SiO2 기판과 dimethylethylamine alane(DMEAA)을 반응소스로 하여 알루미늄을 증착시켜 증착전 전처리 가스 종류와 수소 플라즈마 처리에 따른 증착속도의 차이와 미세구조에 대하여 연구하였다. TiN기판에 증착된 알루미늄의 증착속도는 증착전 수소 가스에 의한 전처리한 경우 아르곤이나 헬륨에 의한 전처리에 비해 빠른 증착속도를 나타내었다. 이르곤 플라즈마 전처리나 플라즈마 전처리 하지 않고 SiO2기판에 알루미늄을 증착하였을 경우에 비해 수소 플라즈마 전처리에 의해 알루미튬증착시 잠복기(incubation time)가 감소하였으며 치밀한 미세조직을 얻을 수 있었다.

카올린을 용해시킨 황산용액을 에탄올에 주입함으로써 알루미늄황산염의 침전물, AI2(SO4)3·18H2O을 제조하고, 그것의 열분해거동을 검토하였다. 합성된 고순도의 침전물은 약 2μm크기의 판상형태의 입자들로 구성되어져 있었다. 에탄올속으로 카올린을 용해시킨 황산용액의 주입속도를 증가시킴에 따라서 생성된 침전물의 결정사 크기는 감소하였다. 침전물의 탄수 및 탄황산에 대한 겉보기 활성화에너지는 각각 11.9Kcal mol-1 과 48.2kcal mol-1 이었다.

Low foaming acidic degreasing agent(LFADAs) were prepared by blending sorbitol, n-octanoic acid, MJU-100A, Tetronix T-701, Na-dioctyl sulfosuccinate, Demol C, and phosphoric acid. The physical properties of LFADAs tested with aluminum specimen showed the following results ; when 3wt% LFADA-6 was performed at 70℃, the degreasing rate was 95% which is comparitively good, and the percentage of etching was 0.275% which was found to be less than that of commercialized product. When 20wt% of LFADA-6 was added at 65℃, the percentage of derusting was 92% and the good defoaming effect proved by following low foaming power tests respectively : Ross and Miles, and Ross and Clark methods.

Joining of AIN ceramics to W and Cu by active-metal brazing method was tried with use of (Ag-Cu)-Ti alloy as insert-metal. Joints were produced under various conditions of temperature, holding time and Ti-content in (Ag-Cu) alloy Reaction and microstructural development in bonded interface were investigated through observation and analysis by SEM/EDS, EPMA and XRD. Joint strengths were measured by shear test. Bonded interface consists of two layers: an insert-metal layer of eutectic Ag- and Cu-rich phases and a reaction layer of TiN. Thickness of reaction layer increases with bonding temperature, holding time and Ti-content of insert-metal. It was confirmed that the growth of reaction layer is a diffusion-controlled process. Activation energy for this process was 260 KJ/mol which is lower than that for N diffusion in TiN. Maximum shear strength of 108 MPa and 72 MPa were obtained for AIN/W and AIN/Cu joints, respectively. Relationship between processing variables, joint strength and thickness of reaction layer was also explained.

A series of test were undertaken in order to estabilish the effect of different milling variables on dimension and quality of aluminium flake powder. Milling conditions such as initial powder size, milling container rotation speed, milling time, and ball size were varied to produce aluminium flake powder. Flake powder could then be obtained with size range from 15 m to 40 m with a maximum specific surface area of 5 /g by controlling milling conditions. Diameter of milled powders with different milling container rotation speed and ball size were compared with that obtained from theoretical model. The best flake powder was obtained in milling condition of initial powder with average size of 19 m, mill container rotation speed of 80 rpm, balls of 9.5 mm diameter, and milling time of 40 hours.

