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Relevant bibliographies by topics / Carbon fiber

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Academic literature on the topic 'Carbon fiber'

Author: Grafiati

Published: 4 June 2021

Last updated: 11 September 2023

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Journal articles on the topic "Carbon fiber"

1

Mishra, Shivam. "Application of Carbon Fibers in Construction." Journal of Mechanical and Construction Engineering (JMCE) 2, no. 2 (2022): 1–7. http://dx.doi.org/10.54060/jmce.v2i2.20.

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Carbon fibers (also known as graphite fibers) are high-performance fibers, about five to ten micrometers in diameter, composed mainly of carbon, with high tensile strength. Plus, they are extremely strong with respect to their size. They have high elastic modulus in comparison with glass fiber. According to the working period, carbon fibre-reinforced polymers possess more potential than those with glass fiber. However, they are relatively expensive as compared to similar fibers, such as glass fiber, basalt fiber, or plastic fiber. Its high quality, lightweight, and imperviousness to erosion, make it a perfect strengthening material. Carbon fibre-reinforced composite materials are used to make aircraft parts, golf club shafts, bike outlines, angling bars, car springs, sailboat masts, and sev-eral different segments which need to have less weight and high quality.

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Yang, Lian Wei, Yun Dong, and Rui Jie Wang. "Wear and Mechanical Properties of Short Carbon Fiber Reinforced Copper Matrix Composites." Key Engineering Materials 474-476 (April 2011): 1605–10. http://dx.doi.org/10.4028/www.scientific.net/kem.474-476.1605.

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The mechanical properties and wear behavior of short carbon fiber reinforced copper matrix composites was studied. In order to avoid any interfacial pronlems in the carbon fibre reinforced composites, the carbon fibers were coated with copper. The fibers were coated by electroless coating method and then characterized. Composites containing different amounts of carbon fibers were prepared by hot pressing technique. The results show that Carbon fiber/Cu–Ni–Fe composites showed higher hardness, higher wear resistance and bending strength than the common copper alloy when carbon fibers content is less than 15 vol.%. The predominant wear mechanisms were identified as adhesive wear in the alloy and adhesive wear accompanied with oxidative wear in the 12 vol.% carbon fiber/Cu–Ni–Fe composites.

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Zaldivar, Rafael J., Gerald S. Rellick, and J. M. Yang. "Fiber strength utilization in carbon/carbon composites." Journal of Materials Research 8, no. 3 (March 1993): 501–11. http://dx.doi.org/10.1557/jmr.1993.0501.

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The utilization of tensile strength of carbon fibers in unidirectional carbon/carbon (C/C) composites was studied for a series of four mesophase-pitch-based carbon fibers in a carbon matrix derived from a polyarylacetylene (PAA) resin. The fibers had moduli of 35, 75, 105, and 130 Mpsi. Composite processing conditions ranged from the cured-resin state to various heat-treatment temperatures (HTT's) from 1100 to 2750 °C for the C/C's. Room-temperature tensile strength and modulus were measured for the various processing conditions, and were correlated with SEM observations of fracture surfaces, fiber and matrix microstructures, and fiber/matrix interphase structures. Fiber tensile strength utilization (FSU) is defined as the ratio of apparent fiber strength in the C/C to the fiber strength in an epoxy-resin-matrix composite. Carbonization heat treatment to 1100 °C results in a brittle carbon matrix that bonds strongly with the three lower modulus fibers, resulting in matrix-dominated failure at FSU values of 24 to 35%. However, the composite with the 130-Mpsi-modulus filament had an FSU of 79%. It is attributed to a combination of tough fracture within the filament itself and a weaker fiber/matrix interface. Both factors lead to crack deflection and blunting rather than to crack propagation. The presence of a weakened interface is inferred from observations of fiber pullout. Much of the FSU of the three lower modulus fibers is recovered by HTT to 2100 or 2400 °C, principally as a result of interface weakening, which works to prevent matrix-dominated fracture. With HTT to 2750 °C, there is a drop in FSU for all the composites; it is apparently the result of a combination of fiber degradation and reduced matrix stress-transfer capability.

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Bedmar, Javier, Belén Torres, and Joaquín Rams. "Manufacturing of Aluminum Matrix Composites Reinforced with Carbon Fiber Fabrics by High Pressure Die Casting." Materials 15, no. 9 (May 9, 2022): 3400. http://dx.doi.org/10.3390/ma15093400.

