• Proceedings of the Korean Magnestics Society Conference
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• 2003.06a
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• pp.130-131
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• 2003

The magnetic and thermal properties of NiFe/IrMn/CoFe with Mn additions have been studied. As grown CoFe pinned-layers with IrMn-Mn have dominantly larger exchange biasing field( $H_{ex}$) and blocking temperature( $T_{b}$) than when pure I $r_{22}$M $n_{78}$ is used. The magnetic properties improve, $H_{ex}$ and $T_{b}$ improve with 77-78 vol% Mn, but drop considerably with more Mn additions, losing magnetic properties of theb NiFe/IrMn/CoFe with addition 0.6 vol % Mn. The average x-ray diffraction peak ratios fcc (111)CoFe of (111)IrM $n_3$ textures for the Mn inserted total vol of 75, 77, and 79 vol% were about 1.4, 0.8, and 0.6, respectively. For the sample without Mn inserted layer, the $H_{ex}$ between I $r_{22}$M $n_{78}$ and CoFe layers is almost nothing. For two multilayer as-grown samples with ultra-thin Mn layers of 77 vol % and 79 vol %, the $H_{ex}$s are 250 Oe and 150 Oe, respectively. In case of IrMn with 77.5 vol% Mn, the $H_{ex}$ was 444 Oe up to 30$0^{\circ}C$ endured of 363 Oe at 40$0^{\circ}C$, respectively. Mn additions improve the magnetic properties and thermal stabilities of NiFe/IrMn/CoFe. Those increase the $H_{ex}$ and $T_{b}$. In applications where higher $H_{ex}$ and $T_{b}$ are accept, proper concentrations of Mn can be used.n can be used.be used.

• Proceedings of the Materials Research Society of Korea Conference
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• 2003.03a
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• pp.216-216
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• 2003

현재 상용화되어 있는 리튬 이차전지용 양극재료로는 비교적 작동전압이 높은 층상 암염구조(LiCoO$_2$, LiNiO$_2$) 및 Spinet계(LiMn$_2$O$_4$) 전이금속 산화물이 대부분 이용되고 있다 하지만 LiCoO$_2$나 LiNiO$_2$ 같은 상용화 물질은 비교적 높은 비용과, 강한 독성 때문에 많은 문제점을 가지고 있다. 또 Spinel(LiMn$_2$O$_4$)는 낮은 비용과 환경친화적인 장점에도 불구하고 Jahn-Teller 변형과 관련된 구조적 변형이 심각하기 때문에 사이클시 비가역적인 용량의 감소가 심각하다. 이러한 관점에서 전이금속보다 그 양이 풍부하고 저렴할 뿐만 아니라 독성이 없는 Olivine 구조 (LiFePO$_4$)를 갖는 phosphate계 화합물에 관심을 가지게 되었다. LiFePO$_4$는 리튬 음극과 3.4V의 방전전압을 나타내며, 170mAh/g의 이론용량을 가지고 있어, Fe-base의 장점은 물론 안정적인 결정구조 및 현재 상용화된 재료들과 비슷한 에너지 밀도를 가진다. 따라서 본 연구에서는 양극물질의 기존 두 제조법인 고상반응법과 sol-gel법으로 대표되는 제조법의 단점을 상호 보완될 수 있다고 판단되는 기계적 합금화법(Mechanical Alloying, MA)공정을 도입하여 초미세립 분말 제조에 초점을 맞추어 Olivine phosphate계 양극물질의 제조 및 전기화학적 특성을 연구하였다.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2018.06a
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• pp.132-132
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• 2018

