• 대한환경공학회지
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• 제35권1호
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• pp.17-22
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• 2013

본 연구는 조류 개체 수 증가로 pH가 급격하게 상승한 원수가 정수장으로 유입될 때 pH 조정을 위해 사용하는 이산화탄소($CO_2$) 주입이 응집효율 및 용존 알루미늄 농도변화에 미치는 영향을 고찰하였다. 응집제 1 mg/L에 주입에 따른 pH 감소는 LAS -0.0384, PAC -0.0254, A-PAC -0.0201, PACS2 -0.0135로 나타났다. 용존 알루미늄 농도는 pH 7.44에서 0.02 mg/L, pH 7.96에서 0.07 mg/L, pH 8.16에서 0.12 mg/L, pH 8.38에서 0.39 mg/L로 응집공정의 pH 증가에 따라 용존 알루미늄 농도가 증가하는 것으로 나타났다. 여기서 주목할 점은 급속 교반 후 pH 8.0을 초과할 때부터 용존 알루미늄 농도는 급격하게 증가하는 것이다. 그러므로 높은 pH의 원수가 유입되는 정수장에서 알루미늄 농도가 먹는 물 수질 기준 만족하기 위해서는 응집공정의 pH가 7.8 이하로 유지되도록 공정관리가 필요하며, 원수 pH가 8.0 이상 유입되는 경우 이산화탄소($CO_2$) 주입으로 pH를 7.3 내외로 일정하게 유지할 수 있었다. 또한 이산화탄소($CO_2$) 주입으로 응집공정에서 pH를 조정함으로써 탁도 및 응집제 절감, 용존 알루미늄 농도 감소 효과를 확인할 수 있었다.

• 항공우주기술
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• 제13권1호
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• pp.20-26
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• 2014

본 논문에서는 충격하중과 잔류 에너지 등의 충격거동에 대한 영향을 확인하기 위하여 항복응력, 탄젠트 강성계수 및 파단 변형률을 변화시켰다. 그리고 섬유금속 적층판의 좌굴거동을 수치해석을 이용하여 수행하였다. 좌굴 성능을 비교하기 위하여 섬유금속 적층판과 알루미늄 판에 대해 인장 및 압축하중에 대한 여러 가지 경우의 해석을 수행하였다. 또한 정적 성능을 평가하기 위하여 박스 보 구조물의 정적해석을 수행하였다. 알루미늄 2024 박판과 유리섬유/에폭시 프리프레그로 만든 섬유금속 적층판에 대한 저속충격 해석을 수행하였다. 그리고 좌굴 및 정적해석 결과를 이용하여 섬유금속 적층판과 알루미늄의 성능을 비교하였다. 구조적 성능 비교를 위하여 동일한 무게의 알루미늄 2024 박판에 대한 해석을 수행하였다.

• 한국생산제조학회지
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• 제21권5호
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• pp.824-829
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• 2012

The purpose of this study is to evaluate the proposed jig for turning process of large-scale aluminum tube of D500mm through Finite Element Analysis (FEA). Also, a machining evaluation is conducted with general heat-treated and cryogenic heat-treated tubes. Dimensions of the specimens are determined to be suitable for collet appearance. The characteristics of equivalent stress and strain according to the expansion of the collet are evaluated by FEA. The aluminum tubes which are heat-treated by T4/T6 condition and cryogenic condition are machined by using a large-scale lathe machine and the roundness of machined tube is evaluated by using a 3D measuring machine. Through the results of this study, effects of each heat treatment and residual stress on the roundness are established.

• 한국CDE학회논문집
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• 제17권3호
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• pp.188-197
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• 2012

Recently, aluminum ships are constructed more than ever because of the environmental pollution generated by FRP (Fiber Reinforced Plastic) ships. In particular, FRP ships have been replaced by the Aluminum ships. The forming process of the curved aluminum plate has been performed only by labor works without systematic technique. Therefore, it is difficult to construct the aluminum ship that the design satisfies both required propulsion performance and hull design. Present study introduces a MPSF (Multi Point Stretching Forming) that is a flexible manufacturing technique to form large sheet panels of doubly curvature. The hull pieces are stretch-formed over the MPSD (multi-point stretching die) generated by the punch element matrix. In this study, MPSF is applied to deform the doubly curved surfaces of aluminum ship. The forming system including FEA (finite element analysis) of the processes for stretching the plate were carried out by static implicit analysis is suggested. Residual deformation of the surface is modeled by an elasto-plastic contact phenomena while the forming process is simulated by FEA. Finally, the proposed system is also validated, comparing the deformed shape by MPSF with that of object surfaces.

• 한국항공우주학회지
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• 제33권6호
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• pp.39-44
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• 2005

섬유금속적층판(Fiber Metal Laminates, 이하 FML)에서 알루미늄과 유리섬유/에폭시 복합재료 사이의 열팽창 계수의 차이는 경화공정 시 FML내부에 열 잔류응력을 남기게 되며, 이러한 열 잔류응력은 FML의 피로특성과 항복강도에 영향을 주게 된다. 잔류응력을 예측하기 위해 두 가지 실험법이 제안 되었으며, 이론식을 통해 그 결과를 예측하고, 실제 실험을 수행하여 그 값을 확인 하였다. 또한, 열 잔류응력의 제거 및 응력의 역전을 위하여 후-인발 가공이 수행 되었으며, 가공 이후 발생한 FML내의 잔류응력이 측정 되었다. 예측된 열 잔류응력 결과와 실험을 통한 값이 일치함을 보이며, 후-인발 가공을 통하여 열 잔류응력 제거 및 항복강도의 증가가 발생하였다.