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Aluminum matrix composites reinforced with carbon fiber have been manufactured for the first time by infiltrating an A413 aluminum alloy in carbon fiber woven using high-pressure die casting (HPDC). Composites were manufactured with unidirectional carbon fibers and with 2 × 2 twill carbon wovens. The HPDC allowed full wetting of the carbon fibers and the infiltration of the aluminum alloy in the fibers meshes using aluminum at 680 °C. There was no discontinuity at the carbon fiber-matrix interface, and porosity was kept below 0.1%. There was no degradation of the carbon fibers by their reaction with molten aluminum, and a refinement of the microstructure in the vicinity of the carbon fibers was observed due to the heat dissipation effect of the carbon fiber during manufacturing. The mechanical properties of the composite materials showed a 10% increase in Young’s modulus, a 10% increase in yield strength, and a 25% increase in tensile strength, which are caused by the load transfer from the alloy to the carbon fibers. There was also a 70% increase in elongation for the unidirectionally reinforced samples because of the finer microstructure and the load transfer to the fibers, allowing the formation of larger voids in the matrix before breaking. The comparison with different mechanical models proves that there was an effective load transference from the matrix to the fibers.

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Wang, Xiaojun, Xuli Fu, and D. D. L. Chung. "Strain sensing using carbon fiber." Journal of Materials Research 14, no. 3 (March 1999): 790–802. http://dx.doi.org/10.1557/jmr.1999.0105.

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Carbon fiber provides strain sensing through change in electrical resistance upon strain. Due to piezoresistivity of various origins, a single carbon fiber in epoxy, an epoxy-matrix composite with short carbon fibers (5.5 vol%), a cement-matrix composite with short carbon fibers (0.2–0.5 vol%), and an epoxy-matrix composite with continuous carbon fibers (58 vol%) are strain sensors with fractional change in resistance per unit strain up to 625. A single bare carbon fiber is not piezoresistive, but just resistive.

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Markovičová, Lenka, Viera Zatkalíková, and Patrícia Hanusová. "Carbon Fiber Polymer Composites." Quality Production Improvement - QPI 1, no. 1 (July 1, 2019): 276–80. http://dx.doi.org/10.2478/cqpi-2019-0037.

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Abstract Carbon fiber reinforced composite materials offer greater rigidity and strength than any other composites, but are much more expensive than e.g. glass fiber reinforced composite materials. Continuous fibers in polyester give the best properties. The fibers carry mechanical loads, the matrix transfers the loads to the fibers, is ductile and tough, protect the fibers from handling and environmental damage. The working temperature and the processing conditions of the composite depend on the matrix material. Polyesters are the most commonly used matrices because they offer good properties at relatively low cost. The strength of the composite increases along with the fiber-matrix ratio and the fiber orientation parallel to the load direction. The longer the fibers, the more effective the load transfer is. Increasing the thickness of the laminate leads to a reduction in the strength of the composite and the modulus of strength, since the likelihood of the presence of defects increases. The aim of this research is to analyze the change in the mechanical properties of the polymer composite. The polymer composite consists of carbon fibers and epoxy resin. The change in compressive strength in the longitudinal and transverse directions of the fiber orientation was evaluated. At the same time, the influence of the wet environment on the change of mechanical properties of the composite was evaluated.

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Wang, Jian Ming, Lei Zhao, and Xiao Qin. "Study on the Mechanical Properties of Jute/Carbon Hybrid Composites." Advanced Materials Research 331 (September 2011): 110–14. http://dx.doi.org/10.4028/www.scientific.net/amr.331.110.

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Carbon fibers were used to lay lengthways into three lays in jute fiber needled mat and the same fiber volume content of jute fiber needled mat were fabricated. Those two mats and the lengthways carbon fibers reinforced vinyl resin composites were made by VARTM. We made a comparison of the hybrid reinforced composites between the test value and the theoretical value which was predicted by establishing tensile and bending math-model and their mechanical properties were analyzed. The results show that there was a certain line between the theoretical value and the test value of the hybrid composites, so we can establish the mixing ratio between jute fiber and carbon fiber during the engineering application. Although the use of carbon fibers had greatly enhanced the tensile properties of hybrid composite, whose tensile strength and tensile modulus increased by 85.94% and 30.99% respectively than that without carbons, the bending model can’t be changed a lot.

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Reichert, Olaf, Larisa Ausheyks, Stephan Baz, Joerg Hehl, and Götz T. Gresser. "Innovative rC Staple Fiber Tapes - New Potentials for CF Recyclates in CFRP through Highly Oriented Carbon Staple Fiber Structures." Key Engineering Materials 809 (June 2019): 509–14. http://dx.doi.org/10.4028/www.scientific.net/kem.809.509.

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Increasing waste streams of carbon fibers (CF) and carbon fiber reinforced plastics (CFRP) lead to increasing need for recycling and to growing amounts of recycled carbon fibers. A main issue in current research for carbon fiber recycling is the reuse of regained fibers. Carbon staple fibers such as recycled fibers hold big potential for mechanical properties of lightweight parts, if used properly. Applying recycled CF (rCF) as milled reinforcement fibers or as nonwoven in carbon fiber reinforced plastic leads to a poor yield of mechanical proper due to low fiber orientation, limitations in fiber volume content or due to short fiber length. The rC staple fiber tape presents a more efficient approach. Recycled carbon fibers are blended with 50 wt. % thermoplastic nylon 6 fibers and processed through a roller card to a sliver, which is a linear fibrous intermediate. The sliver is continuously drawn, formed, heated and consolidated to the thermoplastic rC staple fiber tape. The tape is similar to common carbon fiber tapes or to continuous tows but has different positive properties, such as high fiber orientation, homogeneous blend of fiber and matrix and suitability for deep drawing.

