• 콘크리트학회논문집
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• 제22권2호
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• pp.179-186
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• 2010

철근과 콘크리트의 부착은 콘크리트와 철근의 일체거동에 의한 안전성 확보를 위해서도 필요하지만, 적정수준의 연성을 확보하여, 부재의 거동을 조절하기 위해서도 필요하다. 현재까지 반복하중 하에서의 부착응력-슬립관계에 대한 연구는 진행되어 왔으나, 철근 부식이 이루어진 경우의 반복하중 하에서의 부착응력-슬립관계에 대한 연구는 거의 없는 실정이다. 따라서 이 연구에서는 부식된 철근의 부착 실험을 통하여 단조하중과 반복하중 하에서의 부식률에 따른 부착응력-슬립 관계를 살펴보았다. 실험결과로부터 철근 부식은 할열 균열이 발생하기 전까지는 단조하중에서의 부착강도를 증가시키는 것을 확인하였다. 그리고 반복하중 횟수와 반복하중 하에서의 슬립 및 잔류슬립을 이중로그스케일로 도시한 결과, 철근 부식이 있는 경우에도 철근 부식이 없는 경우와 마찬가지로 선형 관계임을 확인하였다. 그리고 부식에 의한 균열이 발생하지 않는 한, 철근 부식이 반복하중 재하 이후의 부착강도 및 부착강도에서의 슬립 등 부착 특성에 영향을 미치지 않는 것도 알 수 있었다. 마지막으로, 철근 부식으로 인한 균열이후에서의 응력수준에 따른 피로수명은 급격히 감소하는 것을 확인하였다. 이 연구에서 제시하는 철근 부식을 고려한 반복하중 하에서의 부착응력-슬립의 관계는 철근콘크리트 구조물의 내구수명 예측 시 유용하게 사용될 수 있을 것으로 사료된다.

• 한국해양공학회지
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• 제11권4호
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• pp.61-75
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• 1997

The social demand urges us to use some equipments and structures in high temperature environment. By this occasion, the necessity of studying the fatigue crack growth is an important aspect of new materials. However, the present situation is rarely to accumulate the fatigue data. Especially, 1Cr-1Mo-0.25V steel and 304 stainless steel have been increased to be used under the severe condition of high temperature. And so, the fatigue estimation of those materials is important and appropriate. Fatigue tests have been carried out to examine the crack initiation, growth behaviour for the small fatigue crack of 1Cr-1Mo-0.25V steel and 304 stainless steel at room temperature and 538^{\circ}C$. The remote measurement system which has many merits of checking and saving the image for detailed examination was applied to closely detect the crack length. Generally, the fatigue crack initiated in the form of multiple cracks and grew each other. And then it coalesced to become a major crack. The major crack governed the rest of the fatigue life. In the growing process, each peripheral cracks interact and grow for a certain period. After then, it coalesced and fractured. On the basis of the above experimental data for the small crack, a simulation program was developed to predict the residual life time and to estimate the integrity of machine elements and structures. At the same time, the simulation was extended to 1Cr-1Mo-0.25V steel. The simulation results have shown a good agreement to those of the experimental ones for both materials of 1Cr-1Mo-0.25V steel and 304 stainless steel with small cracks. The NASCRAC has applied to compare the fatigue life with the experimental results. And so, it can be said that the simulation program is valuable tools to the industrial fields.

• 대한토목학회논문집
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• 제9권1호
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• pp.1-10
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• 1989

교량에 발생하는 응력이력은 교통류(traffic flow)의 성질에 따라 변하며, 교통류는 차종규성율, 차량중량, 차두시간간격(headway time)등에 따라 다르기 때문에 교량과 같은 휨부재에서 교통류에 의한 응력이력을 추정하기 위해서는 통계적 해석이 필요하며, 이것을 파괴역학에 적용함으로서 구조물의 잔존수명을 추정할 수 있을 것이다. 본 연구에서는 1)교통류의 불규칙성을 해석하기 위하여 차종구성율, 차량중량, 차두시간간격등을 통계적으로 분석 2)실제 교량에서의 응력이력의 측정과 분석 3)차종구성율, 차량중량, 차두시간간격을 확률변수로한 Monte Carlo 시뮬레이션에 의한 응력이력의 재현 4)실측 응력이력과 시뮬레이션한 응력이력의 비교 5)대상교량의 감소계수(reduction factor)의 계산 6)지간길이 변화에 따른 응력범위발생빈도의 비교등을 행하였다. 그 결과 시뮬레이션에 의한 응력이력 추정방법과 구조물의 잔존피로수명 예측에 필요한 기본적인 모형화된 응력이력을 제시하였다.

• 한국자동차공학회논문집
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• 제13권5호
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• pp.142-151
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• 2005

To predict the fatigue life of the Hub Bearing Unit(HBU), preload effect and initial axial clearance have to be considered. Various theory and equations for the HBU design used in the passenger car are well developed in many literatures. But most design hand book for bearings or bearing catalogues do not consider the initial axial clearance and preload effect. So there are limits and difficulties to use those data in actual bearing design. To consider the preload effect and initial axial clearance, complex elliptic integrals and nonlinear equations are involved. These equations are difficult to solve during the design process. In order to solve these problems effectively, a program is developed to solve these equations reliably and to help the designer in obtaining the performance data of the HBU such as load distribution, maximum contact stress and fatigue life. The preprocessor of the program helps users to prepare the input data through a dialog box and the post processor makes graphical presentation of the result. In this paper, theoretical and numerical background for the prediction of the fatigue life of the HBU is explained. A simple example is presented to show the usefulness of developed program.

