• 한국분말야금학회:학술대회논문집
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• 한국분말야금학회 2006년도 Extended Abstracts of 2006 POWDER METALLURGY World Congress Part2
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• pp.1089-1090
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• 2006

Biomimetic apatite deposition behaviors on Zr-1Nb and Ti-6Al-4V plate with various surface conditions were examined. Both alloys were polished with abrasive papers to have different roughness and some of them were treated in NaOH before exposition in simulated body fluid. NaOH treatment was found to enhance the deposition rate of apatite on Ti-6Al-4V significantly. On the other hand, the deposition rate of Zr-1Nb was not influenced by NaOH treatment. Without NaOH treatment, the polished Zr-1Nb with abrasive paper was found to induce more apatite nucleation than the polished Zr-6Al-4V.

• 한국결정성장학회지
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• 제28권5호
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• pp.206-210
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• 2018

에나멜 기법을 활용하여 Ti6Al4V 합금에 두 종류의 생체활성화 유리를 코팅하였다. 재료간의 열팽창계수 차이에 의한 열응력을 줄이기 위해 재료간의 열팽창계수의 차가 $2{\times}10^{-6}/^{\circ}C$ 정도 되도록 생체활성화 유리 조성을 선정하였다. 열팽창계수의 차이에도 불구하고 Ti6Al4V 합금과 코팅 유리간에 확산결합에 의해 양호한 부착이 형성되었음을 FE-SEM과 EDS 분석으로 확인하였다. 의사체액에 담근 후 코팅 표면에 일반적인 생체활성화 유리와 같은 hydroxycarbonate apatite가 형성됨을 FT-IR로부터 확인하였다.

• 한국재료학회지
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• 제9권10호
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• pp.1025-1031
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• 1999

6종류의 조성을 가진 TiAl계 합금, 즉 Ti-(42, 44)Al-2Nb-4V, Ti-(42, 44)Al-4Nb-2V 및 Ti-(42, 44)Al-4Nb-2Cr을 아크용해법으로 제조한 후, 이들의 산화성질을 조사하였다. 700, 800 및 $900^{\circ}C$의 대기 중, 50시간동안의 등온 및 반복 산화실험으로부터, 산화저항은 Ti-(42, 44)Al-2Nb-4V, Ti-(42, 44)Al-4Nb-2V 및 Ti-(42, 44)Al-4Nb-2Cr의 순으로 증가함을 알 수 있었다. 내산화성에서 V은 해로운 원소이고 Cr은 유익한 원소이었다. 산화 중 모든 모재 구성원서는 외부확산하였고 분위기중으로 부터의 산소는 내부확산하는 상호확산이 관찰되었으며, 생성되는 산화물은 최외각 $\textrm{TiO}_2$층, 상부 ($\textrm{TiO}_2+\textrm{Al}_2\textrm{O}_3$) 혼합층 및 하부 $\textrm{TiO}_2$-잉여층으로 이루어진 3층 산화물구조로 구성되어 있었다.

• 한국공작기계학회논문집
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• 제11권2호
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• pp.9-16
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• 2002

The machinability of Ti-6Al-4V titanium alloy and tool wear behavior in machining of Ti-6Al-4V titanium alloy was studied to understand the machining characteristics. This material is one of the strong candidate materials in present and future aerospace or medical applications. Recently, their usage has already been broaden to everybody's commercial applications such as golf heads, finger rings and many decorative items. To anticipate the general use of this material and development of the titanium alloys in domestic facilities, the review and the study of the machining parameters for those alloys are necessary. This study is concentrated to the machining parameters of the Ti-6A1-4V alloy due to their dominant position in the production of titanium alloys.

• 열처리공학회지
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• 제33권3호
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• pp.99-106
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• 2020

Selective laser melting (SLM) is an additive manufacturing process by melting metallic powders and stacking into layers, and can product complex shapes or near-net-shape (NNS) that are difficult to product by conventional processes. Also, SLM process is able to raise the efficiency of production by creating a streamlined manufacturing process. For manufacturing in SLM process using Ti-6Al-4V powder, analysis of microstructural evolution and evaluation of mechanical properties are essential because of rapid melting and solidification process of powders according to high laser power and rapid scan speed. In addition, it requires a post-processing because the soundness and mechanical properties are degraded by defects such as pore, un-melted powder, lack-of-fusion, etc. In this study, hot isostatic press (HIP) was conducted as a post-processing on SLM-printed Ti-6Al-4V alloy. Microstructure of post-processed Ti-6Al-4V alloy was compared to as-built Ti-6Al-4V, and the evolution of quasi-static (Vickers hardness, room temperature tensile characteristic) and dynamic (high-cycle fatigue characteristic) mechanical properties were analyzed.

• 한국기계가공학회지
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• 제21권8호
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• pp.25-31
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• 2022

Recently, investment in the aerospace industry has increased, and titanium alloys have been widely adopted for manufacturing parts in the aerospace industry. The Ti-6Al-4V alloy has high strength in high-temperature and high-pressure environments and is evaluated as a material with excellent heat, corrosion, and abrasion. However, titanium alloys are expensive, difficult to cut, and possess a large cutting load during the drilling process. In this study, the cutting force generated in the drilling process of Ti-6Al-4V alloy was verified via finite element analysis (FEM) and cutting force measurement experiments. A structural analysis was performed based on the cutting analysis data to verify the plastic deformation occurring during the drilling process of cylindrical Ti-6Al-4V alloy aircraft parts. Methods were proposed to predict the amount of deformation that occur during the manufacturing process of titanium-alloy aircraft parts and control the external environment, to minimize the amount of deformation.

• 한국재료학회지
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• 제16권4호
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• pp.264-271
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• 2006

RF sputtering process was applied to produce thin hydroxyapatite(HAp) films on Ti-6Al-4V alloy substrates. The effects of different heat treatment conditions on the chemical composites between HAp thin films and Ti-6Al-4V alloy substrates were studied. After deposition, the HAp thin films were heat treated for 1h at $400^{\circ}C,\;600^{\circ}C\;and\;800^{\circ}C$ under the atmosphere, and analyzed O/M, FESEM-EDX and ESCA, respectively. Experimental results represented that interface of HAp thin films and Ti-6Al-4V alloy substrates was composed Ti-OH, TiO, TiN, $Al_2O_3,\;V_2O_3,\;VO_2$. pyrophosphate and decreased carbide followed by the increase of heat treatment temperature.

• 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.

• 대한용접접합학회:학술대회논문집
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• 대한용접접합학회 1998년도 특별강연 및 추계학술발표 개요집
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• pp.228-230
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• 1998

• 대한용접접합학회:학술대회논문집
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• 대한용접접합학회 2007년 추계학술발표대회 개요집
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• pp.360-362
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• 2007