• 한국진공학회지
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• 제2권2호
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• pp.236-245
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• 1993

SbSI : V, SbSeI : V, BiSI : V, BiSeI : V, SbSI : Cr, SbSeI : Cr, BiSI : Cr, BiSeI : Cr, SbSI : Ni, SbSeI : Ni, BiSI : Ni, 및 BiSeI : Ni 단결정을 고순도(99.9999%)의 성분원소에 혼합물을 투명석 영관내에 넣고, $1{\times}10^{-6}mmHg$의 진공에서 봉입하여 합성한 ingot를 사용하여, 수직 Bridgman 방법으로 성장시켰다. 성장된 단결정의 구조는 orthorhombic 구조이며, 광학적 energy band gap 구조는 간접전이형 이었고, energy gap의 온도의존성은 상전이에 관계되는 2개의 변곡점이 나타났으며, 연속된 영역에서는 Varshni 방정식을 만족하였다. 첨가한 3d 불순문(V, Cr, Ni)은 모결정의 $T_d$ 대칭을 갖는 주격자점에 +2가 ion으로 위치하며, 이들 ion의 energy 준위간의 전자전이에 의하여 불순물 광흡수 peak가 나타난다.

• 대한용접접합학회:학술대회논문집
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• 대한용접접합학회 2004년도 춘계 학술발표대회 개요집
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• pp.168-170
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• 2004

터빈로터는 발전설비 중에서 가장 핵심 부분이며 동시에 심한 고온 응력을 받는 부분이다. 터빈로터 재료로는 Ni-Cr-Mo-V강과 CrMoV 강등이 사용된다. CrMoV 강은 발전 설비로 장시간 사용 중 열적피로나 크립손상, 고온 부식 등의 문제가 단독 혹은 복합적으로 발생하여 재료에 손상을 입히게 되고 결국에는 설비의 수명을 단축 시키곤 한다. (중략)

• Journal of Welding and Joining
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• 제26권3호
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• pp.37-44
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• 2008

Charpy V-Notch test is commonly used to evaluate fracture toughness. However, since the region to be evaluated is limited to bulk material due to the specimen size required, individual evaluation of micro-structures on weldment is very difficult. In this study, ASP(Advanced Small Punch) test was carried out to evaluate material degradation and fracture toughness on the B.M, W.M and each micro-structures of HAZ for X20CrMoV121 and 2.25Cr1Mo steels with artificial aging time. In addition, to evaluate fracture toughness and material degradation of B.M and W.M of X20CrMoV121 steels with aging times, CVN (Charpy V-notch) test was performed. And then the correlation between ASP and CVN test on X20CrMoV121 steels was obtained. Furthermore, through this correlation, material degradation property of each micro-region of the HAZ in weldment, which was impossible to be evaluated by the CVN test, can be estimated and determined.

• 한국재료학회지
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• 제14권8호
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• pp.558-564
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• 2004

In order to improve the low hardness and low wear resistance of Ti-6Al-4V alloy, plasma carburization treatment and CrN film coating were carried out. Effects of the plasma carburization and CrN coating were analyzed and compared with the non-treated alloy by mechanical and creep tests. After plasma carburization and CrN coating treatments, the carburized layer was about 150 ${\mu}m$ in depth and CrN coated layer was about 7.5 ${\mu}m$ in thickness. Hardness value of about $H_{v}$ 402 of the non-treated alloy was improved to $H_{v}$ 1600 and 1390 by plasma carburization and CrN thin film coating, respectively. Stress exponent(n) was decreased from 9.10 in CrN coating specimen to 8.95 in carburized specimen. However, the activation energy(Q) was increased from 242 to 250 kJ/mol. It can be concluded that the static creep deformation for Ti-6Al-4V alloy is controlled by the dislocation climb over the ranges of the experimental conditions.

