• 한국세라믹학회지
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• 제34권12호
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• pp.1268-1274
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• 1997

Effect of elastic/plastic mismatch on the fracture of Si3N4 coating in Si3N4/Si3N4 -BN bilayer was investigated by Hertzian indentation testing. A different amount of mismatch between two layers was induced by different BN addition in the substrate layer, and Hertizian cracks were induced by using WC ball indenter. As a result, as the elastic/plastic mismatch between coating and substrate layer increased, the coating fracture easily occurred. A bending stress induced by different elastic/plastic mismatch was main reason to cause the fracture of coating.

• 한국윤활학회:학술대회논문집
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• 한국윤활학회 2002년도 제35회 춘계학술대회
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• pp.248-254
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• 2002

The most controversial topics in plasma sprayed ceramic coating system are recently mechanical properties such as bond strength, cohesive strength, toughness and so on. Determination of bond strength of coatings is one of the most important problems. In the industry, the bond strength of coating system has been estimated by Pull-off test(ASTM standard C633-79). But, without a fixed jig and specimen, it is impossible to obtain the bond strength. Therefore, it is necessary to study the critical fracture load on interface of the coating by indentation test. Because the critical fracture load plays an important role in evaluating the bond strength for plasma sprayed ceramic coating system. So, we have estimated critical fracture load in plasma sprayed ceramic coating system, and it was shown that inverse relationship between the cross-section hardness of coating and the critical fracture load(Pc). In case of the high load(1kgf, 2kgf) in $Al_{2}O_{3}+13%TiO_{2}$, it was found that the critical point(Pco), which the coating was broken on.

• 한국세라믹학회지
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• 제35권1호
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• pp.48-54
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• 1998

Part I에 이어서 질화규소로 코팅된 질화규소-질화붕소 시스템에 있어서 접촉하중에 의한 코팅층의 파괴에 대한 코팅층의 두께의 영향을 고찰하였다. 코팅층과 기판층간의 elastic/plastic mismatch가 큰 경우 코팅층의 균열생성을 방지하는 어느 임계 두께가 존재한다는 사실을 발견하였으며, mismatch가 감소할수록 이러한 요구 임계두께가 감소하였다. 또한 가해진 하중이 증가할수록 요구 임계두께는 증가하여야 함을 알 수 있었다. 따라서 코팅층의 파괴를 방지하기 위해서는 코팅층과 기판층간의 mismatch와 사용환경(가해지는 하중)을 고려한 적정 임계두께늬 설계가 요구된다.

• 한국정밀공학회지
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• 제24권3호
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• pp.91-99
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• 2007

Fractures of galvannealed coating layer during actual press forming in automotive applications were observed by scanning electron microscopy in order to understand fracture mechanism. Fracture behaviors of galvannealed coating layer in extra deep drawing quality steels and high strength steels have been studied by performing the tests describing the representative plastic deformation in sheet metal forming such as uni-axial tensile test, compression test, bi-axial test and plane strain test. Growth and direction of cracks were deeply related to the plastic deformation modes and history. The material properties of galvannealed coating layer were investigated by nano-indentation test equipped with Berkovich diamond indentor for the specimens. Hardness and elastic modulus of the coating layer were higher than bared steels and that was the reason for crack of coating layer. Flat friction test and drawbead friction test were performed to observe the effect of the surface morphology on the frictional characteristics. The micro-plasto hydrodynamic lubrication were appeared and played an important role in reducing the coefficient of friction.

• Composites Research
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• 제13권3호
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• pp.48-57
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• 2000

앞 동반논문의 이론에서 기술된 기재위에 입혀진 코팅크랙킹의 파괴역학 분석을 4점 굴곡시험을 이용하여 실증하였다. 파괴역학 접근에 의해서 코팅의 다중크랙킹을 예측하여 코팅층에서 새로운 크랙이 생길 때의 변위에너지 방출량(G)을 구하였다. 여러 건조시간과 건조온도의 변화에 따른 금속 및 고분자 기재위에 입혀진 코팅의 변위에 대한 코팅 크랙밀도의 실험데이타가 in-situ 코팅의 파괴인성 값을 구하기 위해 사용되었다. 건조온도가 올라가고 건조시간이 길어짐에 따라 $G_c$는 감소하였다. 본 논문은 코팅의 파괴인성 평가에 있어 4점 굴곡시험이 얼마나 유용한지를 보여주며 in-situ 코팅인성을 구하는 방법을 제시하였다.

