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Carbon fibers

Carbon fibers are thin, strong filaments primarily composed of carbon atoms, with diameters typically ranging from 5 to 10 micrometers and containing more than 90 wt% carbon, making them a high-performance material renowned for their exceptional strength-to-weight ratio and use as reinforcement in advanced composites. These fibers exhibit tensile strengths often exceeding 3.5 GPa and moduli up to 500 GPa or more, depending on the grade, while maintaining a low of approximately 1.7 to 2.0 g/cm³, which is about one-fourth that of , enabling significant weight savings in structural applications. Produced mainly through the of (PAN) precursors, which dominate over 90% of global , carbon fibers undergo stabilization, at around 1,000°C, and optional graphitization up to 3,000°C to achieve their graphitic structure and tailored properties. The material's key attributes include high chemical and thermal stability in non-oxidizing environments, excellent electrical and thermal conductivity (up to 500 W/mK for high-modulus variants), and a negative coefficient of linear thermal expansion, rendering it ideal for demanding conditions. Carbon fibers are categorized by modulus—standard, intermediate (high-strength), and high-modulus—and available in forms like continuous tows (1K to 320K filaments) or chopped strands, with global production capacity reaching 290,000 tons in 2023 and demand projected to grow 144% by 2030 due to expanding uses. In composites like carbon fiber-reinforced polymers (CFRPs), they provide specific strengths around 1300 MPa/(g/cm³)—over 15 times that of steel—and specific moduli of 131 GPa/(g/cm³), about five times steel's, while offering superior fatigue resistance (70–80% of tensile strength) and energy absorption. Applications of carbon fibers span , where they constitute over 50 wt% of structures in like the Boeing 787 and for fuselages and wings; automotive lightweighting, as in body panels and NIO ES6 chassis to reduce vehicle mass and emissions; blades for ; and sporting goods, pressure vessels, and construction for enhanced durability and efficiency. Their integration via processes like or resin transfer molding has driven a of 12.5% over the past two decades, underscoring their role in sustainable, high-performance engineering.

History

Early Discovery

The early discovery of carbon fibers dates back to 1879, when experimented with carbonized cellulose threads derived from or as filaments for incandescent light bulbs, achieving a viable electrically heated solution that lasted over 13 hours. These fibers, formed by baking materials at high temperatures to carbonize them, represented an initial recognition of carbon's potential for high-temperature resistance, though Edison's focus remained on rather than broader applications, and the technology was not scaled for fiber production. Post-World War II, renewed interest in advanced materials for prompted systematic research in the at the Royal Aircraft Establishment (RAE) during the , where scientists sought high-temperature resistant fibers suitable for aircraft components. By the early , the team at the RAE, led by William Watt and colleagues, developed processes using (PAN) as a precursor that aligned carbon atoms into oriented structures for improved strength and stability under extreme heat. In parallel, early U.S. efforts in the late at Union Carbide's Parma Technical Center, led by chemist , produced high-performance whiskers through the of gases, such as heated to approximately 2,000°C in a , yielding structures with tensile strengths up to 20 GPa. These whiskers demonstrated the potential for exceptionally strong carbon-based materials, though initial outputs were limited to small quantities and extremely high costs. Throughout these pioneering experiments, researchers encountered significant challenges, including the inherent of the fibers due to uneven and low yields—often below 20%—resulting from material degradation during processing. These issues were mitigated through refined techniques, such as staged up to 3,000°C in vacuum or environments, which reduced defects and improved molecular orientation without fracturing the structure. Such innovations paved the way for the commercial scalability of carbon fibers in the 1960s.

