• 제목/요약/키워드: fatigue damages

검색결과 150건 처리시간 0.025초

해양구조물의 피로해석시 랜덤응력의 Bandwidth의 영향 (Effect of Bandwidth of Random Stresses on Fatigue Life Estimations of Offshore Structures)

  • 류정수;윤정방
    • 대한토목학회논문집
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    • 제6권2호
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    • pp.85-91
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    • 1986
  • 심해나 해상조건이 나쁜 지점에서 운영될 해양구조물의 설계시에는 파랑하중에 대한 구조물의 피로수명예측이 매우 중요하다. 본 논문에서는 랜덤파랑하중에 의해 해양구조물에 발생되는 응력의 bandwidth가 구조물의 피로수명예측 결과에 주는 영향에 대하여 연구하였다. 구조물의 동적거동해석은 비선형 점성저항력의 선형화를 통한 주파수영역해법을 사용하여 수행되었으며, 랜덤응력스펙트럼을 구하고 이를 바탕으로 피로해석을 수행하였다. 피로손상의 예측을 위한 랜덤응력 cycle의 산정은 narrow band cycle 산정법과 함께 wide band process 에 대하여 더 적정한 rainflow cycle 산정법을 사용하였다. 수심이 다른 지점에 위치한 2개의 구조물을 택하여 예제해석을 수행하였으며, 두 응력 cycle 산정법에 의해 얻은 피로해석 결과들을 비교하고 응력의 bandwidth의 영향을 분석하였다.

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레일의 표면결함크기에 따른 구름접촉수명평가 (Rolling Contact Fatigue Analysis According to Defect Size on Rail)

  • 서정원;권성태;이동형;권석진
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2011년도 정기총회 및 추계학술대회 논문집
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    • pp.637-642
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    • 2011
  • Rails are subjected to damage from rolling contact fatigue, which leads to defects such as cracks. Rolling contact fatigue damages on the surface of rail such as head check, squats are one of growing problems. Another form of rail surface damage, known as "Ballast imprint" has become apparent. This form of damage is associated with ballast particles becoming trapped between the wheel and the surface of rail. These defects are still one of the key reasons for rail maintenance and replacement. In this study, we have investigated whether the ballast imprint is an initiator of head check type cracks and effect of defect size using Finite element analysis. The FE analysis were used to investigate stresses and strains in subsurface of defects according to variation of defect size. Based on loading cycles obtained from FE analysis, fatigue analysis for each point was carried out.

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STS316L용접재의 표면파에 의한 잔류응력 측정과 균열진전시의 음향방출특성 (Residual Stress Measurement by L$_{CR}$ Wave and Acoustic Emission Characteristics from Fatigue Crack Propagation in STS316L Weldment)

  • 남기우;박소순;안석환
    • 한국해양공학회지
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    • 제17권1호
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    • pp.47-54
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    • 2003
  • In this study, the residual stress and the acoustic emission Charactreistics from fatigue crack propagation were investigated, bused on the welded material of STS316L. The residual stress of welding locations could be evaluated by ultrasonic parameters, such as L$_{CR}$ wave velocity and L$_{CR}$ wave frequency; the residual stress between base metal and weld metal was evaluated. In the fatigue tests, three types of signals were observed, regardless of specimen condition, base metal, and weld metal. Based on NDE analysis of AE signals by the time-frequency analysis method, it should also be possible to evaluate, in real-time, the crack propagation and final fracture process, resulting from various damages and defects in welded structural members.

풍력터빈 허브의 피로 강도 해석에 대한 연구 (A Study on the Fatigue Strength Analysis of Hub in a Wind Turbine)

  • 고장욱;김향기;안경민;최원호
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2006년도 추계학술대회
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    • pp.265-268
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    • 2006
  • Performed fatigue strength analysis for Hub to get the targeted service life of 20 years. ANSYS is used to analysis. The major structure of bearing which connect the hub and blades is modeled using the element of LINK10. To represent the stiffness of LINK10 element, initial strain and diameter of LINK10 element is applied. Prior to calculating the fatigue damages, the influence matrix is extracted from the unit loads. The target service life of 20 years is achieved from the Analysis results.

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형상이 다른 브레이크 패드의 구조 및 피로해석을 통한 내구성 연구 (Durability Study through Structural and Fatigue Analyses of Brake Pads with Different Configurations)

  • 한문식;조재웅
    • 한국자동차공학회논문집
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    • 제22권6호
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    • pp.128-133
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    • 2014
  • In this study, Two kinds of pad models with different configurations as the part of brake system are investigated by structural and fatigue analyses. As the maximum equivalent stress of model 2 becomes higher to the extent of 60% than that of model 1, model 2 can endure more load than model 1. In cases of two kinds of models, the maximum fatigue life at 'Sample history' becomes longer 60 times than 'SAE bracket history' and this life in case of 'SAE transmission' becomes longer 3.5 times than the case of 'SAE bracket history'. Maximum fatigue damages in cases of 'SAE bracket history', 'SAE transmission' and 'Sample history' at model 1 become higher than model 2. Model 2 is thought to have more fatigue durability than model 1. These study results can be effectively utilized with the design of brake pad by anticipating and investigating prevention and durability against its fatigue damage.

