• 열처리공학회지
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• 제7권3호
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• pp.206-218
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• 1994

In 50%$NH_3+Air+N_2$ atmospheres, the effect of air additions on the growth characteristics of the compound layer during oxynitriding at $570^{\circ}C$ for 2hr in carbon and alloy steels has been investigated. The ammount of apparent residual ammonia during oxynitriding has shown to be increased with air additions(9~36 Vol. %) and X-ray diffraction analysis of case oxynitreded has shown that the compound layer consist of ${\varepsilon}-Fe_{2-3}$(N, C) phase and ${\gamma}^{\prime}-Fe_4$(N,C) phase. In the case of carbon steels, the thickness of oxide layer, compound layer and porous layer and the amount of ${\varepsilon}-Fe_{2-3}$(N,C) phase in the compound layer were increased with additions of air in 50%$NH_3+N_2$ atmospheres. At the same gas composition, the thickenss of oxide layer, compound layer and porous layer in alloy steels showed slightly thin layer thickness compared to those of carbon steels and the ${\gamma}^{\prime}-Fe_4$(N,C) phase in the compound layer of alloy steels was found barely. Therefore, the most obvious effect of air addition in the gas nitriding atmosphere has been found to in crease further kinetics of nitriding reaction.

• 한국표면공학회지
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• 제44권4호
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• pp.125-130
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• 2011

$Cr_2AlC$ compounds were synthesized by hot pressing, and oxidized between 900 and $1200^{\circ}C$ in air for up to 50 hours. They oxidized to a thin $Al_2O_3$ layer containing a small amount of $Cr_2O_3$with the liberation of carbon as CO or $CO_2$ gases. The consumption of Al to form the $Al_2O_3$ layer led to the depletion of Al and enrichment of Cr just below the $Al_2O_3$ layer, resulting in the formation of an underlying $Cr_7C_3$ layer. As the oxidation temperature and time increased, the $Cr_7C_3$ oxide layer and the underlying $Cr_7C_3$ layer thickened. The oxidation resistance of $Cr_2AlC$ was generally good due to the formation of the $Al_2O_3$ barrier layer.

• 열처리공학회지
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• 제8권4호
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• pp.289-301
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• 1995

The effect of Air/$C_3H_8$ gas addition on the compound layer growth of steels nitrocarburised in $NH_3+Air+C_3H_8$ mixed gas atmospheres was investigated. It is considered that amount of residual $NH_3$ was varied according to alternation of Air/$C_3H_8$ mixing ratio and volume content. The compound layer formed from nitrocarburising was composed of ${\varepsilon}-Fe_{2-3}$(C, N) and ${\gamma}^{\prime}-Fe_4$(C, N). According as Air/$C_3H_8$ mixing ratio increased, the superficial content of ${\gamma}^{\prime}-Fe_4$(C, N) within the compound layer was increased, at the same time the growth rate of compound layer and porous layer was increased. In the case of alloy steel at the fixed gas composition, the growth rate of compound layer and porous layer was worse than carbon steel and compound layer phase composition structure primarily consisted of E phase. As the carbon content of materials was increasing in the given gas atmospheres, the growth rate of compound layer and porous layer was increased and the superficial content of ${\varepsilon}-Fe_{2-3}$(C, N) within the compound layer was increased.

• 한국재료학회지
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• 제14권4호
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• pp.265-269
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• 2004

Plasma nitrocarburising and post oxidation were performed on SCM435 steel by a pulsed plasma ion nitriding system. Plasma oxidation resulted in the formation of a very thin ferritic oxide layer 1-2 $\mu\textrm{m}$ thick on top of a 15～25 $\mu\textrm{m}$ $\varepsilon$-F $e_{2-3}$(N,C) nitrocarburized compound layer. The growth rate of oxide layer increased with the treatment temperature and time. However, the oxide layer was easily spalled from the compound layer either for both oxidation temperatures above $450^{\circ}C$, or for oxidation time more than 2 hrs at oxidation temperature $400^{\circ}C$. It was confirmed that the relative amount of $Fe_2$$O_3$, compared with $e_3$$O_4$, increased rapidly with the oxidation temperature. The amounts of ${\gamma}$'-$Fe_4$(N,C) and $\theta$-$Fe_3$C, generated from dissociation from $\varepsilon$-$Fe_{2-3}$ /(N,C) phase during $O_2$ plasma sputtering, were also increased with the oxidation temperature.e.