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Radulović, Jovan. "Hybrid filament-wound materials: Tensile characteristics of (aramide fiber/glass fiber)-epoxy resins composite and (carbon fibers/glass fiber)-epoxy resins composites." Scientific Technical Review 70, no. 1 (2020): 36–46. http://dx.doi.org/10.5937/str2001036r.

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In this paper a tensile characteristics of filament-wound glass fiber-aramid fiber/epoxy resins hybrid composites and glass fiber-two carbons fibers/epoxy resins hybrid composites are presented. Basic terms about hybride composite materials (origin, reasons for manufacturing, advantages, definitions, levels of hybridization, modes of classifications, types, categorization, and possible interactions between constituents) and used reinforcements and matrices are described. For a manufacturing of NOL rings four reinforcements (glass fiber, polyamide aromatic fiber and two carbon fibers) and two matrices (high and moderate temperature curing epoxy resin system) are used. Based on experimentally obtained results, it is concluded that hybride composite material consisting of carbon fiber T800 (67 % vol) and glass fiber GR600 (33 % vol) impregnated with epoxy resin system L20 has the highest both the tensile strength value and the specific tensile strength value. The two lowest values of both tensile strength and the specific tensile strength have hybrid material containing aramide fiber K49 (33 % vol) and glass fiber GR600 (67 % vol) and epoxy resin system 0164 and hybrid NOL ring with wound carbon fiber T300 (33 % vol) and glass fiber GR600 (67 % vol) impregnated with the same epoxy resin system. This investigation pointed out that increasing the volume content of aramide fiberK49, carbon fiber T300 and carbon fiber T800 in appropriate hybrid composites with glass fiber GR600 increases both the tensile strength value and the specific tensile strength value and decrease the density value, no matter the used epoxy resin system.

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Xie, Wei, Hai Feng Cheng, Zeng Yong Chu, Zhao Hui Chen, Yong Jiang Zhou, and Chun Guang Long. "Comparison of Hollow-Porous and Solid Carbon Fibers as Microwave Absorbents." Advanced Materials Research 150-151 (October 2010): 1336–42. http://dx.doi.org/10.4028/www.scientific.net/amr.150-151.1336.

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A series of polyacrylonitrile-based hollow-porous and solid carbon fibers were prepared by pyrolysis of polyacrylonitrile-based hollow-porous and solid fibers at the same condition. The microstructure, composition, surface electrical conductivity, electromagnetic parameters and reflectivity of carbon fibers were studied. The microwave absorbing properties of two kinds of carbon fibers as microwave absorbents were parallel investigated. Results show that the apparent density of the hollow-porous carbon fibers is lower than that of the solid carbon fibers due to their hollow-porous structure. The surface electrical conductivity of single solid carbon fiber is nearly 10 times that of the hollow-porous carbon fiber. The -10dB bandwidths of solid carbon fiber composites carbonized at 850 and 950°C are both 0GHz, while those of the corresponding hollow-porous carbon fiber composites are up to 3.05 and 2.62GHz, respectively. Results indicate that the microwave absorbing properties of the hollow-porous carbon fiber composites are better than those of solid carbon fiber composites.

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Dissertations / Theses on the topic "Carbon fiber"

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Heisey, Cheryl L. "Adhesion of novel high performance polymers to carbon fibers : fiber surface treatment, characterization, and microbond single fiber pull-out test /." Diss., This resource online, 1993. http://scholar.lib.vt.edu/theses/available/etd-02052007-081244/.

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Luo, Jie. "Lignin-Based Carbon Fiber." Fogler Library, University of Maine, 2010. http://www.library.umaine.edu/theses/pdf/LuoJ2010.pdf.

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Deng, Yuliang. "Carbon fiber electronic interconnects." College Park, Md. : University of Maryland, 2007. http://hdl.handle.net/1903/6997.

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Thesis (Ph. D.) -- University of Maryland, College Park, 2007.
Thesis research directed by: Mechanical Engineering. Title from t.p. of PDF. Includes bibliographical references. Published by UMI Dissertation Services, Ann Arbor, Mich. Also available in paper.

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Joshi, Ninad Milind. "Study of the Effect of Unidirectional Carbon Fiber in Hybrid Glass Fiber / Carbon Fiber Sandwich Box Beams." University of Dayton / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1386188162.

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D'Angelo, Emanuele <1989&gt. "Carbon fiber reinforced polymers: matrix modifications and reuse of carbon fibers recovered by pyrolysis." Doctoral thesis, Alma Mater Studiorum - Università di Bologna, 2018. http://amsdottorato.unibo.it/8363/1/Emanuele_D_Angelo_thesis.pdf.