Commercial Development

The commercial development of carbon fibers accelerated in the , building on early experimental discoveries such as Roger Bacon's 1958 production of high-performance whiskers at . In late 1965, achieved a key breakthrough with the development of high-modulus fibers through optimized hot-stretching and carbonization processes applied to precursors, resulting in the commercial launch of Thornel 25 yarn with a of 172 GPa. This advancement marked the shift from laboratory-scale production to viable industrial methods, initially targeting high-value applications. The first widespread commercial production emerged in the late 1960s, driven by sector demands during the and military programs requiring lightweight, high-strength materials. Companies like initiated commercial-scale manufacturing of rayon-based carbon fibers around 1965, supplying early applications in and missiles. Concurrently, in began test production of (PAN)-based carbon fibers in 1971 under the Torayca brand, scaling to full commercial output by 1973 at a rate of 5 tons per month. These efforts were propelled by the need for materials in space exploration and defense, where carbon fibers offered superior performance over metals. Significant patent developments facilitated this industrialization, notably Akio Shindo's 1959 patent for a -based process that achieved 50-60% carbon yield by oxidizing precursors in air rather than enclosed furnaces. Licensed to firms like Nippon Carbon in 1961 and Toray in 1970, Shindo's innovation enabled efficient production of high-strength fibers, with the U.S. equivalent issued in 1970. Although vapor-grown carbon fibers emerged later in the through separate catalytic processes, Shindo's work laid the groundwork for dominance in commercial markets. By the 1970s, production capacity expanded from lab-scale grams to industrial tons per year, supported by continuous processing techniques that boosted output for and emerging civilian uses. Initial costs, exceeding $400 per pound in the late 1960s due to batch methods, dropped below $100 per pound by the early 1970s through process optimizations and , eventually approaching $25 per pound for standard grades. This cost reduction, combined with rising demand from programs like the U.S. Department of Defense, propelled annual production growth at double-digit rates, establishing carbon fibers as a cornerstone of advanced composites.

Types

Precursor-Based Classification

Carbon fibers are primarily classified based on their precursor materials, which are the starting polymers or compounds converted into the final fibrous structure through processes like spinning, stabilization, and . The choice of precursor significantly influences the fiber's microstructure, mechanical properties, and suitability for applications, with , , and being the main types. Emerging bio-based precursors are also gaining attention for . PAN-based carbon fibers dominate the market, accounting for approximately 90% of production as of 2024 due to their versatility and cost-effectiveness. Derived from copolymers of with comonomers like or , PAN precursors are solution-spun into fibers that undergo oxidative stabilization to prevent melting during subsequent heating. This results in high-strength fibers with tensile strengths often exceeding 3 GPa, making them ideal for and automotive composites. Pitch-based carbon fibers, comprising about 9% of the , are produced from petroleum pitch, coal tar pitch, or synthetic pitches rich in aromatic hydrocarbons. These isotropic or mesophase pitches are melt-spun and yield fibers with a highly graphitic , providing exceptional with Young's moduli up to 900 GPa. Their ordered molecular alignment suits applications requiring high rigidity, such as structural reinforcements in high-temperature environments. Rayon-based carbon fibers, derived from regenerated (viscose ), were the first commercially produced type in the 1950s but now hold less than 1% market share. The precursor is spun into fibers and dehydrated during , leading to a turbostratic structure suitable for flame-resistant textiles and high-temperature . Their production is energy-intensive, limiting widespread use to specialty applications. Emerging precursors like , a renewable byproduct from wood pulping, offer sustainable alternatives to petroleum-based materials, potentially reducing costs by up to 50% and lowering carbon footprints. is processed via melt or solution spinning, though it typically yields around 40-50% carbon, comparable to PAN's approximately 50% yield, but with ongoing optimizations to improve efficiency. As of 2025, advancements in lignin-based fibers have achieved higher , with some blends reaching tensile approaching 200 GPa, and pilot productions demonstrating feasibility for automotive applications. Bio-based options, including alginate- blends, are under development to enhance environmental viability while maintaining integrity. These precursors result in and strength variations that align with specific performance categories.

