• 전기화학회지
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• 제8권3호
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• pp.125-129
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• 2005

본 연구에서는 고순도 알루미늄 호일$(t=300{\mu}m)$양극산화 공정을 통해 AAO 나노템플레이트를 자체 제조하였고, 이렇게 제조된 형틀을 가지고 교류 나노전주법에 의해 경자성 합금인 CoP와 연자성 합금인 CoFe를 나노와이어로 제조하였다. 대표적인 Co계 자성합금인 CoP와 CoFe나노와이어는 각기 독특한 자기적 성질을 나타내었다. 경자성 CoP 합금 나노와이어의 경우 교류 인가전압에 따라 hcp와 fcc가 혼재된 구조가 형성되어 자기적 특성에 영향을 미쳤다. 또한 높은 포화자화 값을 갖는 CoFe연자성 합금 나노와이어는 박막 도금 시와는 달리 이상합금도금현상이 거의 나타나지 않았으며 $Co_{30}Fe_{70}$에서 가장 좋은 238emu/g의 포화자화 값을 나타내었다.

• 전기화학회지
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• 제6권2호
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• pp.145-152
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• 2003

전해 캐패시터와 supercapacitor의 특성을 함께 가지는 하이브리드 캐패시터의 용량은 표면이 산화물로 피복된 양극에 의해서 좌우된다 본 연구에서는 고전압 하이브리드 슈퍼캐패시터의 제조를 위해 양극의 용량 최적화를 수행하였다. $40{\mu}m$의 입자경을 갖는 알루미늄 분말과 NaCl분말을 4:1의 무게비로 혼합하여 디스크 형태의 전극을 만들고 열처리를 하였다. 열처리 후 $50^{\circ}C$의 증류수에서 NaCl을 용해시켜 열처리 온도에 따른 용량과 저항을 비교하였다. 최적의 열처리 과정을 거친 후 electropolishing 및 화학처리, 1차 및 2차 에칭을 단계별로 행하였고 각각의 단계에서 최적의 조건을 조사하였다 각각의 단계에서의 용량과 저항은 ac impedance analyzer를 사용하여 측정하였으며 전극의 표면은 SEM을 이용하여 관찰하였다. 2차 에칭 후 내전압이 300V급인 전극으로 만들기 위하여 365V로 양극산화 시켰으며, 산화된 알루미늄 디스크 전극을 사용하여 단위 셀을 제조하여 주파수에 따른 용량과 저항 특성을 기존의 300V급 알루미늄 전해 캐패시터와 비교하였다.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2008년도 춘계학술대회 논문집
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• pp.1-4
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• 2008

Fuel cells have the potential of providing several times higher energy storage densities than those possible using current state-of-the-art lithium-ion batteries, but current energy density of fuel cell system is not better than that of lithium-ion batteries. To achieve the high energy density, volume and weight of fuel cell system need to be reduced by miniaturizing system components such as stack, fuel tank, and balance-of-plant. In this paper, the thin flexible PCB (Printed circuit board) is used as a current collector to reduce the stack volume. Two end plates are made from light weight aluminum alloy plate. The plate surface is wholly oxidized through the anodizing treatment for electrical insulation. The opening rate of cathode plate hole is optimized through unit cell performance measurement of various opening rates. The performances are measured at room temperature and ambient pressure condition without any repulsive air supply. The active area of MEA is 10.08 $cm^2$ and active area per a unit cell is 1.68 $cm^2$. The peak power density is about 210 mW/$cm^2$ and the air-breathing planar stack of 2 Wis achieved as a small volume of 18 cc.

• 한국재료학회지
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• 제12권2호
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• pp.121-128
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• 2002

Anodic alumina layer can be used as templates for preparation of nano-structured materials, because porous oxide layer on aluminum shows a uniform pore size and a high pore density. In order to find out possibility for template material to prepare nano wire, the effects of the anodic applied potential, anodic time and the temperature of electrolyte on pore diameter of anodic alumina layer were studied using SEM and AFM. The pore diameter of anodic alumina layer increased with applied anodic potential and electrolytic temperature. Especially, the pore diameter of anodic oxide layers formed in chromic acid can be well replicated by widening process in $H_3$$PO_4$solution.

