Carbon Fiber and Composites in Manufacturing
Composites are specified by layup and resin as well as fibre, and machining them is a delamination problem rather than a cutting one. What a capability page needs to state.
Composites are specified by fibre, resin system, and layup together, because the same fibre in a different orientation is a different part. Machining them is a delamination problem rather than a material removal one.
Composites are the one material in this cluster where the stock is manufactured rather than bought, which changes what a supplier is actually being asked for. The programme argument is in manufacturing SEO.
Three things specify a composite, not one
A layup records the fibre orientation and stacking sequence of the plies, and it determines stiffness and strength directionally. The same fibre at a different orientation produces a part with different properties.
A resin system carries the temperature and chemical performance. Epoxy is the general aerospace choice, and other systems exist for higher temperature or faster cure. Prepreg and wet layup are different processes with different equipment.
Fibre type is the third variable. Carbon carries stiffness, glass carries cost, and aramid carries impact and abrasion, and hybrid layups combine them deliberately.
What drives the machining
Delamination is the failure mode rather than dimensional error. Cutting forces separate plies at the edge, and the damage is often invisible on the surface while the part is structurally compromised.
That makes tooling and support the capability rather than the machine. Composite machining is abrasive wear on the tool rather than shear, so diamond-coated tooling and controlled feed are the norm and tool cost is a real line in the quote.
Dust is a handling requirement rather than housekeeping. Carbon dust is conductive and respirable, so extraction and machine protection are prerequisites, and a shop without them should not be quoting the work.
What a capability page should state
A capability page must state process, materials, tolerances, capacity, certifications, and industries served, and composites belong there by fibre, resin, and process.
State whether the shop lays up or only machines supplied stock, since those are different businesses. Name the resin systems handled, whether autoclave or oven cure is available, and the extraction and inspection capability. Non-destructive inspection matters here because delamination is invisible, and aerospace work adds the requirements at aerospace and defense manufacturing.
The structure is at capability page structure and the cluster reasoning at materials.
Common questions
Is machining composites like machining aluminium?
No. The failure is delamination rather than dimension, tool wear is abrasive, and the dust is a facility requirement.
Does a shop need to lay up to serve this market?
No, and it should say which it does. Machining supplied panels and manufacturing parts from prepreg are different capabilities.
How is delamination detected?
By non-destructive inspection rather than by eye, which is why the inspection capability belongs on the page with the machining.
Why is tooling cost so high?
Fibre abrades the cutting edge continuously. Diamond tooling lasts and costs, and quoting from metal experience underprices it.
Last reviewed . Published by ManufacturingSEO.ai.