FRP: Fiber Reinforced Plastics), coming from different industrial processing stages and/or manufacts at end of life, characterized in that it comprises a reaction section, wherein the 15 pyrolysis and upgrading steps take place in sequence.
12. Plant according to the preceding claim, characterized in that it further comprises a fume treating section, wherein the pyrolysis and upgrading vapours are treated to allow discharging the cleaned 20 gases into air, as well as the cogeneration.
13. Plant according to claim 11 or 12, characterized in that it comprises: a) an oxidation subsection, wherein the process gases undergo the complete oxidation to CO 2 and H20 and 25 which provides the energy for the process; b) a discharge subsection wherein the combustion fumes are cleaned and then discharged by a chimney.
14. Plant according to the preceding claim, characterized in that it further comprises: 30 - a "quenching" subsection, for separating the condensable fraction from the pyrolysis vapours; WO 03/089212 PCT/IT03/00247 25 - a "scrubbing" subsection for washing the process gases from the acid components (such as for example HC1, H 2 S, etc.).
AU2003236029A 2002-04-19 2003-04-17 Method and apparatus for recovering carbon and/or glass fibers from a composite material Abandoned AU2003236029A1 (en)

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