p-type(100) 실리콘 기판과 TiN(50nm)/Si 기판에 dimethylethylamine alane(DMEAA)을 반응소스로 하여 알루미늄을 증착시켜 증착온도와 유량, 반송가스 종류에 따른 방향성, 증착속도, 미세구조 변화에 대해 연구하였다. 알루미늄의 증착속도는 기판온도, 반송가스 종류 및 유량에 따라 100-650mn/min으로 다양하게 조절되었다. DMEAA의 증착 활성화에너지는 TiN 기판에서는 약 0.leV이었고 Si와 SiO2 기판에서는 각각 약 0.23eV, 0.24eV이었다. 알루미늄 박막의 방향성은 증착속도의 감소에 따라 (200)에서 (111)방향으로 변하였다. 증착된 알루미늄 박막의 불순물 함량은 산소의 경우 0.2at%, 탄소의 경우 1.8at.%이었다. DMEAA 소스에 의한 알루미늄의 증착속도는 반송가스가 Ar 일 때 보다 H2 가스를 사용하면 증착속도가 크게 증가하였으며 이는 반송가스에 의해 SiO2표면의 흡착 H 농도가 증가하고 흡착 H가 소스 가스와 반응하여 핵생성 site 로 작용하는 것으로 생각된다. 알루미늄 박막의 비저항은 표면 미세조직에 크게 영향을 받으며 그 값은 약 3-7μΩcm이었다.

분말야금법으로 제조된 A6061기 입자분산강화 복합재의 열간압술가공에 있어서 압출특성에 미치는 강화입자의 종류, 빌렛특성 및 암술조건의 영향에 대하여 조사하였다. A6061기 복합재료의 열간 압술 전단 변형저항에 미치는 강화입자종류의 영향은 Si Cw > A12 O3f > A12 O3f > Si Cp의 순으로 되었으며, 모든 강화입자에서 부피분율이 증가함에 따라서 Kw값도 증가하였다. 압출조건, 강화입자의 첨가량 및 첨가입자의 평균입도에 관계없이 A12 O3p가 첨가된 복합재의 열간압출가공에 필요한 소요압력은 Si Cp의 경우보다 컸다. 압출압력은 압출 다이스 반각이 커질수록 감소하는 경향은 나타났다. 이것은 다이스 반각에 의해 생성되는 빌렛과의 접촉면적이 증가하여 전단마찰응력(m k3)이 상승하기 때문이다. 압출시 압출온도 상승은 저온에서 ~50˚C 정도 증가하였으며, 압출온도가 500˚C 이상이 되면 압출재 표면에 극심한 tearing이 발생하였다. 강화입자의 첨가량이 증가할수록 이 현상은 더 심하게 되었다.게 되었다.

Several kinds of coagulants such as aluminum sulfate, PAC, PASS are being used to treat drinking water resulting in residual aluminum ions in the water. Recently, it has been reported that high intake of aluminum ion may cause neurological dieseases such as Alzheimer's diesease and presenile dementia. Because of the possible adverse effect, WHO and EEC recommand to regulate residual aluminum. The autorities in Korea also has plan of regulating residual alunimum from 1995. But there is not enough information about the range of residual aluminum ion concentration when the aluminum sulfate, PAC or PASS has been used as a coagulant. Therefore the study has been conducted to find out the range of residual aluminum ion concentration after using aluminum sulfate, PAC, and PASS. Furthermore the effect of turbidity and alkalinity have been investigated. The experimental results are summarized as; 1. Most of the residual aluminum ion concentrations were within $10^{-6}$ and $10^{-5}mole/l$. Three coagulants have not showed any considerable difference in the residual aluminum concentration up to 50 NTU. However PAC has showed the least residual aluminum in high turbidity water over 100 NTU. 2. The low alkalinity water having 25mg/l as $CaCO_3$ has showed less residual aluminum than the water having 50mg/l alkalinity. However, the difference was not significcant. 3. Even the lowest residual aluminum concentration was over 0.05mg/l. Therefore the process to reduce residual aluminum would be necessary in water treatment plants.

Aluminum was deposited on aluminum oxide powders using a fluidized bed reactor at atmospheric pressure. The aluminum oxide powders were irregular flakes with acute angles and the average particle size was 26 . The fluidized bed was formed by flowing argon gas at the velocity of 60 cm/sec. The optimal fluidization condition was obtained with the reactor designed to be tapered so that the fluid velocity decreases as the fluidizing gas goes up along the reactor. Aluminum was deposited by flowing TiBA(Triisobutylaluminum) evaporated at through the fluidized bed reactor heated to 350~. The result from the analysis by XRD and EDAX confirmed the coating of aluminum and an SEM micrograph showed the conformality.