Performance-Based Classification

Carbon fibers are classified based on their performance characteristics, primarily tensile strength and of elasticity, which determine their suitability for specific applications. This performance-based emphasizes end-product mechanical and functional properties rather than precursor materials, though precursors like () and influence these traits. High-strength fibers prioritize tensile strength for load-bearing roles, while high- variants focus on ; intermediate types offer a balance, and specialty forms like vapor-grown carbon nanofibers (VGCNF) provide unique nanoscale properties for advanced functionalities. High-strength carbon fibers exhibit tensile strengths exceeding 3.5 GPa, often reaching 4-7 GPa, making them ideal for applications requiring high load capacity and impact resistance, such as sporting goods like rackets and frames. These fibers, typically derived from precursors, achieve their performance through optimized processes that enhance fiber integrity without excessive . For instance, commercial grades like Toray's T700S offer a tensile strength of 4.9 GPa alongside a standard of around 230 GPa, enabling lightweight composites in recreational and industrial uses. High-modulus carbon fibers, with values greater than 300 GPa and up to 500 GPa or more, are designed for applications demanding superior stiffness and dimensional stability, such as structural stiffeners and pressure vessels. Predominantly produced from mesophase precursors, these fibers undergo high-temperature graphitization to align layers, resulting in exceptional rigidity but moderate tensile strengths around 2-4 GPa. Examples include pitch-based fibers with moduli of 588 GPa, which provide thermal stability and are used in components where is critical. Intermediate modulus/strength carbon fibers bridge the gap between high-strength and high-modulus types, featuring moduli of 240-300 GPa and tensile strengths of 3-5 GPa, which performance and cost for broader industrial adoption. These hybrids, often PAN-based, are particularly suited for automotive applications like components and body panels, where weight reduction and moderate improve without the premium expense of ultra-high-modulus variants. Commercial offerings, such as those with 290 GPa and strengths over 4.8 GPa, support high-volume manufacturing in electric vehicles and recreational vehicles. Specialty carbon fibers, such as vapor-grown carbon nanofibers (VGCNF), deviate from traditional microscale fibers with diameters under 100 and high ratios exceeding 100, emphasizing electrical and over bulk strength. These nanofibers, synthesized via catalytic vapor deposition, exhibit resistivities as low as 5 × 10^{-7} · and conductivities up to 910 /m· in composites, making them valuable for , electromagnetic interference shielding, and battery anodes in systems. Unlike conventional fibers, VGCNF's nanoscale structure enables unique functionalities like enhanced gas and in matrices at low loadings (e.g., 1.5 vol% for ).
CategoryKey Metrics (Tensile Strength / Modulus)Primary ApplicationsTypical Precursor Influence
High-Strength>3.5 GPa / 200-250 GPaSporting goods, industrial composites for strength optimization
High-Modulus2-4 GPa / >300 GPa stiffeners, pressure vessels for alignment
Intermediate Hybrids3-5 GPa / 240-300 GPaAutomotive components, vehicles for cost-performance balance
Specialty (VGCNF)2.5-3.5 GPa / 100-1200 GPa, Vapor deposition for nanoscale conductivity

Structure

Atomic and Molecular Arrangement

Carbon fibers consist primarily of carbon atoms that are predominantly sp² hybridized, forming planar graphene-like sheets composed of hexagonal rings of carbon atoms bonded covalently within each layer. These sheets are held together by weak van der Waals forces between layers, resulting in a layered structure analogous to but with varying degrees of order depending on the precursor and processing conditions. The atomic arrangement in carbon fibers can adopt turbostratic or graphitic configurations. In the turbostratic structure, common in -based fibers, the sheets are stacked irregularly, with adjacent layers rotated relative to each other by angles up to 20–30°, leading to a disordered three-dimensional network. In contrast, the graphitic arrangement, more prevalent in mesophase pitch-based fibers, features well-aligned sheets with coherent hexagonal lattices parallel to the fiber axis, approaching the ideal structure of single-crystal . The extent of graphitization is characterized by the sizes of graphitic crystallites, denoted as L_a (in-plane lateral dimension) and L_c (stacking height along the c-axis), which are measured using X-ray diffraction based on the broadening of diffraction peaks according to the . In typical PAN-based carbon fibers carbonized at around 2500°C, L_a ranges from 6 to 12 nm and L_c corresponds to at least 12 layer planes (approximately 4 nm). However, in highly oriented pitch-based fibers subjected to high-temperature graphitization, these crystallites grow significantly larger, with L_a and L_c often exceeding 50 nm, enhancing the overall structural coherence. Defects such as atomic vacancies, dislocations, and residual heteroatoms (e.g., and oxygen originating from the precursor) interrupt the perfect alignment of sheets, influencing the local order and overall perfection. These imperfections are more pronounced in lower-temperature processed fibers and diminish with increasing graphitization temperature. The interlayer spacing, denoted as d_{002}, provides a key metric for structural quality, typically ranging from 0.344 in turbostratic regions to 0.335–0.340 in graphitic domains, as determined by the position of the (002) peak via .