NiTi 형상 기억 합금은 형상기억 효과 (Shape memory effect) 또는 초탄성 효과 (superelasticity effect)를 나타낸다고 알려져 있다. 대표적으로 Ni:Ti 조성비가 1:1을 갖는 NiTi(니티놀) 합금은 형상기억 및 초탄성 효과가 우수하여 기계 가공 공정뿐만 아니라 우수한 내마모성을 요구하는 공구에 사용하기 적합하다. 하지만 NiTi 박막은 합금과 같은 Damping capacity를 가지고 있지만 비교적 낮은 물리적 특성을 가지고 있다. 본 연구에서는 NiTi 박막의 낮은 물리적 특성을 향상시키기 위하여 TiN과 NiTi의 2층형 박막을 제조하고 각 층의 두께 변화를 조절하여 특성 향상에 대한 기초연구를 진행했다. 타겟은 NiTi (Ni:Ti=48.2:51.8 at.%) 합금 타겟과 Ti 타겟을 사용하였고, 시편과 타겟 간의 거리는 약 10cm 이며, 시편은 기초분석을 위한 SUS304, 물리적 특성 평가를 위한 초경 을 사용하였다. 초경은 실제 공구에서 사용하고 있는 Co함량이 10% 함유된 시편은 선정했다. 시편 전처리는 알코올과 아세톤으로 세척을 실시한 후 진공챔버에 장착하고 ${\sim}10^{-5}Torr$ 까지 진공배기를 실시하였다. 기판 정청은 글로우 방전 방식으로 약 800 V 전압에서 30분간 실시했다. 공정 가스는 Ar와 $N_2$ 혼합가스를 사용하였으며, UBM(Un-Balanced Magnetron) 스퍼터링 소스를 이용하여 2층형 박막을 제조했다. TiN과 NiTi 층의 두께 비율을 0.5, 1 그리고 2 로 변화시켜 코팅했으며, 박막의 총 두께는 약 ${\sim}3{\mu}m$ 이다. 기초분석은 FE-SEM을 통해 두께와 박막 비율을 확인 및 XRD 분석을 통해 박막 정성분성을 실시했다. 2층형 박막의 물리적 특성은 Nanoindentation test, AFM 및 ball on disc를 이용하여 평가했으며, 그 결과 두께 비율 변화에 따라 물리적 특성 변화가 나타남을 확인했다.

• Korean Journal of Materials Research
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• v.28 no.10
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• pp.583-589
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• 2018

This study investigates the effect of fatigue stress on the damping capacity in a damaged Fe-22Mn-12Cr-3Ni-2Si-4Co damping alloy under fatigue stress. ${\alpha}^{\prime}$ and ${\varepsilon}-martensite$ forms by fatigue stress in the damaged Fe-22Mn-12Cr-3Ni-2Si4-Co damping alloy under fatigue stress. The ${\alpha}^{\prime}$ and ${\varepsilon}-martensite$ forms with the specific direction and surface relief, or they cross each other. With an increasing fatigue stress, the volume fraction of ${\alpha}^{\prime}-martensite$ and ${\varepsilon}-martensite$ increases. With an increasing fatigue stress, the damping capacity increases with an increase in the volume fraction of ${\varepsilon}-martensite$. The increase in the damping capacity in the damaged Fe-22Mn-12Cr-3Ni-2Si-4Co alloy under fatigue stress strongly affects the increase of ${\varepsilon}-martensite$ formed by fatigue stress, but the damping capacity of the damaged Fe-22Mn-12Cr-3Ni-2Si-4Co damping alloy under fatigue stress is strongly controlled by a large amount of ${\alpha}^{\prime}-martensite$.

• Transactions of Materials Processing
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• v.29 no.3
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• pp.163-171
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• 2020

We present a multi-step cold drawing for a non-equiatomic Co₁₀Cr₁₅Fe₂₅Mn₁₀Ni₃₀V₁₀ high entropy alloy (HEA) with a simple face-centered cubic (FCC) crystal structure. The distribution of strain in the cold-drawn Co₁₀Cr₁₅Fe₂₅Mn₁₀Ni₃₀V₁₀ HEA wires was analyzed by the finite element method (FEM). The effective strain was expected to be higher as it was closer to the surface of the wire. However, the reverse shear strain acted to cause a transition in the shear strain behavior. The critical effective strain at which the shear strain transition behavior is completely shifted was predicted to be 4.75. Severely cold-drawn Co₁₀Cr₁₅Fe₂₅Mn₁₀Ni₃₀V₁₀ HEA wires up to 96% of the maximum cross-sectional reduction ratio were successfully manufactured without breakage. With the assistance of electron back-scattering diffraction and transmission electron microscope analyses, the abundant deformation twins were found in the region of high effective strain, which is a major strengthening mechanism for the cold-drawn Co₁₀Cr₁₅Fe₂₅Mn₁₀Ni₃₀V₁₀ HEA wire.

