Carbon fibre composite
Carbon fibre in a resin — stiffer than steel for its weight, and nothing like as strong as the fibre's own number suggests.
A carbon fibre composite is carbon fibre held in a resin, usually epoxy, and its reason for existing is stiffness per unit mass. Along the fibres it is several times stiffer than steel for the same weight, which is the property aerospace and racing are actually buying.
The number that gets quoted is almost always the fibre's. A single carbon filament reaches several thousand megapascals along its axis; a laminate contains perhaps 60 per cent fibre by volume, oriented in several directions because a structure is loaded in several directions, and reaches a fraction of that. Quoting the filament figure for the part overstates it by a factor of several, and it is the commonest error made about this material.
Its weaknesses are specific. It is far weaker across the plies than along them, so a laminate delaminates rather than breaking. It is poor in compression relative to tension. It fails suddenly and without deforming first, which removes the warning an engineer relies on in metal. And impact damage can be invisible from the surface while the plies underneath have separated — which is why aerospace composite structure is inspected ultrasonically rather than by eye.
Processing
Pre-impregnated fabric cured under pressure in an autoclave gives the best and most consistent properties and is how aerospace structure is made. Resin transfer moulding and infusion are cheaper and are taking automotive volume. Filament winding for cylinders. Hand lay-up for one-offs and repairs.
The autoclave is the bottleneck: it is a large pressure vessel, cycles take hours, and out-of-autoclave systems have been an industry objective for twenty years.
It is joined by bonding and by bolting, and both are awkward. A drilled hole cuts the fibres that carry the load, so bolted joints need local reinforcement; bonded joints need surface preparation that is hard to verify.
Uses
Aircraft primary structure — the wings and fuselage of the Boeing 787 and Airbus A350 are more composite than metal, which is the change that took the material from secondary parts to the airframe itself. Rocket structures and pressure vessels. Racing car monocoques, where it is a safety structure as much as a light one. Wind turbine blade spar caps.
Bicycles, sporting goods, prosthetics and a great deal of consumer product where the woven surface is bought for what it signifies as much as for what it does.
History
The fibre dates from work at the Royal Aircraft Establishment in the 1960s. The composite moved from secondary structure — fairings, control surfaces — to primary structure over the 1980s and 1990s, and the argument each time was whether a material that fails without warning could be certified for a part whose failure brings the aircraft down. The answer was damage tolerance analysis and ultrasonic inspection rather than a change to the material.
Environmental impact
Energy intensive to make — the fibre alone takes several times the energy per kilogram of aluminium — and not recyclable as itself. Pyrolysis recovers shortened fibres suitable for moulding compounds rather than for structure, which is downcycling by any honest description.
The case for it is entirely in use. A kilogram removed from an airliner saves fuel for twenty-five years, and the arithmetic on that is comfortably favourable. The same argument does not transfer to a bicycle frame or a phone case, and it is routinely made there anyway.
Galvanic corrosion is a practical consequence worth knowing: carbon is electrically conductive and cathodic to aluminium, so the two in contact in a wet environment corrode the aluminium quickly. It is a real reason titanium and PEEK appear where aluminium otherwise would.
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
Where a connection has been confirmed by an outside reference, that reference is named beside it.
contains
- Carbon — element · the fibre, and it is electrically conductive — which is why an aluminium fitting bolted to it corrodes
is composed of
- Carbon fibre — 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
- Epoxy resin — material · the matrix, which holds the fibres in place and transfers load between them
is used as
- Structural engineering — application · aircraft primary structure since the 1990s, where stiffness per unit mass is what is being bought
is used in
- Aerospace manufacture — industry · primary structure — a modern wide-body wing and fuselage are more composite than metal
is an alternative to
- Glass fibre composite — material · five times the stiffness at 80 per cent of the weight, and perhaps ten times the price — which is why a hull is glass and a wing is carbon
- 7000 series aluminium alloy — alloy · stiffer and lighter, and it fails without deforming first — which removes the warning an inspector relies on in metal, and is why composite structure is inspected ultrasonically
is produced by
- Heat treatment — process · laid up as fibre and resin and cured under heat and pressure, usually in an autoclave — and the cure schedule is as much of the specification as the fibre is
Sources
- Material WorldOur own writing
- Wikimedia Foundation · Creative Commons CC0 1.0 Universal (public domain dedication)