Microscopic Morphology

Carbon fibers typically exhibit diameters in the range of 5 to 10 μm for standard industrial variants, while specialized microfibers can achieve diameters as small as 1 μm. These dimensions influence the observable architecture at the microscopic scale, where cross-sectional textures vary significantly based on the precursor material. -based carbon fibers often display an onion-like radial texture, characterized by concentrically arranged graphene-like layers radiating from the center to the surface, sometimes accompanied by a distinct skin-core structure where the outer layer differs in orientation from the inner core. In contrast, mesophase pitch-based fibers tend to exhibit more uniform microstructures across their cross-section, with less pronounced radial or skin-core gradients, though variations such as random or quasi-onion orientations can occur depending on processing conditions. At the micron scale, imperfections such as voids and micropores are commonly present within the fiber matrix, arising from gas or incomplete during , which contribute to a typical range of 1.7 to 2.0 g/cm³—lower than ideal due to these structural heterogeneities. , often manifesting as longitudinal striations or fibrillar with nanoscale amplitudes (around 5-20 nm), further affects the overall and can stem from precursor spinning or processes. These voids, micropores, and surface features collectively impact the fiber's and , with the atomic-scale arrangement of turbostratic carbon layers forming the basis for such observable defects. Scanning electron microscopy (SEM) is widely employed to visualize surface morphology, revealing details like roughness profiles and external defects, while (TEM) provides insights into internal lamellae orientation and cross-sectional textures at higher resolutions.

Properties

Mechanical Characteristics

Carbon fibers exhibit exceptional mechanical properties that make them ideal for high-performance applications, characterized by high strength-to-weight ratios and . Their tensile strength typically ranges from 3 to 7 GPa, which is influenced by factors such as defect and precursor material; lower defect concentrations in high-quality fibers can achieve values near the upper end of this range. The , a measure of , is defined by the equation E = \frac{\sigma}{\varepsilon}, where \sigma is the applied and \varepsilon is the resulting , with axial values for commercial carbon fibers spanning 200 to 600 GPa and reaching up to 800 GPa for ultra-high modulus variants derived from pitch precursors. Their is approximately 1.7 to 2.0 g/cm³. In compression, carbon fibers demonstrate lower performance compared to tension, with strengths generally in the 1 to 2 Pa range due to susceptibility to and kinking under load. This disparity arises from the fibers' anisotropic microstructure, where transverse are weaker, leading to failure modes like micro. The [G](/page/G), which governs resistance to deformation, can be approximated as [G](/page/G) \approx \frac{[E](/page/E!)}{2(1 + \nu)}, with Poisson's ratio \nu typically 0.2 to 0.3 for axial loading, reflecting the material's lateral contraction behavior under uniaxial . Carbon fibers possess high fatigue resistance, enduring millions of cycles under cyclic loading without significant degradation, provided initial defects are minimal; common failure modes include progressive fiber kinking and matrix cracking in composites. This durability stems from the absence of plastic deformation, unlike metals, allowing sustained performance in dynamic environments. Overall, the pronounced anisotropy of carbon fibers—manifested in axial tensile moduli up to 800 GPa versus much lower transverse values—necessitates careful orientation in design to optimize load-bearing capacity along the fiber axis. Thermal effects can modestly influence these properties by altering defect mobility at elevated temperatures, but mechanical characteristics remain dominant under standard conditions.

Thermal and Electrical Characteristics

Carbon fibers exhibit anisotropic thermal conductivity, with values typically ranging from 10 to 500 W/m·K or higher along the axial direction due to the aligned graphitic structure facilitating phonon transport, while transverse conductivity remains low, often around 1-5 W/m·K, primarily because of significant phonon scattering at the fiber's radial interfaces and imperfections. This behavior aligns with the kinetic theory of heat conduction for phonons, expressed as k = \frac{1}{3} C v l where k is the thermal conductivity, C is the volumetric heat capacity, v is the average phonon velocity, and l is the mean free path of phonons, which is much longer axially than transversely in carbon fibers. The electrical resistivity of carbon fibers generally falls in the range of $10^{-5} to $10^{-3} Ω·m longitudinally, reflecting their semiconducting to metallic-like behavior depending on the degree of graphitization. Higher graphitization temperatures enhance conductivity by promoting the formation of larger graphitic domains, where delocalized π electrons from sp²-hybridized carbon atoms enable efficient charge transport along the fiber axis. Carbon fibers display a near-zero axial coefficient of thermal expansion (CTE), typically between –2.0 × 10^{-6}/K and –0.5 × 10^{-6}/K, which provides excellent dimensional stability under temperature variations and is advantageous for applications requiring precise thermal management.