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Due to their extraordinary properties, Carbon Fiber Reinforced Polymers (CFRPs) are used in a growing number of fields (automotive, military, aircraft, aerospace, wind turbines, sport, civil infrastructure and leisure). Since the matrix in CFRPs is polymer-based, these composites have poor resistance to fire; additionally, when exposed to high temperatures, they can burn or lose their thermo-mechanical stability. Moreover, the recent huge and continuous development of CFRPs opened the question related to their disposal and total dependence on fossil resources. This thesis focussed on epoxy-based CFRPs. In more detail, commercial epoxy resins have been modified and replaced with bio-based alternatives, and short recycled carbon fibers composites have been produced. Two new bentonite-based organoclays were prepared with low cost reactants and mild reactions conditions and used to modify the flame behaviour of a commercial epoxy resin. The epoxy-modified resin flame behaviour was evaluated by cone-calorimeter and some significant improvements with just a 3 %wt loading level of organoclay were obtained. Furthermore, the possibility to recover and reuse carbon fibers by pyrolysis of CFRPs waste was studied: a validation of the recycling conditions and the treatments required to reuse recycled carbon fibers were assessed in order to obtain clean fibers and promote fiber/matrix adhesion in epoxy composites. Recycled carbon fiber were then used in a lab-scale composite manufacturing process and comparable mechanical properties for virgin and recycled short carbon fiber composites were achieved when an optimized coupled pyrolysis/oxidative process to CFRPs waste is applied. Finally, more sustainable CFRPs have been produced and characterized coupling highly bio-based epoxy systems, appropriately modified and optimized, and recycled carbon fibers. This latter work represents the first attempt aimed at replacing petroleum- BPA-based epoxy resins and high cost short virgin carbon fibers in the future CFRPs manufacturing processes.

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Newcomb, Bradley Allen. "Gel spun PAN and PAN/CNT based carbon fibers: From viscoelastic solution to elastic fiber." Diss., Georgia Institute of Technology, 2015. http://hdl.handle.net/1853/54881.

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This study focuses on the processing, structure, and properties of gel spun polyacrylonitrile (PAN) and polyacrylonitrile/carbon nanotube (PAN/CNT) carbon fibers. Gel spun PAN based carbon fibers are manufactured beginning with a study of PAN dissolution in an organic solvent (dimethylformamide, DMF). Homogeneity of the PAN/DMF solution is determined through dynamic shear rheology, and the slope of the Han Plot (log G’ vs log G’’). Solutions were then extruded into gel spun fibers using a 100 filament fiber spinning apparatus in a class 1000 cleanroom. Fibers were then subjected to fiber drawing, stabilization, and carbonization, to convert the PAN precursor fiber into carbon fiber. Carbon fiber tensile strength was shown to scale with the homogeneity of the PAN/DMF solution, as determined by the slope of the log G’ vs log G’’ plot. After the development of the understanding between the homogeneity of the PAN/DMF solutions on the gel spun PAN based carbon fiber tensile properties, the effect of altering the fiber spinning processing conditions on the gel spun PAN based carbon fiber structure and properties is pursued. Cross-sectional shape of the gel spun PAN precursor fiber, characterized with a stereomicroscope, was found to become more circular in cross-section as the gelation bath temperature was increased, the amount of solvent in the gelation bath was increased, and when the solvent was switched from DMF to dimethylacetamide (DMAc). Gel spun fibers were then subjected to fiber drawing, stabilization, and carbonization to manufacture the carbon fiber. Carbon fibers were characterized to determine single filament tensile properties and fiber structure using wide-angle x-ray diffraction (WAXD) and high resolution transmission electron microscopy (HRTEM). It was found that the carbon fiber tensile properties decreased as the carbon fiber circularity increased, as a result of the differences in microstructure of the carbon fiber that result from differences in fiber spinning conditions. In the second half of this study, the addition of CNT into the PAN precursor and carbon fiber is investigated. CNT addition occurs during the solution processing phase, prior to gel spinning. As a first study, Raman spectroscopy is employed to investigate the bundling behavior of the CNT after gel spinning and drawing of the PAN/CNT fibers. By monitoring the peak intensity of the (12,1) chirality in the as-received CNT powder, and in differently processed PAN/CNT fibers, the quality of CNT dispersion can be quickly monitored. PAN/CNT fibers were then subject to single filament straining, with Raman spectra collected as a function of PAN/CNT filament strain. As a result of the PAN/CNT strain, stress induced G’ Raman band shifts were observed in the CNT, indicating successful stress transfer from the surrounding PAN matrix to the dispersed CNT. Utilization of the shear lag theory allows for the calculation of the interfacial shear strength between the PAN and incorporated CNT, which is found to increase as the quality of CNT (higher aspect ratio, increased graphitic perfection, and reduced impurity content), quality of CNT dispersion, and fiber drawing increase. PAN/CNT fibers were then subjected to stabilization and carbonization for the manufacture of gel spun PAN/CNT based carbon fibers. These fibers were then characterized to investigate the effect of CNT incorporation on the structure and properties of the carbonized fibers. The gel spun PAN/CNT based carbon fibers were compared to commercially produced T300 (Toray) and IM7 (Hexcel) carbon fibers, and gel spun PAN based carbon fiber. Fiber structure was determined from WAXD and HRTEM. Carbon fibers properties investigated include tensile properties, and electrical and thermal conductivity. PAN/CNT based carbon fibers exhibited a 103% increase in room temperature thermal conductivity as compared to commercially available IM7, and a 24% increase in electrical conductivity as compared to IM7. These studies provide a further understanding of the processing, structure, property relationships in PAN and PAN/CNT based carbon fibers, beginning at the solution processing phase. Through the manufacture of more homogeneous PAN/DMF solutions and investigations of the fiber spinning process, gel spun PAN based carbon fibers with a tensile strength and modulus of 5.8 GPa and 375 GPa, respectively, were successfully manufactured in a continuous carbonization facility. Gel spun PAN/CNT based carbon fibers exhibit room temperature electrical and thermal conductivities as high as 74.2 kS/m and 33.5 W/m-K.