부유체 대표 평균 위치를 적용한 계류 라인의 시간 영역 피로 해석 효율화에 대한 연구 (Study on Efficient Time Domain Fatigue Analysis of Mooring Chain by Representative Mean Position)

  • 박정문;김유일;김정환
    • 한국해양공학회지
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    • 제32권5호
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    • pp.333-340
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    • 2018
  • This paper addresses the concept of the representative mean position, which was devised to improve the numerical efficiency of a time domain fatigue analysis of a mooring chain. To investigate the influence of an artificial offset of the floater on the fatigue of the mooring chain, a parametric study was performed on the moored FPSO under various combinations of offsets and environmental conditions. Tension time histories were calculated using the de-coupled analysis method, and fatigue damages were calculated to determine the influence of the offset. The parametric study was extended to a more realistic case to determine the actual effect of the representative mean position, where a comparison was made between the two different analysis results, one using the representative mean position and the other one using the actual mean position. It was confirmed that the application of the representative mean position guaranteed the conservatism of the fatigue damage with the enhanced numerical efficiency in the time domain fatigue analysis.

고집적용 구리배선의 electromigration 및 thermal fatigue 연구 (Electromigratoin and thermal fatigue in Cu mentallization for ULSI)

  • 김영후;박영배;;;주영창
    • 마이크로전자및패키징학회지
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    • 제12권1호
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    • pp.53-58
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    • 2005
  • 구리 배선에서의 신뢰성 평가를 위해 직류전류와 교류전류를 각각 인가하였을 때의 파손 발생을 분석해 보았다. 직류 전류에서는 electromigration 현상이 발생하는데, 높은 전류 밀도와 온도에서 더욱 빠르게 파손이 진행되었으며, 실험을 통해 구한 활성화 에너지와 전류밀도 의존지수는 각각 0.96eV와 4의 값을 갖는 것으로 나타났다. 교류 전류에서는 열 피로 현상이 발생하였는데, 높은 주파수와 ${\Delta}$T가 클수록 파손이 심하게 진행되었다. 집합 조직에 따른 failure morphology분석 결과, (100)grains에서는 결함이 넓게 성장하여 facetted grains가 되지만 (111)에서는 배선의 두께 방향으로 성장하여 빠르게 단선을 유발하는 것으로 나타났다.

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접촉하중형태에 따른 복합재의 거동변화 (Behavior of Woven-glass/Epoxy Composites after Impact Loading)

  • 이재준;김병식;황성식;김태우;김찬묵
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2002년도 춘계학술발표대회 논문집
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    • pp.53-56
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    • 2002
  • External low-velocity impact loadings onto the composites cause reduction of stiffness and/or strength. The reductions indicate that internal(external) damages were developed within the composites. These damages could be matrix cracking, fiber/matrix debonding, or delamination between layers. In previous studies, damage evaluation have been done by applying secondary mechanical loading such as buckle-driven compressive, or fatigue, or flexural loadings. An evaluation method by applying indentation loadings on the composites was proposed. The load-displacement curves obtained from the indentation testing provided the extent of damages within the composites due to impact loadings.

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피로균열의 지연거동에 따른 수명예측 및 비파괴평가 (Life Prediction by Retardation Behavior of Fatigue Crack and its Nondestructive Evaluation)

  • 남기우;김선진
    • 한국해양공학회지
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    • 제13권3호통권33호
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    • pp.36-48
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    • 1999
  • Fatigue life and crack retardation behavior after penetration were experimentally examined using surface pre-cracked specimens of aluminium alloy 5083. The Wheeler model retardation parameter was used successfully to predict crack growth behavior after penetration. By using a crack propagation rule, the change in crack shape after penetration can be evaluated quantitatively. Advanced, waveform-based acoustic emission (AE) techniques have been successfully used to evaluate signal characteristics obtained form fatigue crack propagation and penetratin behavior in 6061 aluminum plate with surface crack under fatigue stress. Surface defects in the structural members are apt to be origins of fatigue crack growth, which may cause serious failure of the whole structure. The nondestructive analysis on the crack growth and penetration from these defects may, therefore, be one of the most important subjects on the reliability of the leak before break (LBB) design. The goal of the present study is to determine if different sources of the AE could be identified by characteristics of the waveforms produced from the crack growth and penetration. AE signals detected in four stages were found to have different signal per stage. With analysis of waveform and power spectrum in 6061 aluminum alloys with a surface crack, it is found to be capabilities on real-time monitoring for the crack propagation and penetration behavior of various damages and defects in structural members.

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충격하중을 받은 CFRP 적층판의 손상거동과 잔류굽힘피로강도 (Damage Behavior and Residual Bending Fatigue Strength of CFRP Composite Laminates Subjected to Impact Loading)

  • 임광희;양인영
    • 대한기계학회논문집A
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    • 제20권6호
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    • pp.1836-1842
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    • 1996
  • In this paper, static and fatigue bending strengths of CFRP(carbon fiber reinforced plastic laminates having impact damage(FOD) are evaluated. Composite laminates used for this experiment are CF/EPOXY and CF/PEEK orthotropy laminated plates, which have two-interfaces[${0^0}_4{90^0}_4}$]$_sym$. A steel ball launched by the air gun colides against CFRP laminates to generate impact damages. The damage growth during bending fatigue test is observed by the scanning acoustic microscope(SAM). When the impacted side is compressed, the residual fatigue bending strength of CF/PEEK specimen P is greater that that of CF/EPOXY SPECIMEN B. On the other hand, when the impacted side is in tension, the residual fatigue bending strength of CF/PEEK speicemen P is smaller than that of CF/EPOXY specimen B. In the case of impacted-side compression, fracture is proposed from the transverse crack generated near impact point. On the other hand, fracture is developed toward the impact point from the edge of interface-b delamination in the case of impacted-side tension.