• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2004년도 추계학술대회 논문집
• /
• pp.46-49
• /
• 2004

The spider of a drum washing machine receives the repeated fatigue loadings during laundering. Although the spider is designed statically safely, it often happens fatigue failure. Therefore it requires the safe design for fatigue and needs the prediction of quantitative fatigue life. The S-N diagram for a spider material is developed by fatigue test and statistical analysis. The stresses are measured directly from strain gages on the spider. To predict the fatigue life of spider, the rainflow counting method and Miner's rule are used. The data for fatigue life are analyzed statistically. From these data, reliability estimation for fatigue life can be done and also, equivalent fatigue life can be obtained. It will be applied to make and improve to a short period for design and prototype test.

• Structural Monitoring and Maintenance
• /
• 제5권4호
• /
• pp.429-443
• /
• 2018

Fatigue is a principal failure mode for steel structures, and it is still less understood than any other modes of failure. Fatigue life estimation of metal bridges is a major issue for making cost effective decisions on the rehabilitation or replacement of existing infrastructure. The fatigue design procedures given by the standard codes are either empirical or based on nominal stress approach. Since the fatigue life estimation through field measurements is difficult and costly, more researches are needed to develop promising techniques in the fatigue analysis of bridges through Finite Element Analysis (FEA). This paper aims to develop a methodology for the Fatigue life estimation of railway steel bridge using FEA. The guidelines of IIW-1823-07 were used in the development of the methodology. The Finite Element (FE) package ANSYS and the programming software MATLAB were used to implement this methodology on an Indian Railway Standard (IRS) welded plate girder bridge. The results obtained were compared with results from published literature and found satisfactory.

• 동력기계공학회지
• /
• 제20권3호
• /
• pp.29-35
• /
• 2016

Because of the severe service environment of the large marine vessel, the fatigue strength and its evaluation play an important role in design and maintenance of marine crankshaft. The aim of this work is to investigate the probability distribution of fatigue lives in crank throw forged steel and to develop the methodology for estimation of the probabilistic design fatigue strength. Detailed studies were performed on the constant amplitude axial loading fatigue test. The experiments were controlled by stress ratio of -1 and 15Hz frequency for each stress level. The considerable variability of fatigue life was observed in each stress level under rigidly controlled constant fatigue testing conditions. The fatigue life of crank throw forged steel was well followed the log-normal and Weibull distribution. In addition, it can be used for the estimation of probabilistic design fatigue strength by using the proposed methodology.

• 대한기계학회논문집A
• /
• 제38권10호
• /
• pp.1163-1169
• /
• 2014

본 연구에서는 자동차 서스펜션 구조에 일반적으로 사용되는 용접부 형상에 대하여 굽힘 하중에 의한 피로수명을 예측할 수 있는 절차를 개발하였다. 이종 재료로 이루어진 실제 제품 용접 연결부의 피로수명 예측을 위해, 복잡한 형상의 제품을 단순화한 용접 시편을 설계하고 이에 대한 굽힘 피로 시험을 진행한 후 모멘트-피로수명(M-N) 선도를 제시하였다. 응력 집중에 의한 영향을 분석하기 위해 시편의 형상을 모델링 한 후 정적 하중에 대한 유한요소해석을 수행하여 균열 발생부의 응력을 구하고 응력-피로수명(S-N) 선도를 제시하였다. 유한요소해석을 통해 구한 응력과 이론 계산을 통해 구해준 응력을 이용하여 응력집중계수를 계산하였고, 응력집중부의 피로평가 방법 개선을 위해 보편적으로 사용되는 피로노치계수 평가법과 굽힘 피로 시험 결과를 비교 검토하였다. 그 결과, 이종 재질 용접 연결부의 정확한 피로 수명평가를 위해서는 기하형상을 고려한 피로노치계수 평가 분석뿐만 아니라 두 소재의 맞대기 용접 시편에 대한 피로 시험을 수행해 주어야 할 것으로 판단된다.