• 한국표면공학회지
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• 제23권1호
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• pp.34-43
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• 1990

Al-Si piston alloys such as AlS10CuMg have been anodized to examine apossibility of forming a hard film aat relatively higher temperatures compard with those in conventional sulfuric acid processes. Three types of electrolytes have been employed in this study ; electrolyte A(15% H2SO4, $0^{\circ}C$), electrolyte B(12% H2SO4, 1% oxalic, $10^{\circ}C$), electrolyte C(tartaric acid 125g/L+oxalic 75g/L+aluminum sulfate 225g/L, $25^{\circ}C$). Hard anodisine process in electrolyte B at a current density of 1.54A/dm2 produced a harder film of VHN 396 at a relatibely low film forming voltage compared with those obtained in other electrolyte at equivalent current density. A liner relationship between hardness and abrasion resistance exists for Al-Si piston alloys. The hardness of anodized film decreasees with increasing silicon content in Al-Si alloys and also with bath temperature. The film hardeness of Na-modified alloy os higher than that of P-modified alloy due to its finer microstructre. The film on the silicon phase in Al-Si alloys is observed to be formed by lateral growth of oxide film nucleated at surroundings.

• 반도체디스플레이기술학회지
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• 제17권4호
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• pp.11-15
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• 2018

The parts of equipment for semiconductor are protected by anodic aluminum oxide film to prevent corrosion. This study investigated contamination particle and cracking behavior of anodic oxidation in sulfuric acid containing cerium salt. The insulating properties of the sample were evaluated by measuring the breakdown voltage. It was confirmed that the breakdown voltage was about 50% higher when the cerium salt was added, and that the breakdown voltage after the heat treatment was 55% and 35% higher at $300^{\circ}C$ and $400^{\circ}C$, respectively. After heating at $300^{\circ}C$ and $400^{\circ}C$, cracks were observed in non cerium and cerium 3mM, and more cracks occur at $400^{\circ}C$ than at $30^{\circ}C$. The amount of contamination particles generated in the plasma is about 45% less than that of non-cerium specimens.

• 한국진공학회:학술대회논문집
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• 한국진공학회 2016년도 제50회 동계 정기학술대회 초록집
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• pp.429-429
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• 2016

Organolead halide perovskite have attracted much attention over the past three years as the third generation photovoltaic due to simple fabrication process via solution process and their great photovoltaic properties. Many structures such as mesoporous scaffold, planar heterojunction or 1-D TiO2 or ZnO nanorod array structures have been studied to enhance performances. And the photovoltaic performances and carrier transport properties were studied depending on the cell structures and shape of perovskite film. For example, the perovskite cell based on TiO2/ZnO nanorod electron transport materials showed higher electron mobility than the mesoporous structured semiconductor layer due to 1-D direct pathway for electron transport. However, the reason for enhanced performance was not fully understood whether either the shape of perovskite or the structure of TiO2/ZnO nanorod scaffold play a dominant role. In this regard, for a clear understanding of the shape/structure of perovskite layer, we applied anodized aluminum oxide material which is good candidate as the inactive scaffold that does not influence the charge transport. We fabricated vertical one dimensional (1-D) nanostructured methylammonium lead mixed halide perovskite (CH3NH3PbI3-xClx) solar cell by infiltrating perovskite in the pore of anodized aluminum oxide (AAO). AAO template, one of the common nanostructured materials with one dimensional pore and controllable pore diameters, was successfully fabricated by anodizing and widening of the thermally evaporated Al film on the compact TiO2 layer. Using AAO as a scaffold for perovskite, we obtained 1-D shaped perovskite absorber, and over 15% photo conversion efficiency was obtained. I-V measurement, photoluminescence, impedance, and time-limited current collection were performed to determine vertically arrayed 1-D perovskite solar cells shaped in comparison with planar heterojunction and mesoporous alumina structured solar cells. Our findings lead to reveal the influence of the shape of perovskite layer on photoelectrical properties.

• 전기화학회지
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• 제12권1호
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• pp.47-53
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• 2009

본 연구에서는 불순물이 포함된 Al 기판으로부터 두 단계의 양극산화 (anodization) 법에 의해 균일한 나노기공을 갖는 AAO(Anodic Aluminum Oxide)을 제조하였다. 생성된 AAO템플릿 위에 Deposition-Precipitation(DP)방법을 사용하여 수직으로 형성된 $TiO_2$ 나노섬유에 Au를 첨가시켜 2 wt.% $Au/TiO_2$ 나노섬유룰 제조하였다. 두 단계의 양극산화를 통해 규칙적으로 배열된 AAO 기공 형상과 기판 위에 수직으로 배향된 $TiO_2$ 나노섬유의 형상을 SEM을 통해 확인하였다. 또한 $Au/TiO_2$ 나노섬유의 특성은 XRD와 Raman 분석을 통하여 $TiO_2$의 아나타제(anatase)와 루타일(rutile) 결정구조와 $TiO_2$ 나노섬유에 담지된 Au의 존재를 확인하였다. 또한 일산화탄소(CO) 산화반응을 통해 AAO(Anodic Aluminum Oxide)기판 위에 형성된 $TiO_2$와 2 wt% $Au/TiO_2$ 나노섬유의 광촉매적 활성을 비교하였다.