• 한국산학기술학회논문지
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• 제20권10호
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• pp.296-302
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• 2019

본 연구에서는 이수순환시스템 핵심 장비 중의 하나인 셰일 셰이커 시작품의 핵심 부품을 선정하여 기초 내구성 평가를 수행하고 분석하였다. 기초 내구성 평가의 경우, 바이브레이터 모터(이하, 모터)가 장시간 운전에 따른 모터 베어링의 수명과 모터로 부터 유발된 진동에 의한 지지 스프링의 강성저하가 장비의 내구성에 적지 않은 영향을 미칠 수 있을 것이란 가정을 두었다. 모터 연속운전에 있어, 전 초기 진동 가속도의 P-P 수준은 0.72 g 수준 이었으나 운전 100 시간 경과 후, 진동 가속도의 P-P 수준은 1.26 g로 급격히 상승함을 볼 수 있었으며, 진동 상승의 원인분석을 위해 볼 결함주파수 분석기법을 통해 베어링 결함을 추정할 수 있었다. 또한, 셰일 셰이커의 가진 조건을 피로내구시험에 적용하여 시험 2,000 시간 경과 시, 스프링의 강성이 약 3.78 % 감소함을 확인 할 수 있었다. 향후 본 연구는 스프링 강성의 저하가 셰일 셰이커의 입자제거 효율이 미치는 영향 분석과 그에 따른 고장수명에 예측에 관한 후속 연구를 수행 할 예정이다.

• 한국정밀공학회지
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• 제19권6호
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• pp.166-175
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• 2002

Low cycle fatigue tests are performed on the HSLA steel that be developed for a submarine material. The relation between strain energy density and numbers of cycles to failure is examined in order to predict the low cycle fatigue life of HSLA steel. The cyclic properties are determined by a least square fit techniques. The life predicted by the strain energy method is found to coincide with experimental data and results obtained from the Coffin-Manson method. Also the cyclic behavior of HSLA steel is characterized by cyclic softening with increasing number of cycle at room temperature. Especially, low cycle fatigue characteristics and microstructural changes of HSLA steel are investigated according to changing tempering temperatures. In the case of HSLA steel, the $\varepsilon$-Cu is farmed in $550^{\circ}C$ of tempering temperature and enhances the low cycle fatigue properties.

• 한국군사과학기술학회지
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• 제16권5호
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• pp.631-638
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• 2013

The probabilistic fatigue life analysis is one of the common methods to account the uncertainty of parameters on the structural failure. Frequently, the Bayesian approach has been demonstrated as a proper method to show the uncertainty of parameters. In this work, the application of probabilistic fatigue life prediction method for the aircraft structure was studied. This effort was conducted by using the PoF(Probability of Failure) based on Bayesian approach. Furthermore, numerical example was carried out to confirm the validation of the suggested approach. In conclusion, it was shown that the Bayesian approach can calculate the probabilistic fatigue lives and the quantitative value of PoF effectively for the aircraft structural component. Moreover the calculated probabilistic fatigue lives can be utilized to determine the optimized inspection period of aircraft structures.

• 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.

• 대한기계학회논문집A
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• 제25권5호
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• pp.874-882
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• 2001

The static and fatigue tests have been carried out to verify the validity of a generalized residual strength degradation model. And a new method of parameter determination in the model is verified experimentally to account for the effect of tension-compression fatigue loading of spheroidal graphite cast iron. It is shown that the correlation between the experimental results and the theoretical prediction on the statistical distribution of fatigue life by using the proposed method is very reasonable. Furthermore, it is found that the correlation between the theoretical prediction and the experimental results of fatigue life in case of tension-tension fatigue data in composite material appears to be reasonable. Therefore, the proposed method is more adjustable in the determination of the parameter than maximum likelihood method and minimization technique.

• Journal of Welding and Joining
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• 제31권6호
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• pp.32-36
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• 2013

The large-scale structures have the possibility that there are defects such as cracks due to stress concentration caused by geometric discontinuities in the structure. In this respect, the assessment of fatigue life and the development of structural health monitoring(SHM) are very important. Fatigue design of structure is typically accomplished either using a set of stress cycle (S-N) data obtained from fatigue tests or using the fracture mechanics approach. The stress intensity factor(SIF) is required for the estimation of fatigue crack propagation life from the linear elastic fracture mechanics (LEFM) perspective. In this study, Macro Fiber Composie(MFC) sensor for the measurement of SIF of two dimensional cracks is used. The SIF based on the piezoelectric constitutive law and fracture mechanics are calculated. The measured values of the SIF are later used for the prediction of the crack propagation life. In this study, the measured value of the SIF and the fatigue life are compared with the theoretical results.