• 대한환경공학회지
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• 제37권6호
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• pp.371-379
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• 2015

본 연구에서는 주로 건축자재에 많이 사용된 백석면과 갈석면을 대상으로 산 및 열처리 과정에 따른 두 석면의 특성변화를 살펴보았다. 연구결과, 산처리 과정에 따른 백석면의 굴절률, 신장부호, 소광특성은 대체로 산처리하지 않은 백석면 초기 특성과 유사하게 나타났지만 pH 1.2의 강한 산성용액에서 8주 경과 후, 미지의 입자가 형성되는 등 백석면 고유의 특성이 소실되었다. 산처리 과정에 따른 백석면 구성성분의 중량비(%)는 규소의 경우, 크게 변하진 않았지만, 산소와 마그네슘의 경우, 중량비(%)가 다소 변동하였다. 갈석면의 경우, 굴절률, 신장부호, 소광특성은 pH 및 경과시간과 상관없이 산처리하지 않은 갈석면과 동일하게 나타났으며, 갈석면 구성성분의 중량비(%)는 철의 경우, 산처리 과정에 따라 다소 증가하는 경향을 보였으며, 산소는 이와 반대로 감소하는 경향을 보였고, 규소와 마그네슘은 산처리 전 후 유사하게 나타났다. 열처리 과정에 따른 백석면 굴절률은 온도가 높아질수록 수평방향, 수직방향의 굴절률이 모두 증가하였으며, 신장부호는 $1,100^{\circ}C$에서 10분간 가열했을 때 (+)에서 (-)로 변하였고, 소광특성은 변하지 않았다. 열처리 과정에 따른 백석면 구성성분의 중량비(%)는 규소의 경우, 중량비(%)는 크게 변하진 않았지만, 산소와 마그네슘의 경우, 온도별 열처리 과정에 따라 중량비(%)가 크게 변동하였다. 갈석면의 경우, 굴절률은 온도가 높아질수록 수평방향, 수직방향 모두 증가하는 경향을 보였으며, 열처리 과정에서 신장부호 및 소광특성은 변하지 않았다. 갈석면 구성성분의 중량비(%)는 산소와 철의 경우, 온도별 열처리 과정에 따라 중량비(%)가 크게 변동하였지만, 규소와 마그네슘은 전반적으로 온도 및 가열시간과 상관없이 열처리하지 않은 갈석면과 유사하게 나타났다.

• 한국산업융합학회 논문집
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• 제6권4호
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• pp.299-305
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• 2003

This research is for the relationship with heat treatment cooling temprature and the characteristic of Mechanical properties of Boron-Addition-Steel, the main material and SM25C steel, the sub material, structure viewing fractography, hardness test, tensite test and are carried out after the manufacturing small-specimen treated with heat of $750^{\circ}C$, $850^{\circ}C$, $1050^{\circ}C$. The influence to the Mechanical properties accompanied by AISI51B20, Boron-Addition-steel shows the following result. 1. The influenc of heat treatment by the content of cabon-steel is dominant. Addition of boron result is Strengthening structure effectively by segregation and improving over all mechanical characters such as good. it results from the increase of temacity by the stability of inter granular with improvement of harden-ability. 2. Boron-Addition-Steel exist in the from of martensite structure accompanied by the ferrite precipitition centering around grain boundary, and is improved to Hv 200. 3. The height of harden-ability and fatigue stress the influence of heat results from crystal structure of martensite by difference of strength level in the structure of ferrite and doesn't have am effect on sensibility of temperature, and turns out to defend on production and growth of Matrix-structure-factor.

• 한국식품조리과학회지
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• 제6권3호통권12호
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• pp.25-32
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• 1990