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Hoque, A. K. M. Azizul. "Synthesis of catalyst particles for carbon fiber growth in a Vapor Grown Carbon Fiber reactor." Ohio University / OhioLINK, 1997. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1174617623.

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Fedorenko, O. O., and J. K. Warchoł. "Structural and mass transfer characteristics of carbon-fiber materials." Thesis, Київський національний університет технологій та дизайну, 2017. https://er.knutd.edu.ua/handle/123456789/6750.

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Hengstermann, M., N. Raithel, A. Abdkader, M. M. B. Hasan, and Ch Cherif. "Development of new hybrid yarn construction from recycled carbon fibers for high performance composites: Part-I: basic processing of hybrid carbon fiber/polyamide 6 yarn spinning from virgin carbon fiber staple fibers." Sage, 2016. https://tud.qucosa.de/id/qucosa%3A35421.

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The availability of a considerable amount of waste carbon fiber (CF) and the increased pressure to recycle/reuse materials at the end of their life cycle have put the utilization of recycled CF (rCF) under the spotlight. This article reports the successful manufacturing of hybrid yarns consisting of staple CF cut from virgin CF filament yarn and polyamide 6 fibers of defined lengths (40 and 60 mm). Carding and drawing are performed to prepare slivers with improved fiber orientation and mixing for the manufacturing of hybrid yarns. The slivers are then spun into hybrid yarns on a flyer machine. The investigations reveal the influence of fiber length and mixing ratio on the quality of the card web, slivers and on the strength of the hybrid yarns. The findings based on the results of this research work will help realize value-added products from rCF on an industrial scale in the near future.

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Tsang, Lina. "High modulus carbon fiber/titanium laminates." Thesis, Massachusetts Institute of Technology, 2006. http://hdl.handle.net/1721.1/34584.

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Thesis (M. Eng.)--Massachusetts Institute of Technology, Dept. of Civil and Environmental Engineering, 2006.
Includes bibliographical references (leaves 38-39).
Titanium has been used to meet ever-stricter standards for high-temperature performance, creep resistance, low weight and high strength. Having low density, a high melting point, and high tensile strength, it seems like the perfect material for numerous applications. For structural applications where flexural stiffness and strength play the most important role, titanium's high cost can be a restrictive factor. The cost-effectiveness of the material can be increased by using it together with other less expensive high strength and low weight materials in the form of composite laminates. In this investigation, laminates were fabricated using inorganic matrix/high modulus carbon fiber composites with titanium sheets. Laminates were tested in three-point bending to assess the performance of the upgrade. The results show that combining Geopolymer high modulus carbon composites with titanium sheets significantly increases the performance. Laminates provide a lower cost solution for given stiffness and weight requirements compared with other common structural materials, such as steel and aluminum.
by Lina Tsang.
M.Eng.

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Books on the topic "Carbon fiber"

1

Chung, Deborah D. L. Carbon fiber composites. Boston: Butterworth-Heinemann, 1994.

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Rehkopf, Jackie D. Automotive Carbon Fiber Composites. Warrendale, PA: SAE International, 2011. http://dx.doi.org/10.4271/t-124.

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Kelly, Vincent. Carbon fiber: Manufacture and applications. Kidlington, Oxford, UK: Elsevier, 2004.

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4

Carolyn, Maciag, and United States. National Aeronautics and Space Administration., eds. Improving the interlaminar shear strength of carbon fiber-epoxy composites through carbon fiber bromination. [Washington, DC: National Aeronautics and Space Administration, 1987.