목본식물에 대한 Al독성에 관한 기초자료를 얻고자, 이농도별(1.0, 2.5 및 5.0mM)수용액과 대조구로 지하수를 모래를 채운 화분에 삽목한 개나리와 플라타너스의 삽수에 1993년 4월 28일부터 6월 16일까지 주 3회씩 처리하였다. 6월 16일 삽목묘를 굴취하여 생장관련형질(신초의 생장, 엽수 및 엽록소함량)과 뿌리의 길이를 처리간 비교하였다. 모든 생장관련형질들(신초의 생장, 엽수 및 엽록소함량)에서 처리간 고도의 통계적 유의차가 인정되었으며, 뿌리생장의 경우 개나리삽목묘에서는 처리간 통계적 유의차가 인정되었으나, 플라타너스삽목묘에서는 처리간 유의차가 인정되지 않았다.

목본식물에 대한 Al독성에 관한 기초자료를 얻고자, Al농도별(1.0, 2.5및 5.0mM) 수용액과 대조구로 지하수를 모래를 채운 화분에 파종한 곰솔, 측백나무 및 쥐똥나무에 1993년 4월 28일부터 6월 16일까지 주 3회씩, 1회 5mm의 강도로 처리하였다. 6월 26일 묘목을 굴취하여 생장관련형질(묘목의 수, 묘고, 지상부, 지하부 및 개체당 건중량)을 측정하여 수종간, 처리간 비교하였다. Al수용액 처리에 대한 반응은 수종별로 상이하였으며, 쥐똥나무가 세 수종 중에서는 가장 감수성인 것으로 나타났으며, 곰솔이 가장 내성을 지닌 것이라 판단된다.

목본식물에 대한 Al독성에 관한 기초자료를 얻고자, Al농도별(1.0, 2.5및 5.0mM)수용액과 지하수에 수경삽목한 개나리삽수의 생장관련형질(신초의 생장, 엽수, 엽피해율 및 엽록소함량)을 처리간 비교하였다. 모든 생장관련형질들(신초의 생장, 엽수, 엽피해율 및 엽록소함량)에서 처리간 고도의 통계적 유의차가 인정되었으며. 1.0mM 정도의 Al수용액도 개나리삽수의 생장을 현저히 억제하였다.

점토 광물로부터 황산 처리법을 이용하여 수화 황산 알루미늄을 제조하였다. 하동 카올린 을 황산 처리하였을 때 수화 황산 알루미늄 형성에 미치는 카올린의 하소 온도와 하소 시간, 산처리 반응 온도와 반응 시간 및 황산의 농도의 영향을 조사하였다. 또한, 황산 처리된 용액으로부터 수화 황산 알루미늄이 석출되는 최적 조건을 구하였으며, 생성된 수화 황산 알루미늄을 상온에서 1200˚C 까지 각각의 온도 구간에서 열처리한 분말에 대해서 XRD, TG-DTA, FT-IR, SEM, 입도 분석 및 불순물 분석을 하였다. 최적 조건 하에서, 카올린 중의 알루미나가 수화 황산 알루미늄으로 생성되는 전화율은 약 60%였고, XRD, TG-DTA, FT-IR 등의 분석 결과로 부터 생성된 수화 황산 알루미늄의 열분해 반응은 Al2(SO4)3·18H2O→Al2(SO4)3·6H2O→Al2(SO4)→ amorphous alumina→γ-alumina→δ-alumina→θ-alumina→α-alumina이었다. 또한 생성된 수화 황산 알루미늄을 1200˚C에서 하소 하여 얻은 알루미나 분말의 순도는 99.99%였다.