• Applied Science and Convergence Technology
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• 제23권6호
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• pp.309-316
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• 2014

A large particle accelerator requires an ultrahigh vacuum (UHV) system of average pressure under $1{\times}10^{-7}$ Pa for mitigating the impact of beam scattering from the residual gas molecules. The surface inside the beam ducts should be controlled with an extremely low thermal outgassing rate under $1{\times}10^{-9}Pa{\cdot}m^3/(s{\cdot}m^2)$ for the sake of the insufficient pumping speed. To fulfil the requirements, the aluminum alloys were adopted as the materials of the beam ducts for large accelerator that thanks to the good features of higher thermal conductivity, non-radioactivity, non-magnetism, precise machining capability, et al. To put the aluminum into the large accelerator vacuum systems, several key technologies have been developed will be introduced. The concepts contain the precise computer numerical control (CNC) machining process for the large aluminum ducts and parts in pure alcohol and in an oil-free environment, surface cleaning with ozonized water, stringent welding process control manually or automatically to form a large sector of aluminum ducts, ex-situ baking process to reach UHV and sealed for transportation and installation, UHV pumping with the sputtering ion pumps and the non-evaporable getters (NEG), et al. The developed UHV technologies have been applied to the 3 GeV Taiwan Photon Source (TPS) and revealed good results as the expectation. The problems of leakage encountered during the assembling were most associated with the vacuum baking which result in the consequent trouble shootings and more times of baking. Then the installation of the well-sealed UHV systems is recommended.

• 한국표면공학회지
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• 제41권3호
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• pp.121-128
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• 2008

High strength 7xxx aluminum alloys have been applied to automotive bump back beam of the some limited model for light weight vehicle. The aluminum bump back beam is manufactured through extrusion, bending and welding. The residual stress given on these processes combines with the corrosive atmosphere on the road spreaded with corrosive chemicals to melt snow to occur the stress corrosion cracking. The composition of commercial 7xxx aluminum has Zn/Mg ratio about 3 and Cu over 2 wt% for better strength and stress corrosion cracking resistivity. But this composition isn't adequate for appling to the automotive bump back beam with high resistance to extrusion and bad weldability. In this study the composition of 7xxx aluminum alloy was modified to high Zn/Mg ratio and low Cu content for better extrusion and weldability. To estimate the resistivity against stress corrosion cracking of this aluminum alloy by slow strain rate test, the corrosion atmosphere and strain rate separate the stress corrosion cracking from conventional corrosion must be investigated. Using 0.6 Mol NaCl solution on slow strain rate test the stress corrosion cracking induced fracture was not observed. By adding 0.3% $H_2O_2$ and 0.6M $Na_2SO_4$ to 1M NaCl solution, the corrosion potential and current density of polarization curve moved to active potential and larger current density, and on the slow strain rate test the fracture energy in solution was lower than that in pre-exposure. These mean the stress corrosion cracking induced fracture can be estimated in this 1M NaCl + 0.3% $H_2O_2$ + 0.6M $Na_2SO_4$ solution. When the strain rate was below $2{\times}10^{-6}$, the stress corrosion cracking induced fracture start to be observed.

• Structural Engineering and Mechanics
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• 제53권5호
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• pp.867-880
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• 2015

Mechanical fastening is still one of the main methods used for joining components. Different techniques have been applied to reduce the effect of stress concentration of notches like fastener holes. In this work we evaluate the feasibility of combining laser shock peening (LSP) and cold expansion to improve fatigue crack initiation and propagation of open hole specimens made of 6061-T6 aluminum alloy. LSP is a new and competitive technique for strengthening metals, and like cold expansion, induces a compressive residual stress field that improves fatigue, wear and corrosion resistance. For LSP treatment, a Q-switched Nd:YAG laser with infrared radiation was used. Residual stress distribution as a function of depth was determined by the contour method. Compact tension specimens with a hole at the notch tip were subjected to LSP process and cold expansion and then tested under cyclic loading with R=0.1 generating fatigue cracks on the hole surface. Fatigue crack initiation and growth is analyzed and associated with the residual stress distribution generated by both treatments. It is observed that both methods are complementary; cold expansion increases fatigue crack initiation life, while LSP reduces fatigue crack growth rate.

• 대한기계학회논문집A
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• 제21권2호
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• pp.305-316
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• 1997

A more efficient method for obtaining the fatigue life enhancement of a structure member with fastener holes is described. It is based on the combined process of cold-expansion and ring-indentation. Residual stresses were induced onto premachined holes using ring-indentation process near the fastener hole combined with cold-expansion. And residual stresses at the vicinity of a hole were evaluated using a fracture mechanics approach. The compressive residual stresses were larger using the combined process than is in the case of simple cold-expansion. Fatigue testing of aluminum specimens showed that the fatigue crack growth retardation emanating from a circular hole was greater for the combined process than for a simple cold-expansion alone.

• 한국주조공학회지
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• 제22권5호
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• pp.257-264
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• 2002

Effects of Ca content on the refinement of primary Si of Aluminum B390 alloy have been examined. Ca was found to have an effect on the refinement of primary Si particle. Primary Si particle size has been refined as Ca content of the melts decreased and cooling rate increased. A control of Ca content by the addition of $CuCl_2$ to the melt was the most efficient in the refinement of primary Si particles. The minimum size of primary Si particles in this study was $15.0\;{\mu}m$ when a residual content of Ca element in the alloy was 5ppm, Primary Si particle size was refined as primary Si crystallization temperature increased, which was attributed to the decrease of Ca content in the melts.