Acrylic (PAN) as Carbon Fibre Precursor
topic
PAN-based acrylic precursor fibre is the dominant raw material for carbon fibre manufacturing, accounting for 95% of global carbon fibre production — with precursor quality (molecular weight, co-monomer composition, void content, defect density, filament diameter uniformity) being the single most important determinant of carbon fibre mechanical performance and manufacturing yield. Precursor requirements: high molecular weight PAN homopolymer or copolymer (Mn 100,000–200,000 g/mol, narrow MWD PDI <2.5 — low PDI reduces oxidation stage non-uniformity), co-monomer content 1–3% itaconic acid (IA) or methacrylic acid (MAA) — carboxylic acid co-monomers catalyse cyclisation reaction, reduce stabilisation temperature by 20–30°C and stabilisation time by 30–40%; filament diameter 5–7 µm (aerospace grade) or 7–12 µm (industrial grade); void content <0.1% volume (voids become defects in final carbon fibre, reducing tensile strength by 5–15% per 0.1% void); surface irregularity <5 nm Ra. Precursor production differentiation: aerospace carbon fibre precursor (Toray T800, T1000 grade) — solution wet-spun from DMSO or DMF, 5–6 µm diameter, defect-free, $8–15/kg precursor cost → $25–45/kg carbon fibre; industrial carbon fibre precursor (Toray T300 equivalent) — 7–12 µm, lower quality control, $4–6/kg precursor → $15–25/kg CF. Carbon fibre conversion process: precursor → stabilisation (oxidative, 200–280°C, air atmosphere, 60–90 minutes — PAN ladder polymer formation by cyclisation, dehydrogenation → black oxidised fibre density 1.35–1.40 g/cm³) → low-temperature carbonisation (LTC, 300–800°C, nitrogen, 3–5 minutes — evolution of N₂, HCN, CO, CO₂, non-carbon elements) → high-temperature carbonisation (HTC, 1,000–1,600°C, nitrogen, 1–3 minutes — graphitic carbon layer development, carbon content >93%) → surface treatment (anodic oxidation, 0.3–1.0 A/dm², increases -COOH, -OH functional groups for matrix adhesion) → sizing (epoxy emulsion 0.5–1.5% OWF, protects during handling) → final carbon fibre. CF properties versus precursor: T800 CF tensile strength 5,880 MPa, modulus 294 GPa, strain to failure 2.0%, density 1.80 g/cm³ — conversion efficiency 50% (1 kg PAN precursor → 0.5 kg carbon fibre by mass loss of non-carbon elements). Global carbon fibre market: 190,000 tonnes (2023, Lucintel), $4.5 billion market value — Toray 37% share, Teijin Toho 14%, SGL Carbon 9%, Hexcel 10%; aerospace 25%, wind energy 28%, automotive 15%, sports/leisure 12%.
Role
PAN precursor understanding is fundamental to carbon fibre science — precursor quality parameters (molecular weight, co-monomer type, void content, filament diameter) set upper limits on achievable carbon fibre mechanical performance that no subsequent processing optimisation can overcome, making precursor development the most technically critical investment in the $4.5 billion carbon fibre industry where aerospace-grade fibre commanding $25–45/kg depends entirely on $8–15/kg precursor quality that requires 15+ years of PAN polymer and spinning process optimisation to master.