• Proceedings of the Korean Vacuum Society Conference
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• 2016.02a
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• pp.135-135
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• 2016

차세대 가스터빈 엔진 및 초음속 항공기 내 고온부의 온도가 증가함에 따라, 기존의 초내열합금 기반 소재를 사용하기 어려워지고 있다. 초고온 세라믹스는 높은 기계적 물성, 화학적 안정성 등 우수한 고온 특성을 가지고 있어 기존의 초고온 소재를 대체 할 수 있는 물질로 부상되고 있다. 하지만 기존의 금속 기반 소재 대비 높은 밀도로 인하여 초고온 세라믹 단일체를 비행체 부품에 적용하기에는 어려움이 있다. 이에 초고온 세라믹스와 탄소섬유를 포함하는 세라믹 복합체(Ceramic Matrix Composite, CMC)를 제작하여 동등한 기계적 물성을 보이면서 무게를 감소시키는 연구들이 진행 중에 있다. 초고온 세라믹스가 함침 된 세라믹 복합체의 경우 우수한 내삭마, 내산화 특성을 보이지만, 장시간 고온에 노출되어 탄소 섬유가 드러나게 되면 급격한 산화로 인해 소재 특성의 열화가 진행되는 단점을 가지고 있다. 따라서, 탄소 섬유가 드러나지 않도록 복합체 표면에 코팅층을 형성하여 세라믹 복합체 모재를 보호하는 방법이 활발히 연구되고 있다. 본 연구에서는 진공 플라즈마 용사 공정을 이용하여 다양한 공정조건 하에서 초고온 세라믹 코팅층을 형성하였다. 수십 마이크론 크기 분포를 갖는 HfC 분말을 Ar 유송 가스를 이용하여 플라즈마 화염 내부로 투입하였다. 플라즈마 화염 가스는 Ar 과 H2를 혼합하여 구성되었으며, 분위기 가스로는 N2를 사용하였다. 코팅에 사용된 모재로는 ZrB2 단일체와 SiC가 미량 포함된 HfC 단일체를 사용하였다. 다양한 공정 조건하에서 형성된 HfC 코팅층의 두께, 미세 조직구조를 SEM을 이용하여 관찰하였으며, XRD를 이용하여 형성된 HfC 코팅층의 결정구조를 분석하였다.

• Journal of Welding and Joining
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• v.8 no.4
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• pp.58-68
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• 1990

The formation of thermal stresses by plasma spraying is generally considered as adverse. Therefore, the knowledge of stress distribution in the deposited layer during and after plasma spraying will be of special interest. In this study finite difference heat transfer analysis and finite element stress analysis were carried out to predict the change of stress distribution in the plasma coated layer with the variations of preheat temperature, number of scan, particle size, and bond coat. The results of the numerical analysis were as follows: 1) Transient stresses developed in the coated layer were up to the level of yiedl strength at the temperature. 2) The tensile stresses were developed in the deposited layer and the surface of the substrate, but the compressive stresses were developed in the rest of the substrate. 3) Transient and residual stresses were significantly affected by the preheat temperature. 4) The variations of temperature of powder particle and number of torch scan changed tensile stress distribution, but made no difference on the magnitude of the stresses. 5) Bond coated layer reduced the stree level of deposited layer.

• Journal of Power System Engineering
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• v.9 no.4
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• pp.90-95
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• 2005

The wire-arc process is a low-cost thermal spray method simply utilizes electrical energy to melt the feedstock wire. It is more userful for field applications, especially to coat large surface area. In this paper, a special Fe-based alloy coatings by using the wire-arc process were developed. Nanoscale composite coatings were achieved either during spraying or through a post heat treatment. As-sprayed Fe-based alloy coatings had been an amorphous matrix structure, after heating to $700^{\circ}C$ for 10 minutes a solid state transformation occurred in the some fraction of amorphous matrix which resulted in the formation of nanostructured recrystallized phase. Scanning electron microscopy (SEM) and field emotional scanning electron microscope(FE-SEM) were applied to analyze the microstructure of the coatings. Additionally hardness and bend resistance of the Fe-based alloy coatings were examined, and these results were compared with those of partially stabilized zirconia(PSZ) coatings by using the plasma spray process.

• The Monthly Technology and Standards
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• s.110
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• pp.32-35
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• 2011

ISO TC 107 총회에서 특히 우리나라는 WG1 주요 의제 10건 중 3건을 제안해 '세라믹 용사층의 기공률 측정방법'이 올 해 안 TR(Technical report) 발간을 앞두게 되었다. 김지영 현대하이스코 기술연구소 연구원의 참가 후기를 소개한다.

• Journal of Welding and Joining
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• v.15 no.4
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• pp.126-135
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• 1997

$H_2/O_2$ 비에 따른 Hybrid HVOF 용사된 $Cr_3C_2$-7wt%(NiCr) 용사층의 특성 및 산화거동 This study was performed to investigate the influence of fuel/oxygen ratio (F/O=3.2, 3.0, 2.8) on the characteristics and the oxidation behavior of the hybrid-HVOF sprayed $Cr_3C_2$-7wt%NiCr coatings. Decomposition and the oxidation of the $Cr_3C_2$was occured during spraying. The degree of transformation from $Cr_3C_2$to $Cr_7C_3$ was increased with decreasing the F/O ratio. The microstructural differences of the as sprayed coating with F/O ratio can not be distinguished, However, large pores were diminished and then the coatings became dense by heat treatment. Microhardness of the as-sprayed specimen which sprayed with F/O=3.0 condition was hightest ($Hv_{300}$=1140) and the hardness was increased to 1500 after heat treatment at $600^{\circ}C$ for 50hrs in air. It was supposed that hardness was increased due to the formation of $Cr_2O_3$ within $Cr_3C_2$/$Cr_7C_3$matrix and the densification of coating layer during heat treatment. Apparent activation energy for oxidation was varied from 21.2 kcal$mol^{-1}K^{-1}$ to 23.8 kcal$mol^{-1}K^{-1}$ with respect to the F/O ratio. The surface morphology was changed to porous and oxide chusters were grown after oxidation $1000^{\circ}C$ for 50 hours by the aggressive evolution of gas phase ($CrO_3$ and$CO_2$). The oxide cluster was composed of Ni and Cr.