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Carolyn, Maciag, and United States. National Aeronautics and Space Administration., eds. Improving the interlaminar shear strength of carbon fiber-epoxy composites through carbon fiber bromination. [Washington, DC: National Aeronautics and Space Administration, 1987.

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Delmonte, John. Technology of carbon and graphite fiber composites. Malabar, Fla: R.E. Krieger Pub. Co., 1987.

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Bo, Zhu, ed. Ju bing xi jing ji tan xian wei. Beijing: Ke xue chu ban she, 2011.

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I, Harper Sheila, Bascom Willard D, and Langley Research Center, eds. Effects of fiber, matrix, and interphase on carbon fiber compression strength. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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Veit, Görner, Lower Saxony (Germany). Ministerium für Wissenschaft und Kultur, and CFK-Forschungszentrum Nord, eds. Carbon art. Drochtersen: MCE Verlagsgesellschaft, 2011.

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Chilton, J. E. Hybrid fiber-optic-electrochemical carbon monoxide monitor. Washington, D.C: U.S. Dept. of the Interior, Bureau of Mines, 1992.

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Book chapters on the topic "Carbon fiber"

1

Gooch, Jan W. "Carbon Fiber." In Encyclopedic Dictionary of Polymers, 116. New York, NY: Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-6247-8_1929.

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Endo, Makoto. "Carbon Fiber." In High-Performance and Specialty Fibers, 327–42. Tokyo: Springer Japan, 2016. http://dx.doi.org/10.1007/978-4-431-55203-1_20.

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Fitzer, E., and Lalit M. Manocha. "Carbon Fiber Architecture." In Carbon Reinforcements and Carbon/Carbon Composites, 82–96. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-58745-0_3.

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Herakovich, Carl T. "Boron Fiber to Carbon Fiber." In The Structural Integrity of Carbon Fiber Composites, 59–70. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-46120-5_3.

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Hoyer, Daniel, Eric P. Zorrilla, Pietro Cottone, Sarah Parylak, Micaela Morelli, Nicola Simola, Nicola Simola, et al. "Carbon-Fiber Amperometry." In Encyclopedia of Psychopharmacology, 275. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-540-68706-1_621.

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Chawla, Krishan K. "Carbon Fiber Composites." In Composite Materials, 252–77. New York, NY: Springer New York, 1998. http://dx.doi.org/10.1007/978-1-4757-2966-5_8.

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Potje-Kamloth, Karin, Petr Janata, and Mira Josowicz. "Carbon Fiber Microelectrodes." In Contemporary Electroanalytical Chemistry, 199–203. Boston, MA: Springer US, 1990. http://dx.doi.org/10.1007/978-1-4899-3704-9_20.

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Chawla, Krishan Kumar. "Carbon Fiber Composites." In Composite Materials, 150–63. New York, NY: Springer New York, 1987. http://dx.doi.org/10.1007/978-1-4757-3912-1_8.

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Bertagnoli, R. "Interbody Carbon Fiber." In Advances in Spinal Stabilization, 176–87. Basel: KARGER, 2003. http://dx.doi.org/10.1159/000072641.

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Perumal, Anand Babu, Reshma B. Nambiar, Periyar Selvam Sellamuthu, and Emmanuel Rotimi Sadiku. "Carbon Fiber Composites." In Handbook of Nanomaterials and Nanocomposites for Energy and Environmental Applications, 85–115. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-36268-3_174.

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Conference papers on the topic "Carbon fiber"

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Liberati, Andre C., Payank Patel, Amit Roy, Phuong Vo, Chunzhou Pan, Christian Moreau, Richard R. Chromik, Stephen Yue, and Pantcho Stoyanov. "Effect of Carbon Fiber Orientation when Cold Spraying Metallic Powders onto Carbon Fiber Reinforced Polymers." In ITSC 2023. ASM International, 2023. http://dx.doi.org/10.31399/asm.cp.itsc2023p0280.

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Abstract A previous study on the pull-off testing of metallized carbon fiber reinforced polymers (CFRPs) via cold spray showed that better adhesion strengths could be obtained when features such as carbon fibers or surfacing elements were present, by providing potential mechanical interlocking features. In this work, the effect of the fiber orientation on the deposition and bonding of the metallic coating to the thermoplastic composite substrate is explored. Pure Sn powder was cold sprayed onto two thermoplastic Polyether-Ether- Ketone (PEEK) CFRP substrates, containing carbon fibers with different orientations: one had fibers in the plane of the substrate (uni-directional tape), while the other had fibers mostly perpendicular to the substrate (ZRT film). Characterization of the coatings was performed via scanning electron microscopy (SEM) and confocal microscopy, and some aspects of mechanical testing (namely wear and scratch testing) were carried out to assess the effect of the substrate on the properties of the coatings.

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2

Tehrani, Mehran, Masoud Safdari, Scott W. Case, and Marwan S. Al-Haik. "Using Multiscale Carbon Fiber/Carbon Nanotubes Composites for Damping Applications." In ASME 2011 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. ASMEDC, 2011. http://dx.doi.org/10.1115/smasis2011-5087.

