Figure 3. Materials evolutionThe properties and price of carbon fibers alsoencompass a broad territory. With the pricedecreasing of the higher filament numbered (higherthan 24K), carbon tows produced for commercialusage, the greater volume and the wider industrialusage came to prominence and this tendency,expectedly, will continue.The Carbon Fiber is made mostly (approx; 95 %) from asynthetic fiber well known in the textile industry,namely PAN (Polyacrylonitrile), and it is so calledprecursor fiber (Figure 4), whereas the raw material ofthe remaining 5 % is either tar or regenerated fibers.ACTA TECHNICA CORVINIENSIS – Bulletin of Engineeringfrom the fiber, while its chemical structure changes.The OPAN fiber (approximate with 62% of carboncontent) formed after oxidation, becomes a textilematerial having excellent heat, flame and fire resistantproperties, which after various textile industryoperations (Stretch ‐ Breaking, Carding, Spinning,Weaving, Knitting, or in Tow / Staple fiber form usingnon‐woven methods) may be further processed.Products’ made from OPAN do not melt, have a highLOI value (40‐60), its heat resistance is above (300 ⁰C),and because of this, they are mainly used in areaswhere heat, fire resistance, heat insulation (weldingblankets, protective clothing, etc.) is required. Duringthe oxidation process, a crust forms on the surface ofthe OPAN fiber, and because of this, its loop tenacity islow (8‐15% of the tensile strength), thusly the fiber isbrittle. By increasing of the temperature andprocessing time, the density of OPAN fiber (ρ=1.35‐1.42g/cm³) can also be increased, and with this, heatresistance of the material can be augmented, but thefiber will be more rigid. Although OPAN and carbonfibers are both black, their other properties arebasically different (Figure 6.).Figure 4. Manufacturing processof carbon fibers (PAN‐based)The PAN precursor based oxidized fiber (OPAN),carbon and graphite fiber production process is welldepicted in Figure 5.Figure 6. Properties of OPAN and carbon fibersOPAN products processed by textile industry methodsand then carbonized can be used in a variety of uniqueapplications.In the hydrogen driven electrical transformer, thecarbon membrane allows the protons to pass throughwhile by separating the electrons, electric current isgenerated.In the case of sodium‐sulphur electrical energy storing,the sulphur is stored in the carbonized OPANmembrane sponge.In the C‐C composite technology, the thick felt madefrom OPAN is carbonized at high temperature and theC is diffused into the material. From the thuslycreated, compact structured CandC compositematerial, high temperature 1000 ⁰C bearing, aircraftand racing car brake discs and brake pads are made.In the manufacturing of carbon fiber, by leading thepre‐tensioned fibers exiting from the oxidation oveninto high temperature (800‐1500 ⁰C) nitrogen gasblanketed ovens, the structure of the carbon fiber isformed (Figure 7).Figure 5. The oxidation, carbonizationand graphitisation processThe OPAN fiber is produced by oxidizing themoderately stretched PAN fiber at 220‐250 ⁰C. In theprocess of the oxidation, taking several hours, most ofthe burnable gases and toxic materials are exhausted54Figure 7. Structure of carbon fiber2012. Fascicule 3 [July–September]
ACTA TECHNICA CORVINIENSIS – Bulletin of EngineeringTo forward chemical bonding with the matrix materialof the composite, after exiting from the ovens, thesurface of the fibers is activated and sizing is alsocarried on to their surface.In the course of graphite production the pre‐tensionedfibers are further led through high temperature(2000‐3000 ⁰C) nitrogen gas blanketed ovens. The rawmaterial, production technology parameters(tensioning zones, stressing level, temperatures,surface treatment etc.) all have deciding effect on theproperties of the fiber (by increasing the temperature,rigidity of the fiber also increases), thusly tenacity andstiffness properties of the carbon fibers encompass awide range.The carbon fiber, without twisting is wound onto 5‐12kg‐ spools. To avoid twisting, the tow is unwoundtangentially from the rotating spool. The diameter ofthe carbon fiber is around 5‐7 μm (approx. 0.4 – 0.7dtex). The thickness of the carbon tow is defined bythe number of single filaments it contains, where(K=1000) (1K, 2K, 6K, 12K, 24K, 50K, 60K, 300K, etc.).The tows may also be used in the following forms: Milled powder (less than one mm long) form, orcompacted into chips / pellet form. Chopped (3‐10 mm), As tow, by direct extruding. Laid, spreaded tow, wound or, Using various textile technical methods, variouslystructured sheet forms (UD, BD, MD or 3D may beattained). Impregnated (pre‐pregs) or using thedry infusion process, embedded in matrixmaterial, they can be used as compositereinforcement (Figure 8).Figure 8. Product forms of carbon fibersFrom further processing point of the carbon fiber, it isimportant that the filaments in the tow be orientedand parallel. It is expedient to guide the carbon fiber –similarly to the Kevlar – on orange peel formed towguiding elements.At unwinding of the tows, tow forces should beidentical, minimal and independent from changes inthe diameter of the spool, in short, it must beconstant. At the unwinding creel, when positioningthe tow spools at the lateral guiding of the tows, onemust strive to minimize any breaks and that towsarrive parallel to the positioning reed. During theguiding, contact between the tows must be reducedto the minimum, overlapping of the tows is notallowed.In the 50K, 6‐10 mm wide tow, there are 35‐60filament layers on top of each other. During sheetformation, it is important that the tow filaments bespread homogenously, without gaps in the plane ofthe fabric. Namely, uniform penetration of the matrixinto the thick filament layers is not ensured andbecause of this, the tows, by spreading them, arewidened and thinned out. An important aim, is theformation of homogenous, gap free, thin, low areadensity (80‐120 g/m²) filaments, which make it possibleto form light, selective and valuable compositestructures (Figure 9).Figure 9. Spreading carbon tow and fabricTable 1. The mechanical properties of metalsC – HTHighTenacityC – IMIntermediateModulusDichte ρ g/cc 1.74 1.80Elongation at break % 1.50 1.93Tensile strength, σ MPa 3600 5600Specific tensile strength σ*cN/tex (km)206 301Tensile modulus E GPa 240 290Specific tensile modulus E*cN/tex (km)13800 16100Long time heat resistance ⁰C 500 500Coefficient of Liner ThermalExpansion, α 10−⁶/ ⁰C‐0.91 ‐0.91Fiber diameter, d, μm 7 5Melting / Sublimation ⁰C 3600 3600C – HMHighModulusC – HMSHigh ModulusStrengthE ‐GlassAluminumSteel1.83 1.85 2.55 2.70 7.850.57 0.63 2.5 1.82300 3600 2470 70‐700 2880125194 95 36400 550 70 70 2002185029730 2700 2500500 500‐0.91‐0.91 4‐9 22.2 136.5 5 7‐133600 3600 840 660 1500Spreading of the tow can be intensified by eliminatingtwists, reducing sizing, ensuring long free guiding,heating, vibrating and by blowing air on it.Carbon fiber is a high tenacity, high modulus brittlematerial, and because of this, in its processing, specialhandling is required. Since the density of carbon fiber(ρ≈1.8 g/cm³) and fiber reinforced composites (ρ≈1.4g/cm³) is small, their tenacity, in relation to the weightof the material (σ* = σ/ρg) and their elasticity modulus(E* = E/ρg) values considerably surpass the mechanicalproperties of metals (Table 1).Tensile strength of the various materials, in generalengineering practice is expressed to cross section2012. Fascicule 3 [July–September] 55
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