Fibres de Berre : back to home
Fibres de Berre : back to home
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Aircraft body part
Superior drift of helicopter
AIRCRAFT COMPOSITE PARTS PRODUCTION
(PART 21G N°: FR.21G.135 Approval Certificate Scope of work : C2/D1)
MATERIALS USED :
reinforcements : carbon, aramid,
glass, metal
matrix : epoxy, phenolic, polyester
nida : nomex, aluminium, propylene
PROCESSING METHODS :
- CAD
- prototyping and mould manufacturing,
- contact moulding,
- compression moulding with chambers,
  press or autoclave,
- Resin Transfert Moulding
- Blow moulding
- Riveting
- Bonding
- painting
Engine pannel Engine BOR
doors made in glass
carbon fibres
Electric connexion box