Certify66
← Back to Materials & Hardware
Section 6.3.1(a)

Composite & Non-Metallic Materials

Fibres and matrices, fibre orientation and sandwich structure, and identifying the common composites and transparencies.

Notes

Composite & non-metallic materials, summary notes

Main ideas
  • A composite combines reinforcing fibres in a matrix: the fibres carry the load, and the matrix (usually an epoxy resin) transfers load between fibres, sets the shape and protects them. The result is high strength-to-weight, freedom from corrosion and properties that can be tailored by design.
  • Common fibres: glass (GFRP, cheap, radomes, fairings), carbon/graphite (CFRP, very stiff and strong, primary structure), aramid/Kevlar (tough, impact- and abrasion-resistant) and boron. The matrix is usually thermosetting epoxy.
  • Fibre orientation is everything, a laminate is strongest along its fibres, so plies are laid up at 0°/±45°/90° to carry loads in several directions. Honeycomb sandwich panels (a light core between thin facesheets) give great stiffness for very little weight.
  • ⚠ Exam trap: carbon fibre in contact with aluminium sets up galvanic corrosion that attacks the aluminium, so the two are separated by a glass-fibre or sealant barrier layer.
  • Transparencies are the non-metallic every category meets: acrylic and polycarbonate windows are handled to avoid crazing and scratches, and are never cleaned with solvents or dry-wiped.
Mind map

Composites concept map

Composite & Non-Metallic Materials

Quiz

Composite materials quiz

Composite & Non-Metallic Materials, quiz

Ref 6.3.1(a)8 of 11Pass 75%
  1. 1. In a composite material, the fibres mainly provide:

    Strength and stiffness
    Protection from moisture
    Electrical bonding
  2. 2. The matrix (resin) in a composite serves to:

    Bind the fibres and transfer load between them
    Carry all the strength
    Conduct electricity
  3. 3. In a composite, the load is mainly carried by the:

    Reinforcing fibres
    Resin matrix
    Paint finish
  4. 4. The matrix in a composite serves to:

    Transfer load between fibres and hold their shape
    Carry all the tensile load
    Provide the colour only
  5. 5. Carbon-fibre reinforced plastic (CFRP) is chosen for primary structure because it is:

    Very stiff and strong for its weight
    The cheapest option
    Electrically insulating and soft
  6. 6. A composite laminate is strongest:

    Along the direction of its fibres
    Across the fibres
    Equally in all directions regardless of layup
  7. 7. Carbon fibre in direct contact with aluminium causes:

    Galvanic corrosion of the aluminium
    No reaction
    Corrosion of the carbon
  8. 8. A honeycomb sandwich panel gives:

    High stiffness for very low weight
    High weight for low stiffness
    Good electrical conductivity