• Composites Research
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• 제13권3호
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• pp.38-47
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• 2000

기재위에 입혀진 코팅에서 발생하는 크랙킹 현상을 파괴역학을 이용해서 분석하였다. 코팅/기재 구조에서 굽힘모드시 발생하는 코팅크랙킹을 변분법을 이용하여 분석하였으며, 본 연구에서 유도된 변위에너지 방출량을 통해 기재위에 입혀진 코팅층에서 크랙이 확장되는 것을 예측할 수 있다. 본 연구를 통해 얻어진 코팅의 임계 변위에너지 방출량은 재료의 고유성질이며 코팅크랙킹의 보다 근본적인 의미를 제공할 수 있다.

• Nuclear Engineering and Technology
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• 제53권4호
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• pp.1250-1258
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• 2021

In this paper, the mechanical performance of cracked surface-coated Zircaloy cladding, which has different coating materials, coating thicknesses and initial crack lengths, has been investigated. By analyzing the stress field near the crack tip, the safety zone range of initial crack length has been decided. In order to determine whether the crack can propagate along the radial (r) or axial (z) directions, the energy release rate has been calculated. By comparing the energy release rate with fracture toughness of materials, we can divide the initial crack lengths into three zones: safety zone, discussion zone and danger zone. The results show that Cr is suitable coating material for the cladding with a thin coating while Fe-Cr-Al have a better fracture mechanical performance in the cladding with thick coating. The Si-coated and SiC-coated claddings are suitable for reactors with low power fuel elements. Conclusions in this paper can provide reference and guidance for the cladding design of nuclear fuel elements.

• 한국세라믹학회지
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• 제44권7호
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• pp.368-374
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• 2007

CVD-SiC coating has been introduced as a protective layer in TRISO nuclear fuel particle of high temperature gas cooled reactor (HTGR) due to its excellent mechanical stability at high temperature. In order to prevent the failure of the TRISO particles, it is important to evaluate the fracture strength of the SiC coating layer. It is needed to develop a new simple characterization technique to evaluate the mechanical properties of the coating layer as a pre-irradiation step. In present work, direct strength measurement method with the specimen of hem i-spherical shell configuration was suggested. The indentation experiment on a hemisphere shell with a plate indenter was conducted. The fracture strength of the coating layer is related with the critical load for radial cracking of the shell. The finite element analysis was used to drive the semi-empirical equation for the strength measurement. The SiC hemispherical shells were successfully recovered from the section-grinding of TRISO coated particle and successive heat treatment in air. The strength of CVD-SiC coating layer was evaluated from the experimentally measured critical load during the indentation on SiC hemisphere shell. Weibull diagram of fracture strength was also constructed. This study suggested a new strength equation and experimental method to measure the fracture strength of CVD-SiC coating of TRISO coated fuel particles.

• 한국세라믹학회지
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• 제43권8호
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• pp.492-497
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• 2006

SiC coating has been introduced as protective layer in TRISO nuclear fuel particle of High Temperature Gas cooled Reactor (HTGR) due to excellent mechanical stability at high temperature. In order to inhibit the failure of the TRISO particles, it is important to evaluate the fracture strength of the SiC coating layer. ]n present work, thin silicon carbide coating was fabricated using chemical vapor deposition process with different microstructures and thicknesses. Processing condition and surface status of substrate.affect on the microstructure of SiC coating layer. Sphere indentation method on trilayer configuration was conducted to measure the fracture strength of the SiC film. The fracture strength of SiC film with different microstructure and thickness were characterized by trilayer strength measurement method nanoindentation technique was also used to characterize the elastic modulus and th ε hardness of the SiC film. Relationships between microstructure and mechanical properties of CVD SiC thin film were discussed.

• 한국결정성장학회:학술대회논문집
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• 한국결정성장학회 1997년도 Proceedings of the 12th KACG Technical Meeting and the 4th Korea-Japan EMGS (Electronic Materials Growth Symposium)
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• pp.19-22
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• 1997

The surface modificaion of alumina by $Al_2$O$_3$/SiC nanocomposite coating was studied in terms of processing and microstructure. A powder slurry of 5 vol% SiC composition was dipcoated onto presintered alumina bodies and pressurelessly sintered at 1$700^{\circ}C$ for 2 h in $N_2$. The used of organic binder and plasticizer in the slurry preparation, and the control of the density of presintered alumina body were found to be necessary to avoid cracking and warping during processing. The nanocomposite coating well bonded to the alumina body with thickness about 110 ${\mu}{\textrm}{m}$. The average grain size of coating (2 ${\mu}{\textrm}{m}$) was much finer than that of alumina body (13 ${\mu}{\textrm}{m}$). Fracture surface observations revealed mostly transgranular fracture for the coating, whereas intergranular fracture for the alumina body. Some pores (about 6%) were observed in the coating layer, although the alumina body showed fully dense microstructure.