• 한국표면공학회지
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• 제49권2호
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• pp.211-217
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• 2016

Boride coating applied on steam turbine parts of power plants has provided good particle erosion resistance under temperature of $550^{\circ}C$, but it isn't able to protect the parts effectively any more in ultra super critical (USC) steam turbine which is being operated up to temperature of $650^{\circ}C$. To ensure stable durability for USC steam turbine parts, an alternative coating replacing boride coating should be developed. In this study, multi-component boride coatings containing elements such as chromium (Cr) and vanadium (V) were formed on base metal (B50A365B) using thermochemical treatment method called by pack cementation. The thermochemical treatments involve consecutive diffusion of boron(B) and Cr or/and V using pack powders containing diffusion element sources, activators and diluents. The top layer of Cr-boride coating is primarily consisted of $Cr_2B_3$ and $Cr_5B_3$, while that of V-boride coating is mostly consisted of $VB_2$ and $V_2B_3$. The (Cr,V)-boride coating is consisted of $Cr_2B_3$, $Cr_5B_3$ and $V_2B_3$ mostly. The top surfaces of 3 multi-component boride coatings show hardness of $3200-3400H_v$, which is much higher than that of boride, about $1600-2000H_v$. In 5 wt.% NaCl solution immersion tests, the multi-component boride coatings show much better corrosion resistance than boride coating.

• 콘크리트학회논문집
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• 제18권5호
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• pp.621-630
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• 2006

산업부산물을 활용한 고강도 경량 콘크리트 보의 역학적 거동 구명과 함께 경량 콘크리트 보의 이론식을 바탕으로 합리적인 전단강도식을 제안하였다. 보는 경량 골재를 사용한 고강도 경량 콘크리트 보(L) 8개와 일반 골재를 사용한 고강도콘크리트 보(H) 4개의 실험체를 제작하였다. 그리고 전단스팬비(a/b=1.5, 2.5, 3.5, 4.5), 인장철근비(${\rho}$=0.57, 1.0, 1.59, 2.3%), 콘크리트의 압축강도(35.4, 65.3MPa)를 주요 변수로 설정하여 실험하였다. 이로부터 보에 대한 하중-처짐관계 및 변형률 분포, 파괴성상, 최대내력 등에 대하여 측정하였다. 또한 보의 전단강도식의 제안을 위하여 사인장 균열 강도와 극한전단강도로 세분화하여 기존 제안식과 규준식에 적용시켜 상호 비교 분석을 하였다. $V_{cr}$에 있어서는 a/b=2.5 이상에서는 ACI 규준식과 Zsutty제안식에서 감소하는 결과였지만, Mathey의 제안식에서는 약간의 상승 경향을 보였다. 또한, ${\rho},\;f_c$의 증가에 따라 $V_{cr,\exp}/V_{cr,cal}$은 과대평가의 경향이 나타났다. 한편, $V_{u, \exp}/V_{u,cal}$에서는 통계적인 방법으로 유도된 Zsutty의 제안식이 실험결과와의 일치성에서 좋은 결과를 보였다. 이 식으로부터 유도 수정된 전단강도에 대한 제안식은 $V_{cr},\;V_u$에서 합리적으로 예측할 수 있음을 알 수 있었다. 따라서 본 연구에서 제안된 전단강도 식은 경량 콘크리트의 전단스팬비, 인장철근비, 콘크리트 압축강도의 변화에 따른 전단내력을 합리적으로 평가하는데 유용하게 활용될 수 있을 것으로 사료된다.

• 한국자기학회:학술대회 개요집
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• 한국자기학회 2005년도 하계학술연구발표회 논문개요집
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• pp.44-44
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• 2005

• KSBB Journal
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• 제15권1호
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• pp.49-54
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• 2000

