• 방사성폐기물학회지
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• 제14권4호
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• pp.411-422
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• 2016

최근 국내 원전의 경수로 사용후핵연료 습식 저장시설의 포화시점이 다가옴에 따라 운반 및 저장용기를 이용한 건식저장시스템 개발이 활발하게 수행되고 있다. 일반적으로 사용후핵연료 운반 및 저장용기 설계를 위한 차폐해석 시 장전 가능 연료 중 가장 보수적인 연료를 설계기준연료로 선정하여 해석을 수행한다. 그러나 실제 금속 운반용기에 장전되는 사용후핵연료는 해석평가에 적용된 설계기준연료에 한정되지 않고 다양하기 때문에 초기농축도, 연소도, 최소냉각기간의 특성을 고려한 차폐평가를 통하여 장전가능 여부가 결정된다. 이에 본 연구에서는 금속 겸용용기에 장전 가능한 연료를 대상으로 국내 운반기준을 만족하는 최소냉각기간의 결정을 위한 차폐해석 방법을 기술하였다. 특히 발생량이 많은 초기농축도 3.0~4.5wt%의 사용후핵연료는 차폐해석 구간을 세분화하여 평가하여 연구결과의 활용에 효율성을 높이고자 하였다. 차폐평가를 통해 2008년까지 국내 원전에서 발생한 장전대상연료 중 약 81%의 사용후 핵연료를 금속겸용용기로 운반할 수 있는것으로 평가되었다. 본 연구결과를 통해 금속 겸용용기의 운반조건에 장전 가능한 연료의 특성을 제시함으로써 운반 시 운영절차의 개발을 위한 기술적 근거 수립에 도움이 되고자 한다.

• 폴리머
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• 제35권3호
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• pp.203-209
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• 2011

표면이 매끄럽고 돌기가 있는 2가지 HDPE 지오멤브레인 덤벨형 시료에 두께 10% 간격으로 10~90% 깊이의 노치를 가하여 실험에 사용하였다. ISO 10722에 의거하여 부가하중 횟수를 변화시켜 시공시 손상의 실내 모사시험을 HDPE 지오브레인에 실시하였으며, 부가하중 횟수가 시공시 손상에 미치는 영향을 비교하였다. 항복응력과 변형률은 노지 깊이가 커짐에 따라 감소하였다. 손상된 그리고 노치를 가한 지오멤브레인을 응력균열시험에 사용하였으며, $50{\pm}1^{\circ}C$에서 pH 4와 12 용액에 침지시켜 항복응력 변화에 따른 응력균열저항성을 NCTL 시험을 통하여 고찰하였다. 인장 강도의 35% 이상에서 지오멤브레인은 응력균열에 취약함을 나타냈으며, 손상을 받은 그리고 노치를 가한 지오멤브레인 모두 같은 경향을 나타내었다. 특별히 노치를 가한 지오멤브레인의 경우 각각의 응력균열 조건에서 시공에 의해 손상된 지오멤브레인보다 낮은 강도를 나타내었다.

• Journal of Welding and Joining
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• 제26권3호
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• pp.67-73
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• 2008

Fatigue life evaluation of welded structures in a range of high cycles is one of the most difficult problems since extremely small plastic deformation and damage occur during the loading cycles. Moreover, it is very difficult to identify the strong non-linearities of welding, inducing residual stress. In this paper, numerical fatigue test method for welded structures was developed using continuum damage mechanics with inherent strain. Recently, continuum damage mechanics, which can simulate both crack initiation at the micro-scale level and crack propagation at the meso-scale level, has been adopted in the fracture related problem. In order to consider the residual stresses in the welded strictures, damage calculation in conjunction with welding, inducing inherent strain, was proposed. The numerical results obtained from the damage calculation were compared to experimental results.

• 한국세라믹학회지
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• 제34권3호
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• pp.296-302
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• 1997

SiC휘스커를 첨가한 알루미나 분말 기지 복합체의 치밀화에 미치는 상온 반복 압축의 영향을 조사하였다. 반복 압축 응력과 반복 횟수가 증가할수록, 또한 바이어스 압력이 낮을수록 복합체의 초기 성형 밀도가 증가하였으며 가압 및 제하 속도, 반복 속도는 분말의 미끄러짐과 재배열에 큰 영향을 미치지 않음을 알 수 있었다. 상온 반복 압축으로 인한 SiC 휘스커의 파단은 거의 없었으며 휘스커의 배열 방향은 반복 압축 방향에 관계없이 고른 분포를 나타냄으로써 상온 반복 압축 성형이 SiC 휘스커를 첨가한 알루미나 분말 기지 복합체의 초기 성형 밀도를 높일 수 있는 효과적인 방법임을 알 수 있었다.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 2004년도 춘계학술대회 논문집
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• pp.136-142
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• 2004

Effects of Nb(Niobium) contents and solution annealing on the strength and fatigue lift of 18%Ni maraging steel commonly using in aircraft, space field, nuclear energy, and vehicle etc. were investigated. Also the fatigue life stress intensity factor were compared experiment result and FEA(finite element analysis) result. The more Nb content, the higher or the lower fatigue lift on base metal specimens or solution annealed specimens showing that the fatigue life was almost the same. The maximum stresses of X, Y, and Z axis direction showed about 2.12${\times}$10$^2$MPa, 4.40${\times}$10$^2$MPa and 1.32${\times}$10$^2$MPa respectively. The Y direction stress showed the highest because of the same direction as the loading direction. The fatigue lives showed about 7% lower FEA result than experiment result showing almost invariable error every analyzed cycle. Stress intensity factor of the FEA result was lower about 3.5∼10% than that of the experiment result showing that the longer fatigue crack length, the higher error. It considered that the cause for the difference was the modeled crack tip having always the same shape and condition regardless of the crack growth.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2004년도 추계학술대회 논문집
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• pp.166-169
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• 2004

