Carbon fibre
Filaments of near-pure carbon with extraordinary stiffness-to-weight, used in composites rather than alone.
Carbon fibre is drawn from a polymer precursor, usually polyacrylonitrile, which is oxidised and then carbonised until little but carbon remains, arranged in sheets aligned along the fibre.
Its headline strength figures are real but directional, and that qualification is essential rather than pedantic. Fibres are enormously strong along their length and weak across it. A carbon fibre component's real properties are set by how the fibres are laid up, which is why it is a design material rather than a drop-in substitute for metal.
Processing
Carbon fibre is made by controlled decomposition rather than by melting or drawing. A polymer precursor — usually polyacrylonitrile — is spun into filaments, then stretched and oxidised in air at a few hundred degrees so the chains cross-link and will not melt.
The oxidised fibre is then carbonised in an inert atmosphere at temperatures above a thousand degrees, driving off nitrogen and hydrogen until almost only carbon remains, arranged in sheets aligned along the fibre axis. Higher temperatures give stiffer, less strong fibre; lower ones the reverse. The surface is finally treated and sized so that resin will bond to it, without which the composite fails at the interface.
Uses
Aerospace was the first market and remains the most demanding: large parts of modern airliner structures are carbon composite, chosen because weight saved is fuel saved over decades of service.
Wind turbine blades are now a large consumer, since blade length is limited by what the material can hold up under its own weight. Automotive use is concentrated in performance and electric vehicles, sporting goods take a visible share, and pressure vessels for compressed hydrogen and natural gas depend on carbon fibre overwrap. Cost and the difficulty of recycling the cured composite are the two limits on wider adoption.
How we know: checked recently · only one source, so there is nothing to cross-check it against · stated directly by the source.
How this connects
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is composed of
- Carbon — element · 92–100% · carbonised from a polymer precursor until little but carbon remains
is an alternative to
- Aluminium — element · in aerospace structure: better stiffness for its weight than any metal, against cost, a failure that is sudden rather than gradual, and damage that can be invisible from outside
- Aramid fibre — material · aramid is tougher and better in tension and impact, carbon fibre is stiffer and far better in compression. Hybrid laminates use both, which is the usual answer
- Invar — alloy · as mould tooling that must not change size relative to the composite curing on it — Invar is heavy and predictable, carbon tooling is light and matches the part exactly
is used as
- Structural engineering — application · where stiffness per unit mass justifies the cost — aircraft structure, pressure vessels, and the reinforcement of existing concrete
- Textiles — application · as the fibre in a composite rather than as fabric in its own right, though it is woven first
is used in
- Aerospace manufacture — industry · primary structure since the 1990s — a modern wide-body wing and fuselage are more composite than metal
- Wind turbine blade — object · in the spar caps of the longest blades, where stiffness stops the tip striking the tower
is a component of
- Carbon fibre composite — material · and quoting the filament's strength for the laminate overstates it by a factor of several, which is the commonest error made about the material
is produced by
- Pyrolysis — process · polyacrylonitrile filament, first oxidised in air at 200 to 300 °C so it will not melt, then carbonised above 1,000 °C — and the final temperature sets the stiffness, because it sets how ordered the carbon is
Sources
- Material WorldOur own writing