1.0%(w/v)의 CMC 담체는 고정화를 유지할 수 있는 점도를 가지며 0.1 M 이하의 양이온과 이온가교결합을 할 수 있는 농도이다. Luminometer tube내의 시료에 유동을 최소화함으로써 산소의 공급을 일정하게 하여 P. phosphoreum을 고정화 30분 후 bioluminescence intensity가 안정되어 바로 측정할 수 있는 장점을 가지고 있었다. 1.0%(w/v) CMC담체는 pH 6.92로 최적조건인 pH 7.0에 근접했으며, 발광기작에 필요한 산소전달(oxygen transfer)이 1.5%(w/v)~3.0%(w/v) CMC 담체보다 뛰어나 Bioluminescence intensity의 안정성을 부여하였다. Cr-화합물인 $Na_{2}CrO_{4}$, $K_{2}CrO_{4}$, $CrO_{3}$, CrK$(SO_4)_{2}$ 및 $CrCl_{3}$의 CMC담체에 대한 민감도는 $\gamma$값을 이용해서 $EC_{50}$값으로 나타내었을 때 $Na_{2}CrO_{4}$, $K_{2}CrO_{4}$, CrK$(SO_4)_{2}$ 및 $CrCl_{3}$ 의 $EC_{50}$값이 1.0%(w/v)CMC에서는 5.4~16.3 g/L으로 1.5%(w/v)~3.0%(w/v) CMC에서는 6.2~555.9 g/L의 범위로 나타났다. 이것은 1.0%(w/v) CMC가 낮은 독성 농도에서 bioluminescence intensity가 50% 감소함을 알 수 있고, 상관계수($R^2$)가 0.911~0.990 으로 높게 산출되었다. 따라서 1.0%(w/v) CMC 담체가 P. phosphoreum의 biolumincsene에 안정성을 주었으며, 독성물질에 가장 민감하다는 것을 알 수 있었다.

• 한국해양공학회지
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• 제3권2호
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• pp.125-137
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• 1989

To check technical improvement in the soundness and strength of 12% Cr steel rotor, a 25 tons of rotor with 65 tons of ingot was made in real size and was cut to pieces to take test samples, and the various mechanical tests such as impact, tensile, creep, and fatigue were carried out. The strengths are compared with those of 1% Cr-Mo-V rotor of same size. Microstructures of the samples are examined and reviewed. The results can be summarized as follows. 1) Fracture appearance transition temperatures are 80.deg. C at the center part and 60.deg. C near surface of 12% Cr rotor, and 8.deg. C near surface of 1% Cr-Mo-V rotor. 2) Comparative rapid softening occurs at higher temperatures above 600.deg. C for 12% Cr steel and 550.deg. C for 1% Cr-Mo-V steel in tension tests. 3) Fatigue crack propagation rate of 12% Cr steel is almost same as that of 1% Cr-Mo-V steel at the same corresponding surface part of the rotors. The crack growth rate of center part of 12% Cr rotor is faster than near surface part of the rotor, and the crack growth rate at the load condition of R=0.04 is slower than that of the load condition of R=0.5 for both 12% Cr steel and 1% Cr-Mo-V steel. 4) Crack growth rate of radial direction near surface of 12% Cr rotor is faster than that of transverse direction at the same part because of the difference in residual stresses. 5) Both creep and fatigue strengths of 12% Cr steel are superior to those of 1% Cr-Mo-V steel and the difference is thought the effect of climb and glide controlled creep by solid solution of alloying elements and dispersion of carbides.

• 한국해양공학회지
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• 제3권2호
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• pp.625-625
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• 1989

To check technical improvement in the soundness and strength of 12% Cr steel rotor, a 25 tons of rotor with 65 tons of ingot was made in real size and was cut to pieces to take test samples, and the various mechanical tests such as impact, tensile, creep, and fatigue were carried out. The strengths are compared with those of 1% Cr-Mo-V rotor of same size. Microstructures of the samples are examined and reviewed. The results can be summarized as follows. 1) Fracture appearance transition temperatures are 80.deg. C at the center part and 60.deg. C near surface of 12% Cr rotor, and 8.deg. C near surface of 1% Cr-Mo-V rotor. 2) Comparative rapid softening occurs at higher temperatures above 600.deg. C for 12% Cr steel and 550.deg. C for 1% Cr-Mo-V steel in tension tests. 3) Fatigue crack propagation rate of 12% Cr steel is almost same as that of 1% Cr-Mo-V steel at the same corresponding surface part of the rotors. The crack growth rate of center part of 12% Cr rotor is faster than near surface part of the rotor, and the crack growth rate at the load condition of R=0.04 is slower than that of the load condition of R=0.5 for both 12% Cr steel and 1% Cr-Mo-V steel. 4) Crack growth rate of radial direction near surface of 12% Cr rotor is faster than that of transverse direction at the same part because of the difference in residual stresses. 5) Both creep and fatigue strengths of 12% Cr steel are superior to those of 1% Cr-Mo-V steel and the difference is thought the effect of climb and glide controlled creep by solid solution of alloying elements and dispersion of carbides.