• 펄프종이기술
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• 제40권2호
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• pp.37-42
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• 2008

Defects of corrugated board were limiting factors to the corrugated industry's growth. On-line detecting systems of defects are beneficial to increase profits of the corrugated board companies by reducing base paper consumption, increasing process reliability, and increasing productivity. By replacing naked eye inspection of defects to a defects detecting system, continuous inspection without fatigue may guarantee final products quality. The system was developed, which was consisted of line scan CCD camera, lens, illuminating parts, high speed image processor, software, various input parts, and output parts. First installation location of the system was at before fluting process after base paper unwinding, and surface of liner board was inspected by the system. Second installation location was after fluting process and combining process for liner board. Production loss includes ragged appearance of edge, irregular flute shape, wrong combination of flute, score cracking, defects in base paper, and flute cracking. The production loss was analyzed before and after the system installation at a commercial domestic mill. The production loss ratio was defined as a production loss weight per total production weight. The production loss ratio before the installation was decreased a lot from 1.28%(during 3 months before installation) to 0.76%(during 12 months after the first installation) and to 0.25%(during 6 months after the second installation).

• 한국안전학회지
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• 제24권2호
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• pp.17-22
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• 2009

Thermal stress and elastic creeping stress analysis was conducted by finite element method to simulate start-up process of a boiler header of 500MW standard fossil power plant. Start-up temperature and operating pressure history were simplified from the real field data and they were used for the thermal stress analysis. Two kinds of thermal stress analysis were considered. In the first case only temperature increase was considered and in the second case both of temperature and operating pressure histories were considered. In the first analysis peak stress was occurred during the temperature increase from the room temperature. Hence cracking or fracture may occur at the temperature far below the operating maximum temperature. In the results of the second analysis von Mises stress appeared to be higher after the second temperature increase. This is due to internal pressure increase not due to the thermal stress. When the stress components of radial(r), hoop($\theta$) and longitudinal(z) stress were investigated, compression hoop stress was occurred at inner surface of the stub tube when the temperature increased from room temperature to elevated temperature. Then it was changed to tension hoop stress and increased because of the operating pressure. It was expected that frequent start-up and shut-down operations could cause thermal fatigue damage and cracking at the stub tube hole in the header. Elastic-creeping analysis was also carried out to investigate the stress relaxation due to creep and stabilized stress after considerable elapsed time. The results could be used for assessing the creep damage and the residual life of the boiler header during the long-tenn service.

• 대한기계학회논문집A
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• 제34권9호
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• pp.1227-1233
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• 2010

가스터빈엔진 내의 블레이드에서는 표면에 외부의 찬 공기를 흘려주는 작은 냉각 홀들을 가공하고 열 차단 코팅시스템을 코팅하는 방법으로 기지금속을 고온에서 보호한다. 열 차단 코팅은 열피로 과정에서 산화막의 성장 및 접합층과 산화막의 열팽창계수의 불일치로 산화막내부에 잔류응력이 발생하며 궁극적으로 코팅층의 분리를 유발한다. 본 연구에서는 내열합금 시편 표면에 작은 홀을 가공하여 여러 가지 고온 유지 조건에서 열 및 기계적 피로 시험을 수행하여 홀 주위의 산화막의 변형을 관찰하였다. 실험결과 기계적 피로가 홀 주위의 산화막의 변형에 중요한 영향을 미치며, 동일한 산화막 두께에서 고온 유지 시간이 짧을수록 변형이 쉽게 발생 하였다. 또한 본 연구에서는 홀 주위 산화막의 응력해석을 위한 이론적인 연구도 시도되었다.

• 콘크리트학회논문집
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• 제14권1호
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• pp.76-82
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• 2002

초속경 시멘트 콘크리트는 양생 시 초기재령에서 높은 수화열과 건조수축으로 인해 균열이 발생하기 쉽다. 이러한 문제점을 해결하기 위해 각종 소재를 적극 활용하려는 노력의 일환으로 섬유보강 콘크리트를 사용하게 된다 합성섬유보강 콘크리트는 건조수축에 대한 저항성과 내구성을 증진시키는 것으로 보고되고 있는데 대부분이 일반콘크리트에 대한 연구가 수행되었을 뿐 초속경 시멘트콘크리트에 관한 건조수축의 영향에 대해 정량적 및 정성적 연구가 미미한 상태이다. 따라서, 본 연구에서는 합성섬유보강 콘크리트의 건조수축 저감효과와 초속경 시멘트 콘크리트에서 수축에 대한 구속효과를 평가하기 위하여 콘크리트종류, 섬유보강 여부, 물-시멘트비, 구속여부를 주요 실험변수로 하여 건조수축실험을 수행하였다. 그 결과 일반 콘크리트에 비해 초속경 시멘트 콘크리트의 건조수축의 진행이 상당히 작음을 알 수 있었다. 이는 속경성 콘크리트의 수화반응이 빠르게 진행되어 건조에 의한 중량감소율이 다소 작은 점과 수화생성물과의 관계에 기인되는 것으로 판단된다. 또한 1축으로 구속된 건조수축의 구속으로 인한 초속경 시멘트 콘크리트의 건조수축을 예측할 수 있었고 초속경 시멘트 콘크리트에 섬유보강으로 인한 건조수축 제어는 일반콘크리트에 비해 효과가 매우 큰 것으로 나타났다.

