• Proceedings of the Materials Research Society of Korea Conference
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• 2008.11a
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• pp.38.2-38.2
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• 2008

• Proceedings of the Korean Magnestics Society Conference
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• 1991.11a
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• pp.60-61
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• 1991

• Journal of Powder Materials
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• v.11 no.3
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• pp.193-201
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• 2004

1960년 Au-Si계 합금에서 처음으로 비정질상이 급속 응고법에 의해 보고된 이래/sup 1)/ 지난 40년 간 많은 합금계에서 비정질상이 보고되어졌다. 대표적으로 Fe-, Ni-, Co기 합금 등 많은 합금계에서 비정질상이 보고되었으나, 비정질상의 형성을 위해서는 약 105 K/s이상의 높은 냉각속도를 필요로 하였다. 1980년대 수백 K/s의 낮은 냉각속도 하에서도 비정질상이 형성될 수 있는 다원계 합금(multi-component alloy)이 Mg-Ln-(Ni, Cu, Zn), Ln-Al-TM 합금에서 보고되어 졌으나 많은 관심을 받지 못하다가 1993년 Zr-Ti-Ni-Cu-Be 합금에서 수 ㎝ 크기의 비정질합금 제조가 보고되면서 전 세계적으로 많은 관심을 받게 되었다. Zr-Ti-Ni-Cu-Be계 벌크 비정질 합금이 보고된 후 Zr-(Nb,Pd)-Al-TM, Pd-Cu-Ni-P, Fe-Co-Zr-Mo-W-B, Ti-Zr-Ni-Cu-Sn등 여러 합금계에서 벌크 비정질 합금이 보고되었다. (중략)

• Proceedings of the Korean Magnestics Society Conference
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• 1991.05a
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• pp.87-88
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• 1991

• Journal of the Korean Magnetics Society
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• v.3 no.3
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• pp.190-195
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• 1993

새로운 Fe기 초미세 결정립합금의 제조 가능성 및 자기특성에 관하여 조사하였다. 고포화자화 (Fe.$_{85}$Co.$_{15}$ )$_{80}$B$_{20}$ 비정질합금에서 천이금속을 약 10 at.% Al으로 치환한 (Fe.$_{85}$ Co.$_{15}$ )$_{70}$B$_{20}$Al$_{10}$ 합금은 급속응고에 의하여 비정질 기지내에 직접 .alpha. -Fe(Co)의 석출이 가능하다. 또한 (Fe.$_{85}$Co.$_{15}$ )$_{70}$B$_{20}$Al$_{10}$합금에 2~6 at.% Nb의 첨가는 급속 응고시 결정립성장을 억제하고 포화자왜를 약 6ppm이하로 감소시켜 자기 특성을 개선시킨다. 열처리에 의한 자기 특성은 Nb의 치환량이 증가할 수록 감소한다. 400 .deg. C에서 1시간 열처리한 (Fe.$_{85}$Co.$_{15}$ )$_{70}$ B$_{18}$ Al$_{10}$Nb$_{2}$합금은 평균 약 8nm이하의 .alpha. -Fe(Co) 결정립으로 구성된 초미세 결정립합금 으로 제조가 가능하며, 포화자속밀도, 철손 및 투자율 (f=50 kHz, B$_{m}$ =0.2 T)이 각각 1.2 T, 12W/kg 및 2.5 *$10^{4}$으로 가장 우수하다. 이는 Fe-Si-B-Nb-Cu 초미세결정립합금 및 영자왜 Co기 비정질합금과 거의 같은 자기특성을 나타낸다.다..다.다..낸다.다..

• Journal of Power System Engineering
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• v.5 no.2
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• pp.63-70
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• 2001

To obtain the optimal condition of heat treatment of wear-resistant alloy, hardness and Charpy V-notch test have been performed with Co-based Stellite No.4, No.6 and Tribaloy 800 alloys, following by heat treatment at the various conditions. Heat treatment at $1250^{\circ}C$ for 1 hours caused the as-casted Tribaloy 800 with FCC crystal structure to transform to HCP structure and lamellar eutectic structure was disappeared, which did not influence on the hardness. Aging at $800^{\circ}C$ for 20 hours, following by $1250^{\circ}C$ for 2 hours heat treatment has enhanced hardness significantly, which is due to the precipitation of large amounts of Laves-phase. The hardness of Stellite alloys was increased by the aging at $800^{\circ}C$ to 5 hours, and was nearly constant by the aging over 5 hours. The toughness of Stellite alloys was a few influenced by the aging treatment.

• Korean Journal of Materials Research
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• v.13 no.6
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• pp.381-388
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• 2003

Directional solidification experiments were carried out at 0.5-150 $\mu\textrm{m}$/s in the Co-base superalloy ECY 768. As increasing solidification rate, the dendrite length increased and it reached the maximum at 150 $\mu\textrm{m}$/s, where the tip temperature is close to the liquidus. The liquidus and eutectic temperatures could be estimated by comparing the dendrite lengths and the temperature gradients at the solid/liquid interface and those were estimated as $1424.6^{\circ}C$ and $1343^{\circ}C$ respectively. Between the dendrites just below final freezing temperature, MC carbide and $M_{23}$$C_{6}$ carbide were found. It was confirmed that the script or blocky shape was Ta or W-rich MC carbide, and the lamellar shape was Cr-rich eutectic carbide. The solid/liquid interface morphology clearly showed that the Cr-rich eutectic carbide formed just after the script type MC carbide.

• Korean Journal of Metals and Materials
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• v.47 no.7
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• pp.440-446
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• 2009

Co base superalloys have been widely used for the parts of gas turbine due to their excellent strength, thermal fatigue, oxidation resistance and weldability at high temperature. In this study, directional solidifications were carried out at various solidification rates, including $0.5{\sim}300{\mu}m/s$ in the Co base superalloy FSX-414. The cellular interface were formed at a low solidification rate, $1{\mu}m/s$, and the dendritic interface was found at higher solidification rates, $5{\sim}300{\mu}m/s$. As the spacing of dendrite structure decreased, the size and spacing of eutectics decreased. Dendrite arm spacing decreased with increasing solidification rates and temperature gradient. It was interesting to find the $M_{23}C_{6}$ eutectic microstructure formed between $\gamma$ dendrites. Composition analysis showed that Cr and W were segregated severely between the dendrites, which resulted in the formation of Cr-rich $M_{23}C_{6}$ and W-rich MC carbides.