In this study, the cis to trans isomerization of unsaturated fatty acids were investigated about Soybean oil (SBO), Corn germ oil (CGO), Cottonseed oil (CSO), Margarine (MG), Shortening (ST) incubated at $40{\pm}2^{\circ}C$ for 35 days and heated at $185{\pm}2^{\circ}C$ for 24 hours. The contents and kinds of trans fatty acids in each sample were determined by GLC after seperating by HPLC. The results were obtained as follows; 1. When samples were incubated at $40{\pm}2^{\circ}C$ for 35 days, the contents of total trans fatty acids were increased from $0.5{\sim}12.3%$ to $0.8{\sim}20.5%$. The kinds of trans fatty acids found were $t-C_{18:1},\;t,c-C_{18:2},\;t,t-C_{18:2},\;t,c,c-C_{18:3}$ in $SBO,\;t-C_{18:1},\;t,c-C_{18:2}$ in $CGO,\;t-C_{16:1},\;t-C_{18:1},\;t,c-C_{18:2},\;t,t-C_{18:2}$ in CSO. Processed oil such as MG and ST showed more complicated composition of trans fatty acids than SBO, CGO and CSO. $t-C_{18:1},\;t,c-C_{18:2},\;t,t-C_{18:2},\;t,c,t-C_{18:3},\;t-C_{20:1}$ were detected in ST. 2. In the case of heating at $185{\pm}2^{\circ}C$ for 24 hours, the contents of total trans fatty acid were $1.6{\sim}37%$. 2% in all samples. Heating made more remarkable isomerization than incubation $(40{\pm}2^{\circ}C)$. Specially, $c,c,t-C_{18:3}$ in $SBO,\;t,t,t-C_{18:3}$ in $MG,\;t,c,t-C_{18:3},\;t,t,t-C_{18:3}$ in ST were detected. 3. The total contents of trans fatty acids of processed oil were higher than vegetable oils. During incubation, trans fatty acids increased in the order of MG>ST>CGO>SBO>CSO, and during heat treatment, MG>ST>SBO>CGO>CSO.

• 열처리공학회지
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• 제29권6호
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• pp.259-263
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• 2016

This study was carried out to investigate the effect of hot forging ratio on the microstructure and mechanical properties of incoloy 825 alloy. Hot forging was carried out at the forging ratio of 0%, 60% and 90% respectively in a range of $900^{\circ}C{\sim}1,140^{\circ}C$ and followed solution treatment was conducted at $1,000^{\circ}C$ for 1 hr. In all the specimens of hot forged of 0%, 60% and 90%, precipitates were not observed. The average grain size of 0% specimen is $82{\mu}m$ and that of 60% and 90% is $56{\mu}m$ and $31{\mu}m$, respectively. The range of grain size in the 0% specimen is uneven in $182{\mu}m$ to $31{\mu}m$, but the grain size of 90% specimen is uniform. With increasing hot forging ratio, the mechanical properties such as tensile strength, elongation, hardness increased and impact toughness increased by grain refinement.

• 수산해양기술연구
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• 제14권2호
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• pp.79-87
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• 1978

기관밸브용접 SCr4-21-4N 및 SUH3-21-4N을 연구선정된 최적마찰압접조건 하에서 마찰압접을 하고 이때 생기는 압접부의 잔류응력 및 경도의 peak 등 압접결함의 제거 및 압접성능개선을 위한 열처리에 관하여 실험연구한 결과 다음과 같은 결론을 얻었다. (1) 배기 valve용강 SCr4-21-4N 및 SUH3-21-4N의 마찰압접을 위한 최적조건으로서 회전수 3,000rpm, 마찰가열압 p 하(1)=8 kg/mm 상(2), upset 압 p 하(2)=20 kg/mm 상(2), 압접가열시간 t 하(1)=3초, upset 시간 2.5초를 선정한 것이 매우 타당함이 실험적으로 입증되었다. (2) 이종재질 SUH3-SUH31, SCr4-SUH31, SCr4-SUH3, SUH3-CRK22, SCr4-21-4N 및 SUH3-21-4N의 마찰압접에 관한 저자의 종래 연구와 본연구 결과는 압접부의 압접 특성이 서로 매우 일치하였다. (3) SCr4-21-4N 및 SUH3-21-4N의 마찰압접부의 잔류응력 및 전도의 peak를 제거하기 위한 최적열처리조건은 $600^{\circ}C$$\times$30min.$\times$room air cooling의 normalizing임이 확인되었다. (4) 이때 열처리 후에는, 열처리전의 인장강도의 약 20%가 감소했으나, 파단 위치는 열영향부로부터 모재 SCr4 및 SUH3 측으로 이동하였다. (5) 상기 최적조건 하에서 마찰압접되고 열처리된 압접부의 현미경 조직검사 결과, 압접부가 매우 좁고 압접결함이 없으며, 치밀하고 조밀한 조직의 우수한 압접이었음이 확인되었다. (6) 상기 최적조건은, 기관 valve 생산을 위한 타이종재질의 마찰압접조건으로도 응용될 수 있을 것이다.