Recently, with the tendency of more lightening, high-strength and high-speed in the marine industries such as marine structures, ships and chemical plants, the use of the aluminium Alloy is rapidly enlarge and there occurs much interest in the study of corrosion fatigue crack characteristics. In this paper, the initiation of surface crack and the propagation characteristics on the base metal and weld zone of 5086-H116 Aluminium Alloy Plate which is one of the Al-Mg serious alloy(A5000serious) used most when building the special vessels, were investigated by the plane bending corrosion fatigue under the environments of marine, air and applying cathodic protection. The effects of various specific resistances on the initiation, propagation behavior of corrosion fatigue crack and corrosion fatigue life in the base metal and heat affected zone were examined and its corrosion sensitivity was quantitatively obtained. The effects of corrosion on the crack depth in relation to the uniform surface crack length were also investigated. Also, the structural, mechanical and electro-chemical characteristics of the metal at the weld zone were inspected to verify the reasons of crack propagation behavior in the corrosion fatigue fracture. In addition, the effect of cathodic protection in the fracture surface of weld zone was examined fractographically by Scanning Electron Microscope(S.E.M.). The main results obtained are as follows; (1) The initial corrosion fatigue crack sensitibity under specific resistance of 25Ω.cm% show 2.22 in the base metal and 19.6 in the HEZ, and the sensitivity decreases as specific resistance increases (2) By removing reinforcement of weldment, the initiation and propagation of corrosion crack in the HAZ are delayed, and corrosion fatigue life increases. (3) As specific resistance decreases, the sensitivity difference of corrosion fatigue life in the base metal and HAZ is more susceptible than that of intial corrosion fatigue crack. (4) Experimental constant, m(Paris' rule) in the marine environment is in the range of about 3.69 to 4.26, and as specific resistance increases, thje magnitude of experimental constant, also increases and the effect by corrosion decreases. (5) Comparing surface crack length with crack depth, the crack depth toward the thickness of specimen in air is more deeply propagated than that in corrosion environment. (6) The propagation particulars of corrosion fatigue crack for HAZ under initial stress intensity factor range of δk sub(li) =27.2kgf.mm super(-3/2) and stress ratio of R=0 shows the retardative phenomenon of crack propagation by the plastic deformation at crack tip. (7) Number of stress cycles to corrosion fatigue crack initiation of the base metal and the welding heat affected zone are delayed by the cathodic protection under the natural sea water. The cathodic protection effect for corrosion fatigue crack initiation is eminent when the protection potential is -1100 mV(SCE). (8) When the protection potential E=-1100 mV(SCE), the corrosion fatigue crack propagation of welding heat affected zone is more rapid than that of the case without protection, because of the microfissure caused by welding heat cycle.

Recently with the rapid development in marine and shipbuilding industries such as marine structures, ships and chemical plants, it takes much interest in the study of corrosion fatigue characteristics that was close up an important role in mechanical design. In this study, characteristics of corner crack propagation on the base metal and heat affected zone of 5086 Al-Alloy was tested by using of a rotary bending fatigue tester and was investigated under the environments of specific resistance, σ=25Ω cm and air. The corrosion fatigue crack initiation and corrosion fatigue life sensitivity were quantitatively inspected for 5086 Al-Alloy in the specific resistance, σ=25Ω cm. Main results obtained are as follows: (1) The corrosion sensitivity of heat affected zone under specific resistance, σ=25Ωcm shows approximately 1.69~2.22 and corrosion sensitivity of base metal is more susceptible than that of heat affected zone. (2) The corrosion fatigue life sensitivity on heat affected zone decreases eminently than that of initial corrosion fatigue crack. (3) The characteristics of quarter elliptical corner crack propagation shows that depth crack is more grown than surface crack at crack initiation, but the surface crack is more propagated than depth crack as the crack propagation is increased. (4) The surface crack and depth crack growth on heat affected zone by softness show delayed phenomenon than that of base metal.

평면 굽힘부식피로 시험기를 사용하여 선박용 알루미늄합금재의 부식피로파양에 관한 연구를 한 결과 다음과 같은 결론을 얻었다. 1. 비저항이 증가함에 따라서 초기 부식피로균열발생까지의 반복회수는 지연되고, 그 부식감수성은 감소하는 양상을 나타낸다. 2. 비저항이 감소할수록 Paris rule의 실험상수 m 값은 작아지면서 응력강도 계수값에 비해 부식에 의한 영향이 더욱 민감해 진다. 3. 알루미늄 5086 합금의 부식피로균열은 입계균열파양의 양상을 보이고 있다. 4. 응력강도계수값이 증가함에 따라 부식감수성은 감소되어지고 응력강도계수값이 40kg.mm super(-3/2) 이상일 때 부식감수성은 거의 균일하게 된다.