• Journal of Welding and Joining
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• v.10 no.4
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• pp.213-221
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• 1992

Al$_{2}$O$_{3}$ ceramic coating layer by gas flame spraying was very porous, therefore it could not have wear and corrosion resistance at all. To get a dense and strong coating layer, a method to infiltrate an alloy into the pores of $Al_{2}$O$_{3}$ ceramic coating was investigated. Cu-Ti alloys, which had good wettability and reactivity with $Al_{2}$O$_{3}$ ceramic, were examined for infiltration. Infiltration of the alloys was performed in vacuum at 1100.deg.C. The melt of Cu-50 at % Ti alloy was well penetrated through the porous $Al_{2}$O$_{3}$ coating and tightly sealed the pores, unbounded area and microcracks in the coating. The alloy melt in the pores reacted with $Al_{2}$O$_{3}$ ceramic to produce a suboxide phase, Cu$_{2}$Ti$_{4}$O. This composite layer which was composed of $Al_{2}$O$_{3}$ and Cu$_{2}$Ti$_{4}$O phase had good microstructure and wear and corrosion resistance. Additionally, microstructures at interfaces between coating layers were greatly improved owing to the effect of vacuum heat treating.

• Journal of Welding and Joining
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• v.14 no.2
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• pp.19-27
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• 1996

재료의 표면개질은 표면층의 조직변화에 대한 개질법과 표면피복에 의한 개질 법으로 나눌 수 있다. 조직변화에 의한 개질법으로는 침탄, 질화, 이온주입 및 금속 확산 등이 있고, 표면피복에 의한 개질법으로는 도장, 도금, 육성용접, 물리증착(PVD) 및 화학증착(CVD) 등이 있는데, 용사법은 표면피복에 의한 개질법에 속한다. 용사기술 은 비교적 최근에 발달된 표면피복 기술로서 그림1과 같이 플라즈마, 가스화염 또는 아크열원을 이용하여 금속 또는 비금속 재료를 용융 혹은 반용융 상태로 모재에 고속 도로 분사하여 충돌 적층시켜 피복하는 공정으로 다른 표면개질기술에 비해서 여러 가지 잇점을 가지고 있다. 이것은 거의 모든 재질의 모재(금속, 세라믹, 유기재료 등) 에 대해 피막의 형성이 가능하고, 용사재료의 종류도 다양하다(금속, 합금, 각종 세라 믹, 플라스틱, 각종 복합재료 등). 또한 노재크기의 제한이 없고, 대형의 재료에 대해 서 한정된 부위의 피복이 가능하며, 모재의 열영향이 적고, 피막의 형성속도가 다른 피막법에 비해 빠른 장점을 가지고 있다. 그 예로 알루미나(Al$_{2}$O$_{3}$)를 피복할 경우 화학증착(CVD)법에 의해서는 피막형성 속도가 약 2 * $10^{-4}$mm/min 인데 비해 용사법에 의해서는 약 7.5 * $10^{-1}$mm/min로 매우크다. 이와같은 많은 장점을 갖고있는 용사법을 이용한 표면개질에 대해 본 기술보고에서 서술하고자 한다.

• 연구논문집
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• s.25
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• pp.193-205
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• 1995

Plasma spray coating technology is essential for the microsemiconductor processes based on the electronic and computer industry, and extend gradually the range of application for up-to-date industry such as diesel engine and gas turbine components. These thechonoogies may be applied to the components requiring wear-resistance, heat resistance, fatigue-resistance, and corrosion-resistance. In this research, plasma spray technology was selected for the wear resistant coatings as the most proper technique. The final goal of this study is to improve the wear resistance through establishment of coating soft-ware, and basic research for industrialization of the technology concerned.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.18 no.8
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• pp.1169-1175
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• 1993

Plasma spraying method was used to fabricated the microwave absorbing ferrite-silicon carbide on the aluminum-alloy of the fuselage of an aircraft to protect it from RADAR detection. In this paper 15[rm] instead of 34[rm], the mean size of SIC-powder for ferrite-silicon carbide surface films(I) was used. 50(Kg/h) Instead of 70(Kg/h), the powder feed and 100[mm] Instead of 80(mm), spray distance of spray parameters was used. This M/W absorbers were designed experimentally and fabricated trially, as a result of which the relative frequency bandwidth of 2.8% were obtained under the tolerance limits of the reflection coefficients lower than-10[dB], and the maximum absorption thickness becomes 0.5[mm], which is much thinner than that of the conventional ones.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2014.11a
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• pp.296-297
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• 2014

고체윤활제는 고온부품의 응용에 매우 적합한 소재이다. 세라믹스를 기반으로 하는 고온저마찰소재는 우주항공, 발전시설 등과 같은 다양한 분야에서 매우 중요하다. 본 연구는 고온저마찰 소재를 가지는 자기윤활 $Al_2O_3-ZrO_2$ 세라믹 복합 코팅층의 마찰마모거동에 초점을 맞추고 있다. 이 자기윤활 $Al_2O_3-ZrO_2$ 세라믹 복합 코팅층은 대기플라즈마 용사법으로 제작하였으며, 비윤활상태에서 마찰마모거동을 조사하였다.