TY - JOUR
T1 - Thermal expansion coefficient and thermal fatigue of discontinuous carbon fiber-reinforced copper and aluminum matrix composites without interfacial chemical bond
AU - Lalet, Grégory
AU - Kurita, Hiroki
AU - Heintz, Jean Marc
AU - Lacombe, Guillaume
AU - Kawasaki, Akira
AU - Silvain, Jean François
N1 - Funding Information:
Acknowledgements The authors would like to thank the ‘‘Déléga-tion Générale pour l’Armement’’ and ‘‘Région Aquitaine’’ for financial support.
PY - 2014/1
Y1 - 2014/1
N2 - Fully dense carbon fiber-reinforced copper and aluminum matrix (Cu-CF and Al-CF) composites were fabricated by hot press without the need for an interfacial chemical compound. With 30 vol% carbon fiber, the thermal expansion coefficients (TECs) of pure Cu and Al were decreased to 13.5 × 10 -6 and 15.5 × 10-6/K, respectively. These improved TECs of Cu-CF and Al-CF composites were maintained after 16 thermal cycles; moreover, the TEC of the 30 vol% Cu-CF composite was stable after 2500 thermal cycles between -40 and 150 °C. The thermal strain caused by the TEC mismatch between the matrix and the carbon fiber enables mechanical enhancement at the matrix/carbon fiber interface and allows conservation of the improved TECs of Cu-CF and Al-CF composites after thermal cycles.
AB - Fully dense carbon fiber-reinforced copper and aluminum matrix (Cu-CF and Al-CF) composites were fabricated by hot press without the need for an interfacial chemical compound. With 30 vol% carbon fiber, the thermal expansion coefficients (TECs) of pure Cu and Al were decreased to 13.5 × 10 -6 and 15.5 × 10-6/K, respectively. These improved TECs of Cu-CF and Al-CF composites were maintained after 16 thermal cycles; moreover, the TEC of the 30 vol% Cu-CF composite was stable after 2500 thermal cycles between -40 and 150 °C. The thermal strain caused by the TEC mismatch between the matrix and the carbon fiber enables mechanical enhancement at the matrix/carbon fiber interface and allows conservation of the improved TECs of Cu-CF and Al-CF composites after thermal cycles.
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U2 - 10.1007/s10853-013-7717-7
DO - 10.1007/s10853-013-7717-7
M3 - Article
AN - SCOPUS:84891343597
SN - 0022-2461
VL - 49
SP - 397
EP - 402
JO - Journal of Materials Science
JF - Journal of Materials Science
IS - 1
ER -