• Corrosion Science and Technology
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• 제6권6호
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• pp.275-281
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• 2007

The effect of annealing on the pitting corrosion resistance of anodized Al-Mg alloy (AA5052) processed by equal-channel angular pressing (ECAP) was investigated by electrochemical techniques in a solution containing 0.2 mol/L of $AlCl_3$ and also by surface analysis. The Al-Mg alloy was annealed at a fixed temperature between 473 and 573 K for 120 min in air after ECAP. Anodizing was conducted for 40 min at $100-400A/m^2$ at 293 K in a solution containing 1.53 mol/L of $H_2SO_4$ and 0.0185 mol/L of $Al_2(SO_4)_3$. The internal stress generated in anodic oxide films during anodization was measured with a strain gauge to clarify the effect of ECAP on the pitting corrosion resistance of anodized Al-Mg alloy. The time required to initiate the pitting corrosion of anodized Al-Mg alloy was shorter in samples subjected to ECAP, indicating that ECAP decreased the pitting corrosion resistance. However, the pitting corrosion resistance was greatly improved by annealing after ECAP. The time required to initiate pitting corrosion increased with increasing annealing temperature. The strain gauge attached to Al-Mg alloy revealed that the internal stress present in the anodic oxide films was compressive stress, and that the stress was larger with ECAP than without. The compressive internal stress gradually decreased with increasing annealing temperature. Scanning electron microscopy showed that cracks occurred in the anodic oxide film on Al-Mg alloy during initial corrosion and that the cracks were larger with ECAP than without. The ECAP process of severe plastic deformation produces large internal stresses in the Al-Mg alloy; the stresses remain in the anodic oxide films, increasingthe likelihood of cracks. It is assumed that the pitting corrosion is promoted by these cracks as a result of the higher internal stress resulting from ECAP. The improvement in the pitting corrosion resistance of anodized AlMg alloy as a result of annealing appears to be attributable to a decrease in the internal stresses in anodic oxide films

• Composites Research
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• 제13권4호
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• pp.42-53
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• 2000

차세대 항공기소재로 관심을 가지고 있는 Al 7075/CFRP 적층 복합재인 CARALL(CARbon ALuminum Laminates)하이브리드 복합소재 제조를 위한 중요조건중의 하나인 Al 표면처리조건과 경화방법에 대해 조사하였다. 항공기용 Al 전처리 중 대표적인 것으로 증기탈지, 크롬산 양극산화 피막처리, 황산-중크롬산 나트륨 에칭처리 및 인산 양극산화 피막처리공정이 있다. 본 실험에서는 상기 전처리 공정을 모두 항공 규격에 준해서 실시하여 Lap shear 및 Bell peel strength를 비교함으로써 효과적인 접착강도를 나타내는 표면처리 공정을 찾아내고, 시편의 자연표면상태를 그대로 관찰할 수 있는 AFM(Atomic Force Microscope)장비를 이용하여 각 전처리 시편의 표면형상을 측정함으로써 표면형상과 접착강도와의 상관관계를 고찰 하였다. 그리고 Al 표면처리와 별도로 Al과 접착제 및 탄소섬유 프리프레그를 동시에 경화시키는 방법과 탄소섬유 프리프레그를 미리 경화시킨후 다시 Al과 탄소섬유 라미네이트를 접착필름을 이용하여 재 접착시키는 이차 경화법을 적용하여 상호 접착강도 및 물성을 비교하였다. 또한 이차경화법에서의 오토클레이브 압력 변화와 DMA(Dynamic Mechanical Analysis) 장비를 이용한 접착필름의 유리전이온도($T_g$) 측정을 통해 효과적인 공정압력 및 접착내구성 유지에 필요한 최소 경화시간을 파악하였다. 상기 결과로부터 정밀 치수관리가 필요하며 고접착강도, 내구성 항공기 부품을 제작하기 위한 알루미늄 표면처리 공정과 복합재 경화공정 조건을 제시하고자 하였다.