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A novel technique to grow carbon nanotubes (CNTs) on the surface of carbon fibers in a controlled fashion using simple lab set up is developed. Growing CNTs on the surface of carbon fibers will eliminate the problem of dispersion of CNTs in polymeric matrices. The employed synthesis technique retains the attractive feature of uniform distribution of the grown CNTs, low temperature of CNTs’ formation, i.e. 550 °C, via cheap and safe synthesis setup and catalysts. A protective thermal shield of thin ceramic layer and subsequently nickel catalytic particles are deposited on the surface of the carbon fiber yarns using magnetron sputtering. A simple tube furnace setup utilizing nitrogen, hydrogen and ethylene (C2H4) were used to grow CNTs on the carbon fiber yarns. Scanning electron microscopy revealed a uniform areal growth over the carbon fibers where the catalytic particles had been sputtered. The structure of the grown multiwall carbon nanotubes was characterized with the aid of transmission electron microscopy (TEM). Dynamical mechanical analysis (DMA) was employed to measure the loss and storage moduli of the hybrid composite together with the reference raw carbon fiber composite and the composite for which only ceramic and nickel substrates had been deposited on. The DMA tests were conducted over a frequency range of 1–40 Hz. Although the storage modulus remained almost unchanged over the frequency range for all samples, the loss modulus showed a frequency dependent behavior. The hybrid composite obtained the highest loss modulus among other samples with an average increase of approximately 25% and 55% compared to composites of the raw and ceramic/nickel coated carbon fibers, respectively. This improvement occurred while the average storage modulus of the hybrid composite declined by almost 9% and 15% compared to the composites of reference and ceramic/nickel coated samples, respectively. The ultimate strength and elastic moduli of the samples were measured using standard ASTM tensile test. Results of this study show that while the addition of the ceramic layer protects the fibers from mechanical degradation it abolishes the mechanisms by which the composite dissipates energy. On the other hand, with almost no compromise in weight, the hybrid composites are good potential candidate for damping applications. Furthermore, the addition of CNTs could contribute to improving other mechanical, electrical and thermal properties of the hybrid composite.

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3

N. Sarvestani, Ali, Nekoda van de Werken, Pouria Khanbolouki, and Mehran Tehrani. "3D Printed Composites With Continuous Carbon Fiber Reinforcements." In ASME 2017 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/imece2017-72041.

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Additively manufactured polymers can be reinforced with high-performance reinforcements such as carbon fibers. Printed thermoplastics with embedded continuous carbon fibers are up to two orders of magnitude stronger and stiffer than high-grade 3D printed polymers. In this work, the mechanical response of such 3D printed carbon fiber specimens is evaluated. While the precursor carbon fiber reinforced filaments achieve a stiffness of 50GPa and strength 700MPa, mechanical properties of their printed parts are highly affected by printed carbon fiber curvatures. In this work, the structure of 3D printed parts was examined, and some design rules for 3D printing with continuous carbon fibers are suggested. Moreover, failure mechanisms in these samples are discussed and correlated to the micro-structure of the composites and the carbon fiber configuration.

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4

Zhou, Uuanxin, Ying Wang, Yuanming Xia, and Shaik Jeelani. "Dynamic Tensile Properties of Carbon Fiber and Carbon Fiber Reinforced Aluminum." In ASME 2006 International Mechanical Engineering Congress and Exposition. ASMEDC, 2006. http://dx.doi.org/10.1115/imece2006-15732.

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In this study, dynamic and quasi-static tensile behaviors of carbon fiber and unidirectional carbon fiber reinforced aluminum composite have been investigated. The complete stress-strain curves of fiber bundles and the composite at different strain rate were obtained. The experimental results show that carbon fiber is a strain rate insensitive material, but the tensile strength and critical strain of the Cf/Al composite increased with increasing of strain rate because the strain rate strengthening effect of aluminum matrix. Based on experimental results, a fiber bundles model has been combined with Weibull strength distribution function to establish a one-dimensional damage constitutive equation for the Cf/Al composite.

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5

Xin, Zhuoyang, Guanqi Zhu, Eryu Ni, Chongyi Tang, and Dan Luo. "Adaptive Robotic Fiber Winding System for Multiple Types of Optimized Structural Components." In CAADRIA 2022: Post-Carbon. CAADRIA, 2022. http://dx.doi.org/10.52842/conf.caadria.2022.2.161.

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6

Tomikawa, Yoshiro, Kazuhiro Kimura, and Sumio Sugawara. "Ultrasonic carbon-fiber gyrosensor." In 3rd International Conference on Intelligent Materials, edited by Pierre F. Gobin and Jacques Tatibouet. SPIE, 1996. http://dx.doi.org/10.1117/12.237128.