• 대한토목학회논문집
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• 제26권3D호
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• pp.445-451
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• 2006

본 연구는 노후 콘크리트 포장의 아스팔트 덧씌우기에서 발생하는 반사균열을 억제하기 위한 방안으로 노후 콘크리트와 아스팔트 표층 사이에 응력을 흡수할 수 있는 중간층 혼합물을 개발하기 위하여 수행되었다. 고탄성 응력흡수층은 휨 변형과 수평변형으로 인하여 발생하는 균열응력을 흡수 또는 분산 시킬 수 있는 탄성과 유연성, 균일성 및 불투수성이 요구된다. 본 연구로부터 국외제품을 모델로 국산 바인더를 개발 하였으며 이를 사용하여 제작된 혼합물 시편은 시방규격에 만족하였다. 기존 덧씌우기 공법과 비교한 시험으로부터 고탄성 응력흡수 중간층이 설치된 경우 설치되지 않은 경우에 비하여 전단파괴수명과 수평변위저항도는 약 4배가 증가되었으며 표층재료의 선정에 따라 전단파괴수명은 5배, 수평변위저항도는 9배가 증가되어 고탄성 응력흡수 중간층이 반사균열 억제에 우수한 것으로 본 연구에 나타났다.

• 한국산학기술학회논문지
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• 제21권6호
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• pp.448-454
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• 2020

본 연구는 항공기 운용 중 발생하는 구조결함의 원인을 규명하고 개선형상에 대한 구조 건전성을 확인하고자 한다. 항공기 균열은 Bulkhead 체결구조로서 연료탱크 경계 Web 파열로 인한 연료누유 현상에서 식별되었다. 균열의 특성을 확인하기 위해 파단면을 분석하였고 반복하중에 의해 균열이 진전되어 최종 파단으로 이어지는 피로파괴로 판단하였다. 또한 다중 시작점에서 균열이 시작되는 것으로 소재의 결함이 균열의 주요 원인으로 판단되지 않는다. 항공기 운용 중 발생하는 기동하중에 대한 균열 영향을 확인하기 위해 항공기 지상 및 비행시험을 통해 분석을 수행하였다. 항공기 운용 중 균열 부위의 하중 측정 데이터와 항공기 설계하중과의 비교를 통한 분석 결과 측정하중은 설계 대비 30% 수준으로 파손을 유발할 수준은 아니라고 판단하였다. 항공기 운용 시 진동하중의 원인으로 조립 및 단품 제작공차가 최대 0.06inch 발생할 수 있는 Gap을 검토하였고, 분석결과 균열부위에서 큰 응력인 약 32ksi가 발생하였다. 또한 Pre-Load에 의해 M.S.(Margin of Safety)가 +0.71에서 +0.34로 약 50%이상 감소되는 것으로 확인되어 항공기 설계 하중과 조합 시 균열 가능성이 급격히 증가하였다. 따라서 항공기 균열부위에 대하여 구조 보강 및 Gap 제거를 통해 결함을 개선하였다. 개선형상에 대하여 구조강도 해석 결과 Bulkhead는 허용응력 대비 M.S.가 약 +0.88이고 Fitting 형상은 약 +0.48로서 충분한 마진이 확보되었다. 또한 수명해석 결과 형상 개선 전 수명인 약3,600 시간 대비 개선형상은 약84,000 시간으로서 항공기 설계수명 대비 구조건전성을 확인하였다.