• 열처리공학회지
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• 제15권5호
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• pp.219-227
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• 2002

This study has been performed to investigate the effect of $CO_2$ content on the growth characteristics of the compound layer, porous layer and corrosion characteristics of carbon steels after gaseous nitrocarburizing in $70%-NH_3-CO_2-N_2$ at $580^{\circ}C$ for 2.5 hrs. The results obtained from the experiment were the thickness of the compound and porous layers increased with increasing $CO_2$ contents. At the same fixed gas composition the thickness of the compound and porous layer increased with increasing carbon content of the specimens. X-ray diffraction analysis showed that compound layer was mainly consisted of ${\varepsilon}-Fe_{2-3}(N,C)$ and ${\gamma}^{\prime}-Fe_4N$ as the increased with $CO_2$ contents in atmosphere, compound layer was chiefly consisted of ${\varepsilon}-Fe_{2-3}(N,C)$ phase. With increasing $CO_2$ content and total flow rate in gaseous nitrocarburizing, the amount of ${\varepsilon}-Fe_{2-3}(N,C)$ phase in the compound layer was increased. The current density of passivity decreased with increasing $CO_2$ content due to the development of porous layer at the out most surface of ${\varepsilon}-Fe_{2-3}(N,C)$.

• 한국진공학회:학술대회논문집
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• 한국진공학회 2016년도 제50회 동계 정기학술대회 초록집
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• pp.237.2-237.2
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• 2016

A pure hafnium-carbide (HfC) coating layer was deposited onto carbon/carbon (C.C) composites using a vacuum plasma spray system. By adopting a SiC buffer layer, we successfully integrated C.C composites with a $100-{\mu}m-thick$ protective coating layer of HfC. Compared to the conventional chemical vapor deposition process, the HfC coating process by VPS showed increased growth rate, thickness, and hardness. The growth behavior and morphology of HfC coatings were investigated by FE-SEM, EDX, and XRD. From these results, it was shown that the addition of a SiC intermediate layer provided optimal surface conditions during the VPS procedure to enhance adhesion between C.C and HfC (without delamination). The thermal ablation test results shows that the HfC coating layer perfectly protected inner C.C layer from thermal ablation and oxidation. Consequently, we expect that this ultra-high temperature ceramic coating method, and the subsequent microstructure that it creates, can be widely applied to improve the thermal shock and oxidation resistance of materials under ultra-high temperature environments.

• 한국재료학회지
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• 제8권10호
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• pp.925-930
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• 1998

LPE법을 이용하여 $Bi_2Sr_2-\chi_LCa_1+\chi_LCu_2O_{8+d}$(xL=0, 0.1, 0.2 ,0.3, 0.4, 0.5, 0.6)막(film)을 작성하여 XPS 측정과 EPMA측정을 통하여 Sro-layer와 Ca-layer에 있어서 Sr과 Ca의 상호치환 상태와 초전도특성을 조사하였다. 작성한 막(film)은 c-축으로 강하게 배향되었고, $\chi_L$(용액조성비)의 증가에 따라 임계온도 $T_C^{zero}$와 c-축의 길이는 단조로이 감소를 보였으며, Car-rier농도는 약간 감소하는 경향을 보였다. 또한, SrO-layer에서는 Sr은 $\chi_L$의 증가에 따라 감소를 보이며, Ca는 약 0.15에 포화된 후 약간 감소하였다. Ca-layer에서의 Sr과 Ca는 $\chi_L$에 비례적으로변하며, 이때 변화율은 SrO-layer보다 컸다. 이런 현상은 Sr이 양쪽 layer에서 감소하는데 비하여, Ca는 거의 Ca-layer에서만 증가함을 의미하는 것이다. $\chi_L$의 증가에 따라, SrO-layer에서의 결손은 증가를 보였으며, 이는 SrO-layer에서 결손이 임계온도 $T_C^{zero}$의 감소에 영향을 미쳤다고 생각된다.