Manufacturing

Precursor Materials and Spinning

Carbon fibers are primarily produced from precursor materials that are spun into filament form prior to thermal conversion. The most common precursors include polyacrylonitrile (PAN), mesophase pitch, and rayon (cellulose-based), each offering distinct advantages in terms of availability, processing, and final fiber properties. These materials are selected for their ability to form stable, orientable fibers that can withstand subsequent high-temperature treatments. PAN, the dominant precursor accounting for over 90% of commercial carbon fiber production, is synthesized through copolymerization of with comonomers such as to enhance solubility in spinning solvents like or solutions. , typically incorporated at 1-2 mol%, improves the polymer's processability and promotes uniform cyclization during later stabilization, resulting in a with a molecular weight of around 100,000-200,000 g/mol. The PAN dope is then extruded into fibers using spinning, where filaments are coagulated in a liquid bath, or dry-jet spinning, which involves a short air gap before to reduce skin-core defects and achieve better molecular ; these methods produce filaments with diameters of 10-20 μm. Mesophase precursors, derived from or , are prepared by of isotropic at 350-400°C under inert conditions to form a nematic crystalline , enabling self-alignment of polyaromatic molecules for high graphitizability. This thermotropic mesophase, with 30-100% , is melt-spun directly through a into fibers, as the material exhibits flow at elevated temperatures without needing solvents. The aligned structure in the spun fibers contributes to the high of the resulting carbon fibers. Rayon precursors are regenerated fibers produced via the viscose process, where from wood pulp is dissolved in and to form a spinning , which is then extruded into an to precipitate filaments. Post-spinning, the fibers are impregnated with catalysts such as or to enhance oxidative stability and promote during , addressing the low yield inherent to due to its oxygen content. This impregnation step is crucial for preventing and maintaining integrity. Spinning parameters, particularly the draw ratio of 5-10x applied during and post-coagulation , significantly influence the initial molecular and radial uniformity of precursor fibers, setting the foundation for properties after . This drawing aligns chains, reducing diameter while increasing tensile strength of the precursor to 300-500 . Overall, the from precursor to carbon fiber anticipates approximately 50% mass loss due to volatile evolution, primarily during stabilization and .

Carbonization and Graphitization Processes

The carbonization and graphitization processes represent the core thermal conversion stages in carbon fiber production, transforming stabilized precursor fibers—primarily ()—into turbostratic carbon structures with high carbon content and aligned graphitic domains. These steps involve progressive under controlled conditions to eliminate heteroatoms and promote molecular reorganization, yielding fibers with densities of 1.8–2.1 g/cm³ and carbon contents exceeding 92%. Oxidative stabilization initiates the conversion by heating the precursor fibers at 200–300 °C in an air or oxygen atmosphere, inducing cross-linking reactions that convert the linear structure into a cyclic, infusible ladder . This prevents fiber fusion or melting during later heating and incorporates 8–10% oxygen for thermal stability, with the process typically lasting 1–2 hours under controlled heating rates of 1–5 °C/min to manage exothermic reactions and minimize defects. Low-temperature carbonization follows in an inert atmosphere, such as , at 1000–1500 °C, where volatile non-carbon elements (, oxygen, ) are driven off as gases, resulting in approximately 50% weight yield and formation of a disordered carbon matrix with 80–95% carbon content. Tension is applied throughout to counteract shrinkage, preserve fiber (typically 5–10 μm), and promote axial of the evolving . High-temperature graphitization, conducted at 2000–3000 °C in an like , refines the microstructure by enlarging and aligning graphitic crystallites, which enhances (up to 500–900 GPa for high-modulus variants) while slightly reducing tensile strength due to defect annealing. This step achieves >99% carbon purity and is highly energy-intensive, accounting for a substantial portion of the overall process energy demand of 50–80 kWh/kg. Industrial implementations often employ continuous vertical or horizontal furnaces for and graphitization to enable uniform tension control (e.g., 0.1–1 g/denier) and high throughput, contrasting with batch furnaces used for smaller-scale or experimental runs where precise isothermal holds are feasible.