• 한국표면공학회:학술대회논문집
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• 한국표면공학회 2003년도 추계학술발표회초록집
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• pp.134-135
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• 2003

The dental implant materials required good mechanical properties, such as fatigue strength, combined with a high resistance to corrosion. For increasing fatigue resistance and delaying onset of stress corrosion cracking, shot peening has been used for > 50 years to extend service life of metal components. However, there is no information on the electrochemical behavior of shot peened and hydroxyapatite(HA) coated Ti-6Al-4V alloys. To increase fatigue strength, good corrosion resistance, and biocompatibility, the electrochemical characteristics of Ti/TiN/HA coated and shot peened Ti-6Al-4V alloys by electron beam physical vapor deposition(EB-PVD) have been researched by various electrochemical method in 0.9%NaCl. Ti-6Al-4V alloys were prepared under the condition of hydrogen and vacuum arc furnace. The produced materials were quenched at 1000$^{\circ}C$ under high purity dried Ar atmosphere and were hold at 500$^{\circ}C$ for 2 hrs to achieve the fatigue strength(1140㎫) of materials. Ti-6Al-4V alloys were prepared under the condition of hydrogen and vacuum arc furnace. Shot peening(SP) and sand blasting treatment was carried out for 1, 5, and 10min. On the surface of Ti-6Al-4V alloys using the steel balls of 0.5mm and alumina sand of 40$\mu\textrm{m}$ size. Ti/TiN/HA multilayer coatings were carried out by using electron-beam deposition method(EB-PVD) as shown Fig. 1. Bulk Ti, powder TiN and hydroxyapatite were used as the source of the deposition materials. Electrons were accelerated by high voltage of 4.2kV with 80 - 120mA on the deposition materials at 350$^{\circ}C$ in 2.0 X 10-6 torr vacuum. Ti/TiN/HA multilayer coated surfaces and layers were investigated by SEM and XRD. A saturated calomel electrode as a reference electrode, and high density carbon electrode as a counter electrode, were set according to ASTM GS-87. The potentials were controlled at a scan rate of 100 mV/min. by a potentiostat (EG&G Co.273A) connected to a computer system. Electrochemical tests were used to investigate the electrochemical characteristics of Ti/TiN/HA coated and shot peened materials in 0.9% NaCl solution at 36.5$^{\circ}C$. After each electrochemical measurement, the corrosion surface of each sample was investigated by SEM.

• Smart Structures and Systems
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• 제21권4호
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• pp.421-433
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• 2018

Carbon fiber reinforced polymer (CFRP) cable has good mechanical properties and corrosion resistance. However, the anchorage of CFRP cable is a big issue due to the anisotropic property of CFRP material. In this article, a high-efficient bonding anchorage with novel configuration is developed for CFRP cables. The acoustic emission (AE) technique is employed to evaluate the performance of anchorage in the fatigue test and post-fatigue ultimate bearing capacity test. The obtained AE signals are analyzed by using a combination of unsupervised K-means clustering and supervised K-nearest neighbor classification (K-NN) for quantifying the performance of the anchorage and damage evolutions. An AE feature vector (including both frequency and energy characteristics of AE signal) for clustering analysis is proposed and the under-sampling approaches are employed to regress the influence of the imbalanced classes distribution in AE dataset for improving clustering quality. The results indicate that four classes exist in AE dataset, which correspond to the shear deformation of potting compound, matrix cracking, fiber-matrix debonding and fiber fracture in CFRP bars. The AE intensity released by the deformation of potting compound is very slight during the whole loading process and no obvious premature damage observed in CFRP bars aroused by anchorage effect at relative low stress level, indicating the anchorage configuration in this study is reliable.

• 한국분말재료학회지
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• 제20권6호
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• pp.460-466
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• 2013

4 mol% Yttria-stabilized zirconia (4YSZ) coatings with $200{\mu}m$ thick are fabricated by Electron Beam Physical Vapor Deposition (EB-PVD) for thermal barrier coating (TBC). $150{\mu}m$ of NiCrAlY based bond coat is prepared by conventional APS (Air Plasma Spray) method on the NiCrCoAl alloy substrate before deposition of top coating. 4 mol% YSZ top coating shows typical tetragonal phase and columnar structure due to vapor phase deposition process. The adhesion strength of coating is measured about 40 MPa. There is no delamination or cracking of coatings after thermal cyclic fatigue and shock test at $850^{\circ}C$.

• 한국주조공학회지
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• 제38권2호
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• pp.48-54
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• 2018

To improve the durability of the turbocharger, it is important to suppress cracking of the turbine housing; therefore, we investigated the initiation and growth of these cracks. First, we initiated a crack in the turbine housing using endurance experiments. After the endurance test, cracks mainly occurred in the valve seat, the nozzle area, and the scroll part of the turbine housing. The results of a fracture analysis of the cracks showed that cracks in the valve seat were initiated by fatigue fracture. This seems to be caused by the accumulation of mechanical and thermal stresses due to vibration of the turbine wheel and high-temperature exhaust gas. Also, cracks in nozzle and scroll area were initiated by intergranular corrosion due to the exhaust gas. Thus, although there are differences in the cause of initiation according to the site, a concentric waveform was observed in all fracture planes. This phenomenon indicates that cracks gradually grow due to repeated stress changes, and the main causes are the temperature difference of the exhaust gas and the vibration caused by the turbine shaft.