• 한국세라믹학회지
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• 제31권8호
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• pp.874-878
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• 1994

To increase the anti-oxidation and anti-wear properties of graphite for the propellant-burning environment, SiC, Pt and Al2O3 multi-layer coatings were conducted succesisvely and the optimum condition was researched. The SiC layer was produced by pack cementation and SiC layer in thickness of 30 ${\mu}{\textrm}{m}$ coating was produced after coating for 6 hours. Pt layer was coated by sputtering, and the Al2O3 layer was coated by reactive sputtering. the thickness of Pt layer and Al2O3 layer was less than one-tenth of that of SiC layer. The pack coated specimens and multi-layer coated specimens were made using above conditions and test-fired. The test result showed that the wear rate of SiC layer is approximately 1/10 compared to that of uncoated graphite.

• The Korean Journal of Ceramics
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• 제3권3호
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• pp.163-168
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• 1997

Most of heteroepitaxial $\beta$-SiC thin films have been successfully grown on Si(100) adapting a carburizing process, by which a few atomic layers of substrate surface is chemically converted to very thin SiC layer using hydrocarbon gas sources. Using an organo-silicon precursor, bis-trimethylsilymethane (BTMSM, [$C_7H_{20}Si_2$]), heteropitaxial $\beta$-SiC thin films were successfully grown directy on Si substrate without a carburized buffer layer. The defect density of the $\beta$-SiC thin films deposited without a carburized layer was as low as that of $\beta$-SiC films deposited on carburized buffer layer. In addition, void density was also reduced by the formation of self-buffer layer using BTMSM instead of carburized buffer layer. It seems to be mainly due to the characteristic bonding structure of BTMSM, in which Si-C was bonded alternately and tetrahedrally (SiC$_4$).

• 대한원격탐사학회지
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• 제17권1호
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• pp.1-14
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• 2001

굴절 지수 구조 매개 변수(refractive index structure parameter) $C_n^2$의 증가는 보통 가온위(virtual potential temperature) ${\theta}_v$와 혼합비(mixing ratio) q의 연직 기울기가 최대가 되는 고도에서 발생하며, 대류 경계층(convective boundary layer)의 고도를 추정하는데 있어서 매우 유용한 매개 변수로 사용된다. 이 연구에서는 대류 경계층 고도의 추정에 이용되는 $C_n^2$ 첨두의 발생 특성이 조사되었으며, 또한 UHF 레이더로 관측된 $C_n^2$와 연직 속도의 분산 ${\sigma}_w$ 자료를 이용하여 대류 경계층 고도를 객관적으로 추정하는 방법이 제시되었다. UHF 레이더의 $C_n^2$ 연직 분포에서 첨두는 대류 경계층의 정상부뿐만 아니라 잔류층의 정상부나 구름층에서도 발생하였다. 약한 태양 복사로 연직 혼합이 뚜렷하지 않은 경우에 대류 경계층 고도에 상응하는 $C_n^2$ 첨두는 레윈존데(rawinsonde) 관측 자료로부터 추정된 대류 경계층 고도보다 약간 낮았다. 반면에, 강한 태양 복사에 의해 연직 혼합이 강하고 유입대에서 ${\theta}_v$와 q의 연직 기울기가 매우 클 경우에 대류 경계층 고도에 상응하는 $C_n^2$ 첨두는 레윈존데 관측 자료로부터 추정된 대류 경계층 고도와 잘 일치하였다. $C_n^2$ 첨두의 고도를 대류 경계층 고도로 결정하는 최대 후방 산란 강도 방법(maximurn backscatter intensity method)은 $C_n^2$ 연직 분포에서 하나의 첨두가 있을 경우에는 오류 없이 대류 경계층 고도를 추정하였지만 대류 경계층 고도 위에 잔류층이나 구름층이 있을 경우에는 대류 경계층 고도를 잘못 추정하였다. 본 연구에서 새로이 제시된 방법은 UHF 레이더의 $C_n^2$와 ${\sigma}_w$ 자료를 이용하여 대류 경계층 고도로부터 오는 $C_n^2$ 첨두를 잔류층이나 구름층으로부터 오는 $C_n^2$ 첨두로부터 구별하여 오류 없이 대류 경계층 고도를 추정하였다. 또한 이 방법은 대류 경계층 고도의 일반화 추정에 적용되었으며, 후방 산란 강도의 연직 분포에서 두개의 첨두가 존해할 경우에도 더욱 신뢰성 있고 안정되게 대류 경계층 고도를 실시간으로 추정하였다.