Post-Processing Treatments

After the and graphitization stages, which yield the core carbon fiber structure, post-processing treatments are essential to refine surface properties, protect the fibers, and facilitate integration into composites or textiles. These steps address the inert and smooth nature of as-produced fibers, improving and processability without altering the bulk microstructure. is a critical post-processing step where a thin polymeric , typically 0.5-2 % of the fiber mass, is applied to the fiber surface. This , often formulated with epoxy-compatible resins or coupling agents, serves dual purposes: it protects the fibers from mechanical damage during handling and , and it enhances wettability and chemical bonding with matrices in composites. For instance, epoxy-based sizings promote covalent interactions at the -matrix , significantly boosting by up to 30% in carbon fiber-reinforced epoxies. Surface oxidation treatments further tailor the fiber surface for improved adhesion by introducing polar functional groups. Plasma etching, using oxygen or air plasmas, or chemical methods like nitric acid immersion, etch the graphitic surface to generate oxygen-containing groups such as -OH and -COOH. These treatments increase surface energy from around 30-40 mJ/m² to over 50 mJ/m², enabling stronger hydrogen bonding or chemical reactions with resin matrices. Plasma oxidation is particularly favored for its rapid, dry process that avoids excessive fiber degradation, achieving uniform functionalization across tow bundles. For applications in textiles, and cleaning processes remove agents and contaminants to restore fiber purity and flexibility. Solvents like acetone or are commonly used in or Soxhlet to dissolve polymeric residues, reducing surface oxygen functional groups and preventing stiffness in woven fabrics. This step is vital for textile-grade carbon fibers, as residual can impair dyeability or cause uneven , with chemical at ambient temperatures preserving tensile strength better than methods. Tow conversion involves bundling individual filaments into multifilament tows, typically ranging from 1K (1,000 filaments) to over 300K (300,000+ filaments), with larger tows used in high-volume applications to suit specific processing needs. Optional twisting or crimping is applied during this stage to enhance handling stability, reduce tow slippage in winding or , and form a more cohesive structure for applications. Twisting, in particular, imparts a rounder profile to the tow, improving resistance under while maintaining high directional strength.

Applications

Composite Reinforcement

Carbon fibers serve as a primary in composite matrices, particularly polymers, to produce high-strength, lightweight structures that outperform traditional metals in specific applications. By embedding continuous or discontinuous carbon fibers within a matrix, such as or , these composites achieve superior and tensile strength while minimizing weight, making them ideal for load-bearing components in demanding environments. The integration of carbon fibers into matrices like metals and ceramics is less common but emerging for hybrid systems requiring enhanced . In , (CFRP) are extensively used in fuselages and primary structures to reduce overall weight and improve . For instance, the incorporates CFRP comprising 50% of the by weight, which contributes to a 20% reduction in fuel consumption compared to similar-sized conventional . This design leverages the high of carbon fibers to enable larger, more aerodynamically efficient without compromising structural integrity. In the automotive sector, CFRP reinforces and body panels to lower vehicle mass and enhance , particularly in electric vehicles. The employs a CFRP passenger cell, known as the Life Module, which reduces the vehicle's weight by up to 30% relative to equivalents, thereby extending range and improving handling. volume fractions in such automotive CFRP components typically range from 40% to 60%, balancing reinforcement effectiveness with manufacturability. Carbon fiber composites are also widely used in pressure vessels, such as (CNG) and tanks for vehicles and industrial applications. These Type IV vessels, with carbon fiber overwrapped on a liner, offer high burst pressures over 700 while weighing 70-80% less than equivalents, enabling efficient storage for vehicles and portable systems. In , carbon fibers reinforce and other materials to enhance structural integrity in bridges, buildings, and seismic . Carbon fiber reinforced (CFRP) sheets or bars provide tensile strength to replace or supplement , reducing corrosion risks and allowing for slender designs, as seen in projects like the strengthening of historic structures. For infrastructure, carbon fibers reinforce blades, enabling longer spans and higher energy capture. Blades exceeding 100 meters in length, such as those up to 143 meters, often employ designs combining carbon fibers in high-stress regions with fibers elsewhere to optimize while maintaining cost-effectiveness. This approach reduces blade mass by approximately 20-30% compared to all-glass configurations, allowing turbines to operate in stronger winds with minimal material escalation. Key processing methods for these CFRP composites include autoclave molding, where pre-impregnated fiber layups are cured under vacuum and elevated pressure to minimize voids, and , which injects liquid resin into a dry fiber preform for net-shape parts. In both techniques, is meticulously controlled during —often using unidirectional tapes or woven fabrics aligned in 0°, 90°, and ±45° configurations—to tailor anisotropic properties for specific load paths. These methods exploit the inherent mechanical advantages of carbon fibers, such as their high tensile , to yield composites with exceptional strength-to-weight ratios.

