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Lu<sub>2</sub>O<sub>3</sub>-SiO<sub>2</sub>계 소결조제를 포함하는 Silicon Nitride의 소결 특성 및 기계적 거동
이세훈,조춘래,박영조,고재웅,김해두,Lee, Sea-Hoon,Jo, Chun-Rae,Park, Young-Jo,Ko, Jae-Woong,Kim, Hai-Doo 한국세라믹학회 2011 한국세라믹학회지 Vol.48 No.5
Gas pressure sintering (GPS) of reaction bonded silicon nitride (RBSN) was performed using $Lu_2O_3-SiO_2$ additive and the properties were compared with those of specimens prepared using high purity $Si_3N_4$ powder. The relative density of RBSN and compacted $Si_3N_4$ powder were 68.9 and 47.1%, and total linear shrinkage after sintering at $1900^{\circ}C$ were 14.8 and 42.9%, respectively. High nitrogen partial pressure (5MPa) was required during sintering at $1900^{\circ}C$ in order to prevent the decomposition of the nitride and to promote the formation of SiC. The relative density and 4-point bending strength of RBSN and $Si_3N_4$ powder compact were 97.7%, 954MPa and 98.2%, 792MPa, respectively, after sintering at $1900^{\circ}C$. The sintered RBSN also showed high fracture toughness of 9.2MPam$^{1/2}$.
보론과 카본 조제를 사용한 AlN-SiC-TiB<sub>2</sub>계의 고온가압 및 Spark Plasma Sintering
이세훈,김해두,Lee, Sea-Hoon,Kim, Hai-Doo 한국세라믹학회 2009 한국세라믹학회지 Vol.46 No.5
Effects of boron and carbon on the densification and thermal decomposition of an AlN-SiC-$TiB_2$ system were investigated. $SiO_2$ was mostly removed by the addition of carbon, while $Al_2O_3$ formed $Al_4O_4C$ and promoted the densification of the systems above $1850^{\circ}C$. Rather porous specimens were obtained without the additives after hot pressing at $2100^{\circ}C$, while densification was mostly completed at $2000^{\circ}C$ by using the additives. The sintering temperature decreased further to $1950^{\circ}C$ by applying spark plasma sintering. The additives promoted the shrinkage of AlN by forming a liquid phase which was originated from the carbo- and boro-thermal reduction of $Al_2O_3$ and AlN.
이세훈 ( Sea-hoon Lee ),룬펑 ( Feng Lun ),정경운 ( Kyeongwoon Chung ) 한국복합재료학회 2017 Composites research Vol.30 No.2
ZrB<sub>2</sub>, ZrC, HfB<sub>2</sub>, HfC 및 TaC 등의 초고온 세라믹스들은 극초음속 체계의 노즈콘, 로켓 노즐 및 리딩 엣지 등에 적용하기 위하여 최근 활발한 연구가 진행되고 있다. 그러나 그 실제 적용은 다양한 원인 때문에 제약받고 있는데 취성 특성에 의한 낮은 열충격 저항 특성이 그 원인 중 하나이다. 그러한 문제는 세라믹 섬유강화 복합재료를 제조함으로써 개선될 수 있다. 본 리뷰에서는 초고온 세라믹스의 개념과 초고온 세라믹스 섬유강화 복합재료(UHTC-CMC)의 제조 공정 및 평가에 대하여 간단히 정리하였다. 또한 UHTC-CMC의 제조를 위한 세계적인 연구를 요약하였으며 한국에서 수행중인 초고온 세라믹스 연구에 대해 간단히 소개하였다. Ultra-high temperature ceramics (UHTC) such as ZrB<sub>2</sub>, ZrC, HfB<sub>2</sub>, HfC and TaC has been recently actively investigated for the application as components such as nose-cone, rocket nozzle and leading edge of hypersonic systems. However, the application has been limited by various reasons. The brittleness of the materials and consequent low thermal shock resistance is one of the reasons. The property can be improved through the fabrication of ceramic matrix composites. In this paper, the concept of UHTC and the fabrication process and testing of UHTCbased ceramic matrix composites (UHTC-CMC) were briefly reviewed. Also, international activities regarding the fabrication of UHTC-CMC were summarized and a UHTC-CMC project, which was performed in Korea, was introduced.