• Journal of the Korean Society for Heat Treatment
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• v.36 no.3
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• pp.128-136
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• 2023

In this study, the effects of heat treatment on the nano-scale creep behavior of CoCrFeMnNi high-entropy alloy (HEA) processed by high-pressure torsion (HPT) was investigated through nanoindentation technique. Nanoindentation experiments with a Berkovich indenter were performed on HPT-processed alloy subjected to heat treatment at 450℃, revealing that the hardness of the HPT-processed alloy (HPT sample) significantly increased with the heat treatment time. The heat treatment-induced microstructural change in HPT-processed alloy was analyzed using transmission electron microscopy, which showed the nano-sized Cr-, NiMn-, and FeCo-rich phases were formed in the HPT-processed alloy subjected to 10 hours of heat treatment (HPT+10A sample). To compare the creep behavior of HPT and HPT+10A samples, constant load nanoindentation creep experiments were performed using spherical indentation indenters with two different radii. It was revealed that the predominant mechanism for creep highly depended on the applied stress level. At low stress level, both HPT and HPT+10A samples were dominated by Coble creep. At high stress level, however, the mechanism transformed to dislocation creep for HPT sample, but continued to be Coble creep for HPT+10A sample, leading to higher creep resistance in the HPT+10A sample.

• Journal of Powder Materials
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• v.26 no.2
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• pp.112-118
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• 2019

Infiltration is a popular technique used to produce valve seat rings and guides to create dense parts. In order to develop valve seat material with a good thermal conductivity and thermal expansion coefficient, Cu-infiltrated properties of sintered Fe-Co-M(M=Mo,Cr) alloy systems are studied. It is shown that the copper network that forms inside the steel alloy skeleton during infiltration enhances the thermal conductivity and thermal expansion coefficient of the steel alloy composite. The hard phase of the CoMoCr and the network precipitated FeCrC phase are distributed homogeneously as the infiltrated Cu phase increases. The increase in hardness of the alloy composite due to the increase of the Co, Ni, Cr, and Cu contents in Fe matrix by the infiltrated Cu amount increases. Using infiltration, the thermal conductivity and thermal expansion coefficient were increased to 29.5 W/mK and $15.9um/m^{\circ}C$, respectively, for tempered alloy composite.

• Proceedings of the Materials Research Society of Korea Conference
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• 1997.10a
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• pp.173-173
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• 1997

• Korean Journal of Materials Research
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• v.14 no.11
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• pp.813-820
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• 2004

The electrolytic reduction of spent oxide fuel involves the liberation of oxygen in a molten LiCl electrolyte, which is a chemically aggressive environment that is very corrosive for typical structural materials. So, it is essential to choose the optimum material for the process equipment handling molten salt. In this study, corrosion behavior of Haynes 263, 75, and Inconel X-750, 718 in molten salt of $LiCl-Li_{2}O$ under oxidation atmosphere was investigated at $650^{\circ}C\;for\;72\sim360$ hours. At $3\;wt\%\;of\;Li_{2}O$, Haynes 263 alloy showed the highest corrosion resistance among the examined alloys, and up to $8\;wt\%\;of\;Li_{2}O$, Haynes 75 exhibited the highest corrosion resistance. Corrosion products were formed $Li(Ni,Co)O_2,\;LiNiO_2\;and\;LiTiO_2\;and\;Cr_{2}O_3$ on Haynes 263, $Cr_{2}O_3,\;NiFe_{2}O_4,\;LiNiO_2,\;Li_{2}NiFe_{2}O_4,\;Li_{2}Ni_{8}O_10$ and Ni on Haynes 75, $Cr_{2}O_3,\;(Al,Nb,Ti)O_2,\;NiFe_{2}O_4,\;and\;Li_{2}NiFe_{2}O_4$ on Inconel X-750 and $Cr_{2}O_3,\;NiFe_{2}O_4\;and\;CrNbO_4$ on Inconel 718, respectively. Haynes 263 showed local corrosion behavior and Haynes 75, Inconel X-750, 718 showed uniform corrosion behavior.

• Proceedings of the Korean Society of Machine Tool Engineers Conference
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• 2004.04a
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• pp.129-135
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• 2004

This study was to evaluate the effect of carbon content on metallic change and fatigue characteristics with Fe-29% Ni-17% Co, low heat expansion alloy, widely using electronic components, precision machines, and sealing with glass and metal etc. The steels were fabricated with variation of carbon content, 0, 0.03, 0.06, 0.1, and 0.20% with VIM and tensile test and fatigue test were performed to achieve the above purpose. The more carbon content, the higher hardness value and yield strength. But elongation of 0.03%C, 0.06%C, and 0.10%C specimen decreased about 2.2%, 1.5% and 0.8% respectively mote than that of the base metal. Especially the strength and elongation of 0.20%C specimen increased simultaneously about 14.4% and 7.5%. Fatigue life of 0.03%C specimen decreased but the more carbon content, the higher fatigue life over 0.06% carbon content more than that of base metal.