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On the impact performance of carbon fibre laminates with epoxy and PEEK matrices
Authors:G Dorey  SM Bishop  PT Curtis
Affiliation:Materials and Structures Department, Royal Aircraft Establishment, Farnborough, Hampshire GU14 6TD Great Britain
Abstract:A study was made of the mechanical properties and impact performance of carbon fibre/PEEK (0,90), (±45) and (±45,0) laminates and comparisons were made with similar carbon fibre/epoxy laminatesFibre dominated properties such as plain tensile strength were similar to those of epoxy laminates with similar fibres and volume fractions. Because of the increased toughness of PEEK there was less extensive matrix cracking, even though there was fibre debonding, and this gave increased transverse and shear cracking strains, increased shear strengths but decreased notched tensile strengths. The lower modulus and yield stress of PEEK caused lower compressive strengths, but PEEK absorbed little moisture and at 120°C moisture had little effect on mechanical properties.Dropweight impact produced less extensive damage in carbon fibre/PEEK laminates. Residual tensile strengths were similar but, because of the less extensive damage and greater delamination fracture energy, the residual compressive strengths were significantly greater with a PEEK matrix.Microscopic examination showed less matrix cracking and more fibre buckling in the carbon fibre/PEEK and this is discussed in relation to mechanical properties.
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