• Proceedings of the Korean Ceranic Society Conference
• /
• 2002.10a
• /
• pp.101.1-101
• /
• 2002

• Journal of the Korean Ceramic Society
• /
• v.38 no.4
• /
• pp.351-359
• /
• 2001

배향 입자층과 비배향 입자층이 상호적층된 알루미나 적층복합체를 연속 테입캐스팅 및 상압소결에 의해 제조하였다. 알루미나의 미세구조 배향을 위하여 알루미나 판상입자를 배향물질(template)로 사용하였으며, 알루미나의 입자배향 거동에 미치는 액상의 영향을 알아보기 위해 anorthite(CaAl$_2$Si$_4$O$_{8}$)를 첨가하였다. 적층체 내의 알루미나 입자배향을 X-선 회절법으로 분석한 결과 (006)면과 (1010)면으로 배향되어 있었다. 액상조성이 첨가되지 않은 경우와 비교시 anorthite를 첨가한 경우 입자배향층 내에는 액상으로 인한 큰 기공이 생성되었으며 배향도는 감소되었다. 그러나, 액상조성으로 anorthite가 첨가되어 입자배향이 이루어진 적층체 계면에서는 입자배향으로 인한 효과적인 균열전파 제어 거동이 관찰되었다.

• Proceedings of the Korean Ceranic Society Conference
• /
• 2003.04a
• /
• pp.195.2-195
• /
• 2003

• Proceedings of the Korean Ceranic Society Conference
• /
• 2003.10a
• /
• pp.207.1-207
• /
• 2003

• Journal of Power System Engineering
• /
• v.18 no.6
• /
• pp.166-173
• /
• 2014

In this study, a laminated composite material with dispersing aluminum oxide powder between the CFRP laminate plies, and also CFRP composites without aluminium oxide powder were fabricated for Mode I experiments using the DCB specimen and a tensile test. The behavior of the crack and the change of the interfacial fracture toughness were evaluated. Also in order to evaluate the damage mechanism for the crack extension, the AE sensor on the surface of the DCB test specimen was attached. AE amplitude was estimated for CFRP-alumina and CFRP composite. And the fracture toughness was evaluated by the stress intensity factor and energy release rate. The results showed that an unstable crack was propagated rapidly in CFRP composite specimen along with the interface, but crack propagation in CFRP-alumina specimen was relatively stable. From results, we show that aluminium oxide powder spreaded uniformly in the interface of the CFRP laminate carried out the role for preventing the sudden crack growth.

• Korean Journal of Materials Research
• /
• v.23 no.9
• /
• pp.531-536
• /
• 2013

This paper investigates the effect of prolonged high temperature exposure on concentric laminated $Al_2O_3-ZrO_2$ composites. An ultrafine scale microstructure with a cellular 7 layer concentric lamination with unidirectional alignment was fabricated by a multi-pass extrusion method. Each laminate in the microstructure was $2-3{\mu}m$ thick. An alternate lamina was composed of 75%$Al_2O_3$-(25%m-$ZrO_2$) and t-$ZrO_2$ ceramics. The composite was sintered at $1500^{\circ}C$ and subjected to $1450^{\circ}C$ temperature for 24 hours to 72 hours. We investigated the effect of long time high temperature exposure on the generation of residual stress and grain growth and their effect on the overall stability of the composites. The residual stress development and its subsequent effect on the microstructure with the edge cracking behavior mechanism were investigated. The residual stress in the concentric laminated microstructure causes extensive micro cracks in the t-$ZrO_2$ layer, despite the very thin laminate thickness. The material properties like Vickers hardness and fracture toughness were measured and evaluated along with the microstructure of the composites with prolonged high temperature exposure.