• Title/Summary/Keyword: 피로 손상 해석

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Reliability Analysis of Fatigue Truck Model Using Measured Truck Traffic Statistics (통행차량 특성을 반영한 강교량 피로설계트럭의 피로파괴 신뢰도해석)

  • Shin, Dong Ku;Kwon, Tae Hyung;Park, Young Suk
    • Journal of Korean Society of Steel Construction
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    • v.19 no.2
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    • pp.211-221
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    • 2007
  • A structural reliability analysis of fatigue truck model for fatigue failure of highway steel bridges was performed by applying the Miner's fatigue damage rule expressed as a function of various random variables affecting fatigue damage. Among the variables, the statistical parameters for equivalent moment, impact factor, and loadometer were obtained by analyzing recently measured domestic traffic data, whereas the parameters on fatigue strength, girder distribution factor, and headway factor of the measured data available in the literature were used. The effects of various fatigue truck models, fatigue life, ADTT, fatigue detail category, loadometer, and gross vehicle weight of fatigue truck on the reliability index of fatigue damage were analyzed. It is expected that the analytical results presented herein can be used as a basic background material in the calibration of both fatigue design truck and fatigue load factor of LRFD specification.

A Study on Prediction of Fatigue Damage Crack Growth for Stiffener Bonded Composite Laminate Panel (보강재 본딩접합 복합재 적층판구조 피로손상 균열진전 수명예측에 대한 연구)

  • Kwon, Jung-Ho;Jeong, Seong-Moon
    • Composites Research
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    • v.26 no.2
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    • pp.79-84
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    • 2013
  • The prediction and analysis procedure of fatigue damage crack growth life for a stiffener bonded composite laminate panel including center hole and edge notch damage, was studied. It was performed on the basis of fatigue damage growth test results on a laminated skin panel specimens and the analysis results of stress intensity factor for the stiffener bonded composite panel. According to the comparison between experimental test and prediction results of fatigue damage growth life, it was concluded that the residual strength and damage tolerance assessment can be carried out along to the edge notch crack growth.

Fatigue Behavior and Probabilistic Fatigue Analysis of Concrete Offshore Structures (콘크리트 해양구조물(海洋構造物)의 피로거동(疲勞擧動)과 확률론적(確率論的) 피로해석(疲勞解析))

  • Oh, Byung Hwan;Kim, Jee Sang
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.8 no.3
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    • pp.31-41
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    • 1988
  • Recently, the offshore structures are increasingly constructed to explore the natural resources. These offshore structures are to be designed to resist the repetitive wave forces. A probabilistic method for the fatigue analysis of offshore concrete structures is presented in this study. The present spectral fatigue analysis calculates wave forces first and then the transfer functions for unit waves from which stress spectra are determined. The calculated fatigue stresses may then be used to evaluate the fatigue damage of concrete structures. A simplified model for the estimation of fatigue damage of the structures, which employs only the probabilistic moments of the peak stress distribution without direct integration, is also proposed. The present study allows more realistic fatigue analysis of offshore concrete structures.

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Fatigue Damage Analysis of a Low-Pressure Turbine Blade (저압터빈 블레이드의 피로손상 해석)

  • Youn, Hee Chul;Woo, Chang Ki;Hwang, Jai Kon
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.39 no.7
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    • pp.713-720
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    • 2015
  • The sizes of the final blades of a low-pressure (LP) steam turbine have been getting larger for the development of high-capacity power plants. They are also larger than the other blades in the same system. As a result, fatigue damage is caused by a large centrifugal force and a low natural frequency of the blade. Recently, many failure cases have been reported due to repeated turbine startups and their prolonged use. In this study, the causes and mechanism of failure of a LP turbine blade were analyzed by using a finite element method to calculate the centrifugal force, the natural frequency of a stress-stiffening effect, and the harmonic response. It was observed that the expected fatigue damage position matched the real crack position at the airfoil's leading edge, and an equivalence fatigue limit approached a notch fatigue limit.

Fundamental research for the development of full spectral-atigue analysis software to consider hydroelasticity effects (유탄성 효과를 고려한 완전통계 피로해석 프로그램 개발을 위한 기초 연구)

  • Park, Jun-Bum
    • Journal of Advanced Marine Engineering and Technology
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    • v.39 no.9
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    • pp.903-910
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    • 2015
  • The purpose of this research is to develop a full-spectral fatigue analysis program, based on rigid-body ship motion analysis, in order to perform a full-spectral fatigue analysis that considers hydroelasticity effects. To gain credibility, fatigue analysis results of two ship types, performed by the developed program, were compared with those of a classification society, and it was found that both are identical. Full-spectral fatigue analysis considering hydroelasticity effects would be developed in further studies by including flexible-body ship motion analysis results and by supplementing the developed program with a wide-band fatigue damage model.