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Porter, A., C. Ni, K. Deng, K. Fu, and C. Zhang. "Additive Manufacturing of Three-Dimensional Carbon Fiber Scaffold from Recycled Carbon Fibers." In SAMPE 2022. NA SAMPE, 2022. http://dx.doi.org/10.33599/nasampe/s.22.0827.

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8

Yamashita, Shinji. "Carbon-nanotube and Graphene Photonics." In Optical Fiber Communication Conference. Washington, D.C.: OSA, 2011. http://dx.doi.org/10.1364/ofc.2011.othl1.

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9

Mitsuguchi, S., M. Hiramatsu, H. Kondo, M. Hori, and H. Kano. "Fabrication of Carbon Nanowalls on Carbon Fiber Paper." In 2011 International Conference on Solid State Devices and Materials. The Japan Society of Applied Physics, 2011. http://dx.doi.org/10.7567/ssdm.2011.k-1-2.

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Kawada, H., S. Sato, and M. Kameya. "Modification of the Interface in Carbon Nanotube-Grafted T-Glass Fiber." In ASME 2012 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/imece2012-89318.

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In recent years, carbon nanotubes (CNTs) have attracted a lot of interest as an additional component in fiber reinforced plastics (FRP) to improve the properties of the fiber/matrix interface. An improvement of the apparent interfacial shear strength (ISS) was achieved by grafting CNTs onto reinforcement fibers instead of dispersing CNTs in the matrix. In one study, composites containing CNT-grafted fibers and epoxy resin demonstrated 26% ISS improvement over the baseline composites. However, few studies are focused on glass fibers, due to their low heat resistance. In this study, the effects of grafting CNTs onto T-glass fibers were evaluated by investigating the mechanical and interfacial properties of the CNT-grafted fiber/epoxy resin model composites. Elastic shear-lag analysis was also used to investigate the effect of CNTs on ISS. We used the chemical vapor deposition (CVD) method to graft CNTs onto T-glass fibers. As a result, CNTs were grafted relatively uniformly and cylindrically onto the fibers, which indicates that the CNT-grafting process was appropriate. The CNT-grafted fiber/epoxy resin model composites showed a significant (46∼67%) increase of interfacial shear strength. The formation of an interfacial region containing CNTs was observed around each fiber. Elastic shear-lag analysis showed a 20% increase of ISS. Those results imply that the elastic modulus of the interfacial region around the fibers was higher than that of epoxy resin.

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Reports on the topic "Carbon fiber"

1

Milbrandt, Anelia, and Samuel Booth. Carbon Fiber from Biomass. Office of Scientific and Technical Information (OSTI), September 2016. http://dx.doi.org/10.2172/1326730.

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2

Burchell, T. D., J. W. Klett, and C. E. Weaver. A novel carbon fiber based porous carbon monolith. Office of Scientific and Technical Information (OSTI), June 1995. http://dx.doi.org/10.2172/115403.

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Rellick, G. S., R. J. Zaldivar, and P. M. Adams. Fiber-Matrix Interphase Development in Carbon/Carbon Composites. Fort Belvoir, VA: Defense Technical Information Center, January 1998. http://dx.doi.org/10.21236/ada341620.

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4

Burchell, T. D., M. R. Rogers, and A. M. Williams. Carbon fiber composite molecular sieves. Office of Scientific and Technical Information (OSTI), June 1996. http://dx.doi.org/10.2172/450756.

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5

Abhiraman, Agaram S. Precursor Structure - Fiber Property Relationships in Polyacrylonitrile- Based Carbon Fibers. Fort Belvoir, VA: Defense Technical Information Center, April 1992. http://dx.doi.org/10.21236/ada249888.

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6

Shewey, Megan, Patti Tibbenham, and Dan Houston. Carbon Fiber Reinforced Polyolefin Body Panels. Office of Scientific and Technical Information (OSTI), October 2019. http://dx.doi.org/10.2172/1600931.

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Wilkerson, Justin, Daniel Ayewah, and Daniel Davis. Fatigue Characterization of Functionalized Carbon Nanotube Reinforced Carbon Fiber Composites. Fort Belvoir, VA: Defense Technical Information Center, January 2007. http://dx.doi.org/10.21236/ada515475.

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Norris, Jr, Robert E., Jeff A. McCay, and Connie D. Jackson. Comparison of ORNL Low Cost Carbon Fiber with Commercially Available Industrial Grade Carbon Fiber in Pultrusion Samples. Office of Scientific and Technical Information (OSTI), February 2016. http://dx.doi.org/10.2172/1246777.

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Norris, Jr., Robert E., and Hendrik Mainka. Carbon Fiber Composite Materials for Automotive Applications. Office of Scientific and Technical Information (OSTI), June 2017. http://dx.doi.org/10.2172/1394272.

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10

Kay, G. Simulations of carbon fiber composite delamination tests. Office of Scientific and Technical Information (OSTI), October 2007. http://dx.doi.org/10.2172/923091.

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