A fatigue test was used to evaluate the fatigue life of an actual structure. The loaded state and the constraint condition of an actual structure must be same as the specimen in order to apply the test results to an actual structure by the specimen. The loaded state and constraint conditions can't be same as the specimen in the actual structure which is complicated. In order to reduce these differences, an actual structure test with a lot of frequencies is need to get a fatigue life curve. Therefore, ten sets of accelerated test units which attached unbalanced mass were composed in this study. Acceleration history about the vibration of an actual structure was acquired. Rainflow counting was used on acceleration history, and the life curve return formula was assumed. The return formula that damage satisfied `1' was acquired in a feedback process by the Miner's rule, which was the linear cumulative damage theory. A conservative fatigue life curve was determined with a return formula to have been presumed by each set. The fatigue life of regular rpm condition was calculated by these conservative fatigue life curves.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2004년도 추계학술대회 논문집
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• pp.1256-1261
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• 2004

Nonlinear Response Optimization using Equivalent Static Loads (NROESL) method/algorithm is proposed to perform optimization of non-linear response structures. It is more expensive to carry out nonlinear response optimization than linear response optimization. The conventional method spends most of the total design time on nonlinear analysis. Thus, the NROESL algorithm makes the equivalent static load cases for each response and repeatedly performs linear response optimization and uses them as multiple loading conditions. The equivalent static loads are defined as the loads in the linear analysis, which generates the same response field as those in non-linear analysis. The algorithm is validated for the convergence and the optimality. The function satisfies the descent condition at each cycle and the NROESL algorithm converges. It is mathematically validated that the solution of the algorithm satisfies the Karush-Kuhn-Tucker necessary condition of the original nonlinear response optimization problem. The NROESL algorithm is applied to two structural problems. Conventional optimization with sensitivity analysis using the finite difference method is also applied to the same examples. The results of the optimizations are compared. The proposed method is very efficient and derives good solutions.

• 한국해양공학회지
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• 제1권1호
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• pp.104-110
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• 1987

Fatigue tests by axial loading (R = 0.05) were carried out to investigate fatigue crack growth characteristics of small surface cracks in 2 1/4 Cr-1 Mo steel at room temperature by using flat specimens with a small artificial pit. All the data of the fatigue crack growth rate obtained in the present test are determined as a function of the stress intensity factor range about a semi-elliptical crack, so that the application of linear fracture mechanics to the surface fatigue crack growth and to the fatigue crack growth into depth, and all the data obtained from tests were discussed in comparison with the data of Type 304 stainless steel and two type of mild steel under the same test conditions. The obtained results are as follows: 1)When the cycle ratios are same, surface fatigue crack length and its depth are almost same and fall within a narrow scatter band in spite of different stress levels. 2)Relations of the surface fatigue crack growth rate (da/dN) and fatigue crack growth rate into depth (db/dN) to its stress intensity factor range ($\Delta K_{Ia}, \Delta K_{Ib}$) can be plotted as a straight line at log-log diagram without dependence of stress level and coincide with the data of part-through crack in various steels.

• Composites Research
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• 제12권4호
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• pp.8-16
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• 1999

본 연구는 인장하중의 방향변화에 따른 의사 등방성 복합재 적층판의 피로손상거동의 변화에 대하여 알아보았다. [0/-60/＋60]$_s$ 적층판과 [＋30/-30/90]$_s$ 적층판의 저 싸이클 피로시험을 행하였고, 재료계는 AS4/Epoxy와 AS4/PEEK를 사용하였다. [＋30/-30/90]$_s$ 적층판의 피로손상은 [0/-60/＋60]$_s$ 적층판에 비하여 아주 달랐다. AS4/Epoxy와 AS4/PEEK [＋30/-30/90]$_s$ 적층판에 발생한 층간분리의 위치가 모재의 종류에 따라 다르게 나타났다. 층간분리 진전시 측정된 변형률을 사용하여 임계 변형률 에너지 해방률을 계산하였다. 실험결과를 모드별 변형률 에너지 해방률의 제안된 계산법으로 얻어진 해석 결과와 비교한 결과, 잘 일치되었다.

• 한국윤활학회:학술대회논문집
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• 한국윤활학회 2004년도 학술대회지
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• pp.339-349
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• 2004

The method for fatigue life prediction of ball bearing is proposed applying the algorithm of contact fatigue prediction based on stress analysis. In order to do this, a series of simulation such as initial surface stress analysis, EHL analysis, subsurface stress analysis and fatigue analysis are conducted from the loading at each ball location calculated for a bearing subjected to external bearing load and contact shape function. And uniaxial fatigue tests are performed to obtain fatigue parameter of AISI 52100 steel. It was found that since stress is usually higher at the inner raceway contact than at the outer raceway contact, fatigue failure occurs on the inner raceway first. When the fatigue life calculated in the stress-based method are compared with $L_{50}$ life of L-P model, Crossland criterion for the radial load increment is similar to $L_{50}$ life and Dang Van criterion for the axial load increment is similar. In the case of EHL contact. there is no difference of fatigue life between dry contact and EHL contact, when maximum Hertz pressure exceeds 2.5GPa.