• 한국분말재료학회지
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• 제6권2호
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• pp.171-177
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• 1999

Ti-45.2at.%Ni-5at.%Cu and Ti-40.2at.%Ni-10atat.%Cu alloy powders were fabricated by gas atomization process. The microstructures, Shape, hardness and phase transformation behaviors of the powders were investigated by means of optical microscopy, scanning electron microscopy, micro-hardness measurement, x-ray diffraction analyses and differential scanning calorimetry. The hardness of the Ti-Ni-XCu alloy powders decreased as Cu-content increased. The x-ray diffraction analyses were carried out for powders without heat treatment, and those that treated at 85$0^{\circ}C$ for an hour in a vaccum state($10^5$ torr) and then quenched into ice water. The intensity of B$19^t$ phase increased with heat treating. The monoclinic B$19^t$ martensite was formed in the Ti-Ni-XCu alloy powders during cooling.

• 열처리공학회지
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• 제20권5호
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• pp.243-249
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• 2007

The age hardening behavior and mechanical properties of an extruded Al-Zn-Mg-(Cu)-0.1 wt.%Sc alloy were investigated with the Sc addition and ageing temperature. The results showed that the $Al_3Sc$ compounds were formed by Sc addition and distributed preferentially along the extrusion direction. The age hardening of Al-Zn-Mg-Cu-0.1 wt.%Sc alloy which was treated by T6 process was more significant than that of Al-Zn-Mg-0.1 wt.%Sc alloy. The tensile property of Al-Zn-Mg-Cu+0.1 wt.%Sc alloy was also higher than that of Al-Zn-Mg-0.1 wt.%Sc alloy, which is 691 MPa and 584 MPa in strength and 9% and 11% in elongation, respectively.

• The Korean Journal of Ceramics
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• 제6권1호
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• pp.9-14
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• 2000

Glass transition temperature (T/sub g/) is proportional to the quadrupole splitting(Δ) of Fe(III) obtained from the /sup 57/Fe Mossbauer spectra (T/sub g/-Δ rule (1990)). The values of Δ reflect the distortion of Fe(III) atoms, which occupy the sites of network-forming atoms. Heat treatment of potassium vanadate and calcium gallate glasses at around the individual T/sub g/ causes a structural relaxation, accompanying a linear decrease of T/sub g/ and Δ values. These experimental results prove that T/sub g/ decreases with a decrease in the distortion of VO₄, GaO₄, and FeO₄tetrahedra, as the T/sub g/-Δ rule predicted.

• 열처리공학회지
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• 제15권4호
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• pp.172-177
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• 2002

The steady-static creep behaviors of Ti-6Al-4V alloy, using the constant stress creep tester, were investigated over the temperature range of $510{\sim}550^{\circ}C$(0.42~0.44Tm) and the stress range of 200~275 MPa($20.41{\sim}28.06kg/mm^2$). The stress exponents(n) for the static creep deformation of this alloy were 9.85, 9.35, 9.24 and 8.85 at the temperature of 510, 525, 535 and $550^{\circ}C$, respectively. The stress exponent(n) decreased with increasing the temperature and became close to about 5. The apparent activation energies(Q) for the static creep deformation were 254.4, 241.8, 234.4 and 221.9 kJ/mole for the stress of 200, 225, 250 and 275MPa, respectively. The activation energy(Q) decreased with increasing the stress. From the above results, it can be concluded that the static creep deformation for Ti-6Al-4V alloy was controlled by the dislocation climb over the ranges of the experimental conditions. Larson-Miller Parameter(P) for the crept specimens of Ti-6Al-4V alloy under the static creep conditions was obtained as $P=(T+460)({\log}\;t_r+21)$. The failure plane observed by SEM showed up dimple phenomenon at all range.

• 열처리공학회지
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• 제18권3호
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• pp.177-182
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• 2005

The steady state cyclic mechanism, and the behaviour of Nicoseal(Fe-29Ni-17Co) have been examined under the condition of square wave stress cyclic tension creep test at the temperature, stress and frequency range of $430{\sim}470^{\circ}C$($0.41{\sim}0.43T_m$), 353~383 MPa, and 3 cpm, respectively. Also, the relationship between cyclic creep and static creep have been examined. The stress exponents(n) for the static creep deformation of this alloy were 11.6, 10.0, 8.4 and 7.9 at the temperature of 430, 445, 460 and $470^{\circ}C$, respectively. The apparent activation energies (Q) for the static creep deformation were 54.2, 51.8, 49.7 and 46.8 kcal/mole for the stress of 353, 363, 373 and 383 MPa, From the above results, it could be considered that the cyclic creep accelaration phenomena was obtained and that the cyclic deformation for Nicoseal seemed to be controlled by dislocation climb over the range of experimental conditions. Nicoseal alloy under the cyclic creep conditions was obtained as P=(T+460)(logt+17). The failure plane observed by SEM showed up transgranular fracture at all range.