• Proceedings of the Korean Vacuum Society Conference
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• 2013.02a
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• pp.137-137
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• 2013

지속 가능한 발전을 위해, 한정된 자원인 석유의 고갈을 막기 위해 석유를 수송에너지로 주로 사용하는 자동차에서 바이오 디젤이나 연료전지, 전기자동차 등 다양한 대안이 제시되고 있다. 그러나 식량 가격 상승, 낮은 안정성, 인프라 확충 등의 문제의 해결이 필요할 뿐만 아니라, 석유의 소비를 감소시키는 대신, 지구에서 소비할 수 있는 다른 형태의 에너지를 소모한다는 측면에서 근본적인 에너지 문제의 해결책의 모색이 필요하다. 19세기 후반, 백열전구의 필라멘트 용도로 사용되기 시작한 탄소 섬유는, 철에 비해 5배 가볍고 강도는 10배가 높으며 내열성이 뛰어난 소재로서, 복합소재의 형태로 제조되어 비행기, 우주선, 풍력 발전 블레이드 등 다양한 산업 분야에서 소재의 장점을 발휘하는 재료로 적용 분야가 확대되고 있다. 특히 비행기 분야에서는 최근 비행기 몸체 구조에 기존 알루미늄 합금을 탄소섬유복합재가 대체하고 있으며, 최근에는 부피 기준 50% 가량까지 탄소섬유 복합재를 사용하여 비행기를 제작하고 있다. 이에 따라 기존에 비해 20% 가량 연료 소모가 감소하여, 비행기 한 대 당 연간 2,700톤의 이산화탄소 배출을 저감하고 있다. 이와 같이 탄소섬유 복합재를 다양한 분야에 적용함으로써, 에너지 문제에 대한 보다 근본적인 접근이 가능하다. 그러나 탄소섬유 복합소재는 금속 등 기존 재료에 비해 높은 가격으로 상용 자동차 등 에너지 소비량이 많은 분야에 널리 적용되는데 한계가 존재한다. 이와 같이 높은 탄소섬유의 가격은, 원가의 50% 가량을 차지하는 PAN 원사 가격과 나머지 반절에 해당하는 안정화/탄화 공정 비용에서 기인하는 것으로, 미국의 ORNL (Oak Ridge National Laboratory), 한국의 KIST 복합소재연구소 등에서는 원사, 안정화 공정, 탄화 공정 등 다양한 측면에서 탄소섬유 복합재의 가격을 절감할 수 있는 방안을 연구 중이다. 미국 ORNL에서는 마이크로웨이브 플라즈마를 이용하여 기존에 열을 이용해 수행하던 탄화 공정 비용을 크게 절감하고 있으며, KIST에서는 대기압 플라즈마를 이용하여 기존에 열을 이용해 2시간 가량이 소요되는 안정화 공정을, 대기압 플라즈마를 이용하여 30분여로 단축된 시간에 수행하는 공정을 개발 중이다. 본 발표에서는 탄소섬유 복합재의 개요와, 탄소섬유 가격 절감 방안으로서의 플라즈마에 대해 논의하며 대기압 플라즈마의 다양한 응용에 대해 소개할 예정이다.

• 유체기계공업학회:학술대회논문집
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• 2006.08a
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• pp.531-534
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• 2006

This study is concerned with radial turbine design and performance improvement of a turbo generator system, which is used for maximizing performance of a 250kW MCFC fuel cell system. A preliminary design of a radial turbine has been performed under the thermodynamic and fluid-dynamic conditions determined by a cycle analysis of the MCFC BOP system. Basic demensions are determined by a meanline analysis and calculation of radial variation at the exit of the turbine. The turbine impeller is designed and modified by iterative processes of three dimensional flow analysis.