Electrical and Thermal Uses

Carbon fibers' electrical , typically ranging from 10^2 to 10^5 S/m depending on graphitization degree, enables their use in applications requiring precise flow and dissipation. Their , often 10-100 W/m·K along the , further supports roles in thermal management without excessive weight. In , carbon microelectrodes are employed for neural recording due to their and minimal damage from small diameters (4-10 μm). These electrodes achieve low impedance, often below 1 MΩ at 1 kHz, attributed to the high effective surface area from their porous structure and coatings like PEDOT:PSS, which enhance charge transfer for stable signal detection. For instance, PEDOT:pTS-coated carbon fibers exhibit impedances around 118 kΩ at 1 kHz, enabling high-fidelity extracellular recordings . Flexible heating elements based on carbon fibers find applications in wearables for and in de-icing systems for or . In wearable garments, they operate at low voltages such as 5-12 , providing uniform heating through Joule effect while maintaining flexibility. For de-icing, carbon fiber tapes in panels function at 24 , delivering power densities around 0.13 /cm² to melt effectively on surfaces like aircraft wings. Advanced nano-carbon variants achieve up to 1.05 /cm² at higher voltages, supporting rapid response in compact designs. Carbon fibers serve as current collectors or electrodes in supercapacitors and batteries, leveraging their high and strength to reduce weight compared to metal foils. In the , hybrid carbon fiber electrodes, such as those combined with oxide or conducting polymers, have advanced performance, achieving specific capacitances of 200-300 F/g in flexible devices. For example, carbon fiber composites yield 203 F/g, enabling wearable with improved cycle stability. In lithium-ion batteries, carbon fiber interlayers lower and enhance rate capability. For electromagnetic interference (EMI) shielding in housings, carbon fiber composites provide effective through and mechanisms. Multi-layer continuous carbon fiber-reinforced polyamides achieve >60 shielding effectiveness in the 0.03-3 GHz range, with specific shielding up to 60 ·cm³/g, ideal for enclosures in devices. Epoxy-based carbon fiber laminates with 4 layers offer 60-90 , meeting commercial requirements for protecting sensitive circuits.

Textile and Protective Applications

Carbon fibers are integrated into textiles for applications requiring high strength, properties, and , particularly in , protective gear, and systems. These fibers, often in the form of woven or knitted fabrics, provide enhanced performance without sacrificing flexibility, making them suitable for dynamic uses where mechanical stress and environmental exposure are concerns. In and apparel, carbon fibers are blended with materials like or to create high-performance garments, such as cycling jerseys and athletic wear, where their superior strength-to-weight ratio allows for significant reductions in overall fabric weight compared to traditional synthetics. For instance, carbon fiber-infused fabrics can reduce garment weight by up to 30% while maintaining tensile strength, enabling athletes to achieve better mobility and endurance during activities like . This lightweighting is particularly beneficial in high-performance cycling gear, where the fibers' helps in reducing and fatigue. For protective clothing, carbon fibers are woven into flame-resistant suits for and industrial workers, forming a thermal barrier that withstands extreme temperatures exceeding 1000°C. These fabrics, such as those using oxidized or variants, provide against radiant heat, molten metal splashes, and direct flames up to 1300–6000°F, offering critical escape time during thermal hazards. In garments, carbon fiber layers enhance durability and chemical resistance, reducing skin exposure to carcinogens and heat stress in structural and wildland scenarios. Carbon fibers also serve as filtration media in air and water purification systems, leveraging their chemical inertness and high mechanical strength to capture contaminants effectively. fibers (ACF), in particular, exhibit superior adsorption for volatile compounds (VOCs) like and , with low pressure drops in pleated filter designs suitable for HVAC and indoor air systems. In , these fibers remove pollutants and pathogens, such as bacteriophages, outperforming granular due to their fibrous structure and high surface area. Weaving techniques for carbon fibers include braiding and to produce and fabrics, often with blends of carbon and other s for improved comfort and drapability. Braiding interlaced strands diagonally to form tubular or flat structures, while knitting creates interlocking loops that enhance flexibility and pore size variability in textiles. These methods, supported by post-processing treatments like surface to reduce , ensure compatibility for apparel and protective uses by minimizing fiber breakage during deformation.