Damage Tolerance Assessment for Fatigue-Critical Locations of Wing Structure of Aged Aircraft (장기운영 항공기 주익 구조물 피로임계부위의 손상허용평가)

  • Chun, Young-Cheol;Kim, Won-Cheol;Jin, Ji-Won;Chung, Tae-Jin;Kang, Ki-Weon
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.41 no.2
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    • pp.129-136
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    • 2017
  • This study aims to assess the damage tolerance of the wing structure of aged aircraft with long-term service through the fatigue crack growth analysis and tests. For the fatigue-critical locations (FCL) W2 and W4 in the wing structure, the fatigue stress spectrum was derived based on a previous study. Thereafter, a crack propagation analysis for the FCLs was conducted using the commercial software $NASGRO^{TM}$. The algorithm for the fatigue stress spectrum was verified. Fatigue crack growth tests were then performed for two types of specimens: Type #1 was extracted from the wing structure of aged aircraft, and Type #2 was made of the same material as the wing structure. By comparing the experimental results of these specimens, we assessed the damage tolerance of the wing structure of aged aircraft with service time.

Vibration Fatigue Analysis of Spot Welded Component considering Change of Stiffness due to Fatigue Damage (피로손상의 누적에 따른 강성변화를 고려한 점용접부의 진동피로해석)

  • Kang, Ki-Weon
    • Journal of the Korea Convergence Society
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    • v.5 no.1
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    • pp.1-8
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    • 2014
  • The purpose of this paper was to evaluate the fatigue life to apply the vibration fatigue analysis considering the stiffness change of the spot welding due to fatigue damage accumulation. For this, the mechanical and fatigue properties of base and spot welded standard specimens were obtained through the tensile and constant amplitude fatigue test. The transfer function of the spot-welded structure was obtained from the frequency response analysis and fatigue analyisis was performed under the condition of PSD=0.11. A vibration fatigue analysis that considered changes in the frequency response due to the fatigue damage that is, failure of some wleding point was conducted on spot-welded structure. The fatigue life of the spot-welded structure was determined by combining the transfer function, the S-N curve of the tensile-shear spot-welded joint and the input PSD.

Reliability Analysis for Fatigue Damage of Steel Bridge Details (강교 부재의 피로손상에 대한 신뢰성 해석)

  • Park, Yeon Soo;Han, Suk Yeol;Suh, Byoung Chal
    • Journal of Korean Society of Steel Construction
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    • v.15 no.5 s.66
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    • pp.475-487
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    • 2003
  • This study developed an analysis model of estimating fatigue damage using the linear elastic fracture mechanics method. Stress history occurring to an element when a truck passed over a bridge was defined as block loading and crack closure theory explaining load interaction effect was applied. Stress range frequency analysis considering dead load stress and crack opening was done. Probability of stress range frequency distribution was applied and the probability distribution parameters were estimated. The Monte Carlo simulation of generating the probability various of distribution was performed. The probability distribution of failure block numbers was obtained. With this the fatigue reliability of an element not occurring in failure could be calculated. The failure block number divided by average daily truck traffic remains the life of a day. Fatigue reliability analysis model was carried out for the welding member of cross beam flange and vertical stiffener of steel box bridge using the proposed model. Consequently, a 3.8% difference was observed between the remaining life in the peak analysis method and in the proposed analysis model. The proposed analysis model considered crack closure phase and crack retard.

Damage Assessment of Bridges by Overloaded Vehicles (과적차량에 의한 교량의 손상평가)

  • Bang, Myung Suk
    • Journal of the Korea institute for structural maintenance and inspection
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    • v.2 no.1
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    • pp.81-88
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    • 1998
  • 과적차량의 통행에 의한 교량구조물의 손상도를 평가하는 방법의 개발이 매우 활발하다. 본 연구에서는 과거 15년동안 통행한 교통데이타를 분석하고, 이 데이타를 근거로 교량의 손상도를 분석한다. 차량의 분류는 4종으로 대표하여 차량하중을 분석하였으며 해석시에는 이를 대표하는 2종을 사용하였다. 3차원해석을 통하여 구한 영향면을 이용하여 부재력을 계산하고 이를 이용하여 등가응력범위를 구한다. 이 결과는 모형실험을 통하여 구한 피로결과와 비교하였다. 분석결과 설계하중을 초과하는 과적차량이 교량에 미치는 손상정도는 적은 통행빈도에도 불구하고 매우 큼을 알 수 있고, 이러한 실제교통량의 분석을 통한 교량의 손상평가방법은 과적차량에 의한 교량손상정도를 유용하게 평가할 수 있다.

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Analysis of Fatigue Truck Model for LRFD Code (LRFD 설계기준(안) 피로설계트럭 모형 분석)

  • Cho, Eun Young;Shin, Dong Ku
    • Journal of Korean Society of Steel Construction
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    • v.21 no.3
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    • pp.331-342
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    • 2009
  • A reliability analysis of the fatigue failure of highway steel bridges was performed by applying the Miner's fatigue damage rule for the fatigue design truck proposed for the LRFD code and for the current DB 24 truck. The limit state function for fatigue failure is expressed as a function of various random variables that affect fatigue damage. Among these variables, the statistical parameters for the equivalent moment, the impact factor, and the loadometer were obtained by analyzing recently measured domestic traffic data, and the parameters for the fatigue strength, the girder distribution factor, and the headway factor were obtained from the measured data reported in literature. Based on the reliability analysis, the fatigue truck model for the LRFD code was proposed. After applying the proposed fatigue truck to the LRFD code, 16 composite plate and box girder bridges were designed based on the LRFD method, and the LRFD design results for the fatigue limit state were compared with those by the current KHBDC.