• Journal of Sensor Science and Technology
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• v.9 no.5
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• pp.380-388
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• 2000

The finite element analysis of a micro turbine was made to investigate safety margin of its operating condition for the high aspect ratio nickel micro turbine blades fabricated by conventional LIGA-like method. From our study, we found that the fabricated turbine could not exceed its yield strength even if the pressure difference between inlet and outlet of turbine blade was about 44kPa, and the correlation of friction coefficient and the maximum stress, caused by contact friction between outer diameter of shaft and inner diameter of turbine blade, was somewhat reciprocal. The maximum stress was decreased with the increasing contact friction, when turbine blade was in its state of rotation. By the results of our study, we conclude that it is possible to fabricate metal micro turbine more easily han surface micromachining technology and to operate with no risk of metal structure's damage, which is caused by yield strength, if the operating condition with the design of micro turbine itself are optimized. It is useful to adopt other applications which have the contact problems between a moving part and the fixed one in micro structures.

• Journal of the Korean Academy of Esthetic Dentistry
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• v.29 no.2
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• pp.84-91
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• 2020

Regeneration of interdental papilla damaged by periodontal disease is a very challenging task. So far, many dentists have devised and introduced great surgical methods. Comparing the pros and cons of the methods introduced so far, I came up with the best way to regenerate interdental papilla. Temporarily creating space between narrow interdental papilla, which cannot be solved by periodontal surgery alone, was a great help for connective tissue graft(CTG). The CTG was performed using a microblade, and only one vertical incision was performed off the gingival margin, and the graft was performed by inserting the grafts through here. Along with the orthodontic treatment, the area between the narrow interdental papilla was widened to make it easier for the CTG was carried out. After a period of maintenance, I was able to gather the teeth again with orthodontic force and regenerate the interdental papilla. I named this method ELSA (Enlargement of space-Labial graft-Squeezing-for Augmentation of papilla) technique.

• Composites Research
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• v.33 no.5
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• pp.275-281
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• 2020

The mechanical property related to lap shear strength of the joint structure between carbon fiber reinforced polymer (CFRP) composite and metal (Ni-Cr Alloy) under varying environmental conditions (temperature and humidity) was studied in order to apply to the aircraft fan blade. Room temperature dry (RTD), elevated temperature wet (ETW), and cold temperature dry (CTD) environmental conditions were chosen for investigation based on the flight conditions of aircraft. Lap shear strength tests were conducted according to ASTM Standard D3528 to evaluate the shear strength. The microstructure characteristic of failure zone was analyzed by SEM images to check the adhesive shear strength with the three environmental conditions. In comparison with shear strength for the RTD condition, the shear strength in the ETW condition was reduced by 72.8% while those for the CTD condition increased by 56.5%. The moisture absorption and high temperature in ETW condition strongly had an affect on mechanical property of adhesive, while cold temperature could enhance the adhesive shear strength due to the higher brittleness.

• Journal of Korea Foundry Society
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• v.41 no.2
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• pp.127-131
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• 2021

Based on its good compatibility with high-temperature environments, the Ti-48Al-2Cr-2Nb alloy is used for high-temperature materials of industrial equipment. In this study, a Ti-48Al-2Cr-2Nb alloy turbocharger turbine wheel was fabricated by a vacuum centrifugal casting method. The conditions that prevent misrun defects of the turbocharger turbine wheel blade from centrifugal casting using alumina molds were investigated. The microstructure of the alloy prepared by vacuum centrifugal casting was studied by means of optical microscopy (OM), with a micro-Vickers hardness analyzer (HV), by X-ray diffraction (XRD) and by SEM-EDS. The HV and SEM-EDS examinations of the as-cast Ti-48Al-2Cr-2Nb alloy showed that the thickness of the oxide layer (α-case) was typically less than 50 ㎛. At a high preheating temperature of 1,100℃, a moderate RPM of 260, and with an alumina mold with a large gate size, there were almost no misrun defects. Therefore, it was confirmed that a Ti-48Al-2Cr-2Nb alloy turbocharger turbine wheel with fewer misrun defects could be achieved through a high preheating temperature, a moderate RPM, a large gate size and an alumina mold to suppress the formation of alpha-case components.