Sustainability

Environmental Impacts of Production

The production of carbon fibers is highly energy-intensive, with total energy consumption ranging from 180 to 290 GJ per metric ton, predominantly attributed to the high-temperature graphitization stage where temperatures exceed 2000°C. This process accounts for the majority of the energy demand, as it involves controlled heating in inert atmospheres to align carbon structures, contributing significantly to the overall environmental footprint. Associated with this energy use are substantial , estimated at 13 to 34 kg CO₂ equivalent per kg of carbon fiber, largely from fossil fuel-based electricity and heat generation. The precursor stage, particularly the production of (), exacerbates emissions through the release of oxides () and () during ammoxidation processes. Additionally, consumption in precursor synthesis and fiber processing totals approximately 2400 m³ per metric ton, primarily for cooling and washing operations. Waste generation is another key impact, with approximately 50% mass loss occurring as volatile gases and byproducts during carbonization and graphitization, often resulting in landfill disposal or incineration that releases additional pollutants. In the 2020s, manufacturers like Toray have shifted toward renewable energy sources in production facilities, achieving a 36% reduction in greenhouse gas emissions per unit of revenue from the 2013 baseline as of 2023 through fuel switching and efficiency improvements. As of 2025, emerging innovations include bio-based carbon fibers from sustainable precursors like lignin and novel low-energy production methods that can reduce energy consumption by up to 50%. Recycling efforts serve as a potential mitigation strategy to offset these production impacts by recovering fibers from waste streams.

Recycling and Lifecycle Management

Recycling carbon fibers from end-of-life composites is crucial to mitigate the environmental burdens associated with their production, enabling a approach. Mechanical represents the simplest and most cost-effective method, involving the shredding of carbon fiber-reinforced (CFRP) composites into short fibers typically ranging from 50 µm to 10 mm in length. This process breaks down the material through crushing or milling, producing fibers that retain approximately 40-50% of their original tensile strength. Due to the reduced length and potential surface damage, these recycled fibers are primarily suited for non-structural applications, such as reinforcement in cement-based composites, where they enhance without compromising compressive properties. Chemical recycling via solvolysis offers a higher-quality , particularly using to dissolve the polymer matrix. In this , is heated above 374 °C and pressurized beyond 22.1 , achieving over 90% degradation of the and recovering clean carbon fibers with minimal defects. The recovered fibers maintain 90–98% of their virgin tensile strength, resembling virgin-like properties and enabling reuse in high-performance applications. For instance, treatments at 400 °C with additives like 0.5 M KOH for 15.5 minutes yield fibers suitable for structural composites. Pyrolytic thermal recycling decomposes the matrix through heating in an inert atmosphere at 500–1000 °C, yielding clean carbon fibers by volatilizing resins and organic components. This method produces fibers with intact surfaces but incurs about 20% loss in fiber length due to thermal stresses. While effective for bulk recovery, the process requires energy management to minimize further degradation, often resulting in fibers applicable to semi-structural roles. Lifecycle assessments highlight the environmental benefits of these recycling routes, demonstrating cradle-to-grave CO2 savings of up to 80% compared to virgin carbon , particularly for second-tier recycled fibers retaining 80% tensile strength via . In the , regulations under the Action Plan are driving targets, aiming to double the overall circularity rate to 24% by 2030 and promoting composite waste recovery to reduce dependence.

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