• 항공우주시스템공학회지
• /
• 제3권2호
• /
• pp.12-19
• /
• 2009

The research for the fatigue analysis is regarded greatly as important in aerospace field. Moreover, a study on the fatigue characteristic is very actively progressing. In this study, the fatigue life estimation was performed for Flaperon Joint which has FCL(fatigue critical location) of tilt-rotor UAV. The Flaperon Joint should be taken the various loads by several missions profiles of UAV. The fatigue load spectrum of Flaperon Joint is generated by the standard mission segment for the tilt-rotor UAV, and this spectrum is used for the fatigue test and analysis. The in-house fatigue analysis program is applied to calculate the fatigue life based on Stress-Life(S-N) method. The S-N curve is generated from the S-N data of Mil-Handbook by second order polynomial regression method. Moreover, the coefficient of determination is used to ensure how accuracy it has. In addition, the Goodman equation is used to consider the mean stress effect for evaluating more accurate fatigue life. Finally, the result of fatigue analysis is verified by comparing with the fatigue test result for the Flaperon Joint.

• Journal of Advanced Marine Engineering and Technology
• /
• 제25권5호
• /
• pp.1058-1064
• /
• 2001

In this paper, the development of probability distribution estimation program for fatigue crack growth lives was summarize. The probability distribution estimation program of life was developed to increase the reliability of life estimation. In this study, it is considered that the cause of scatter in fatigue crack growth data is due to material inhomogeneity. The material resistance to fatigue crack growth is modelled as a spatial stochastic process, which varies randomly along the crack path. We developed the GUI program to estimate the probability distribution and reliability using the non-Gaussian stochastic process method. This program can be used for the reliability assessment.

• 대한기계학회논문집A
• /
• 제35권4호
• /
• pp.393-400
• /
• 2011

본 연구에서는 현장의 축적된 피로 수명 시험 데이터를 바탕으로 유한요소해석(Finite Element Analysis)을 이용하여 스프링의 피로 수명 파라미터를 역 추정(Inverse Estimation)하는 연구를 수행하였다. 베이지안 접근법(Bayesian Approach)을 이용하여 불확실성 피로 수명 파라미터의 사후분포(Posterior distribution)를 구하였고, 마코프체인몬테카를로(Markov Chain Monte Carlo) 기법을 이용하여 역 추정된 파라미터의 샘플 데이터를 생성하였다. 얻어진 샘플링 데이터를 기반으로 피로 수명을 예측한 결과 신뢰 수준 내에서 실제 수명 시험 결과가 예측한 범위 내에 잘 포함되고 있음을 알 수 있었다.

• 한국자동차공학회논문집
• /
• 제20권6호
• /
• pp.100-106
• /
• 2012

Recently, the demand to acquire and improve durability performance has steadily risen in rubber components design. In design process of a rubber component, an analytical prediction is the most effective way to improve fatigue life. Existing methods of analytical estimation have mainly used an equation for fatigue life obtained from fatigue test data. However, such formula is rarely used due to costs and time required for fatigue testing, as well as randomness of rubber materials. In this paper, we describe fatigue life estimation of rubber component using only the results from a relatively simple tearing test. We estimated fatigue life of the Janggu type fatigue specimen and the automotive motor mount, and evaluated reliability of the proposed method by comparing the estimated values with actual test results.

• 한국해양공학회지
• /
• 제25권5호
• /
• pp.47-51
• /
• 2011

This paper analyzes the fatigue-life of welded joints using the notch stress approach. In the notch stress approach, the notch effects are usually approximated by introducing weld-bead parameters for the local detailed weld joints. The actual bead shape is complex and 3-dimensional. It may also greatly influence the fatigue strength. In this study, the welded shape was modeled using a 3D-scanner. The critical distance method was adopted in the evaluation of the fatigue effective notch stress for the weldments. Fatigue life tests were performed to verify the present method of fatigue life estimation for two types of welded plates with longitudinal attachments. The estimated results of the present methods were applied to the results of the experiment. The results of the analysis showed that the scatter of fatigue-life for the experimental data expressed in the nominal stress was significantly reduced by applying the effective fatigue stress of the present study.

• 한국안전학회지
• /
• 제15권4호
• /
• pp.163-169
• /
• 2000

본 연구는 노치가 있는 구조물의 피로수명 예측 평가에 대하여 연구하였다. DEN시험편에 대한 피로균열 발생수명과 피로균열 성장수명은 SIF K해석에서 유도한 식과 Paris의 균열성장 식을 사용하였다. 예측평가 결과는 일정하중 진폭 하에서의 실험적 균열성장거동과 잘 일치하는 결과를 보였다.