• 제목/요약/키워드: Plain fatigue

검색결과 47건 처리시간 0.022초

노치 에서의 피로 균열 발생 과 전파 에 관한 연구 (Fatigue Crack Initiation and Propagation at Notches)

  • 이강용;이택성
    • 대한기계학회논문집
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    • 제8권2호
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    • pp.141-144
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    • 1984
  • 본 연구에서는 완전 역 피로응력(completely reversed fatgue stress)를 받는 타원 노치에서 균열 발생과 전파에 대한 이론 임계 피로 한도를 응력 세기 계수 개념 을 도입하여 임의의 재질과 임으의 타원 노치 형상에 대해서 적용할 수 있도록 유도하 며 그 결과는 기존 이론보다 Frost의 실험치에 더 잘 일치함을 보이고자 한다.

철도 차축재료의 프레팅 피로거동 평가 (Evaluation of Fretting Fatigue Behavior for Railway Axle Material)

  • 최성종;권종완
    • 한국자동차공학회논문집
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    • 제15권5호
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    • pp.139-145
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    • 2007
  • Fretting is a kind of surface damage mechanism observed in mechanically jointed components and structures. The initial crack under fretting damage occurs at lower stress amplitude and lower cycles of cyclic loading than that under plain fatigue condition. This can be observed in automobile and railway vehicle, fossil and nuclear power plant, aircraft etc. In the present study, railway axle material RSA1 used for evaluation of fretting fatigue life. Plain and fretting fatigue tests were carried out using rotary bending fatigue tester with proving ring and bridge type contact pad. Through these experiments, it is found that the fretting fatigue limit decreased about 37% compared to the plain fatigue limit. In fretting fatigue, the wear debris is observed on the contact surface, and oblique cracks at an earlier stage are initiated in contact area. These results can be used as useful data in a structural integrity evaluation of railway axle.

고강도 알루미늄 합금의 Fretting Fatigue에 관한 연구 (A Study on Fretting Fatigue of High Strength Aluminum Alloys)

  • 이학선;김상태;최성종;양현태;김재경;이동석
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.168-173
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    • 2004
  • Fretting is a kind of surface degradation mechanism observed in mechanical components and structures. The fretting damage decrease in 50-70% of the plain fatigue strength. This may be observed in aircraft, automobile and nuclear power plant used in special environment and various loading conditions. In the present study, the characteristics of the fretting fatigue are investigated using the two aluminum alloy(Al2024-T3511 and Al7050-T7451). Through the experiment, it is found that the fretting fatigue strength of the Al7050-T7451 alloy decreased about 50% from the plain fatigue strength, while the fretting fatigue strength of the Al2024-T3511 alloy decreased about 45%. The tire track was widely observed in fracture surface area of oblique crack which was induced by contact pressure. These results can be the basic data to the structural integrity evaluation of aluminum alloy subjected to fretting damage.

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알루미늄 합금(AI7050-T7451)의 반복 굽힘 하중하의 프레팅 피로거동 평가 (Evaluation of Fretting Fatigue Behavior of Aluminum Alloy(A17050-T7451) Under Cyclic Bending Load)

  • 김종성;윤명진;최성종;조현덕
    • 한국기계가공학회지
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    • 제9권1호
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    • pp.25-34
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    • 2010
  • Fretting damage reduces fatigue life of the material due to low amplitude cyclic sliding and changes in the contact surfaces of strongly connected machine and structures such as bolt, key, fixed rivet and connected shaft, which have relative slip of repeatedly very low frequency amplitude. In this study, the fretting fatigue behavior of 7050-T7451 aluminum alloys used mainly in aircraft and automobile industry were evaluated. The plain fatigue test and fretting fatigue test under cyclic bending load carried out commercial bending fatigue tester and specially devised equipments to cause fretting damage. From these experimental work, the following results obtained: (1) The plain fatigue limit for stress ratio R=-l was about 151MPa. (2) In case of fretting fatigue, fatigue limit for stress ratio R=-l about 72MPa, the fatigue limit for R=0 about 81MPa, and the fatigue limit for R=0.3 about 93MPa. (3) The fatigue limit reduction rates by the fretting damage were about 52%(R=-1), 46%(R=0) and 38%(R=0.3) respectively. (4) The fatigue limit reduction rate decreased with stress ratio increase. In fretting bending test, as stress ratio increased, occurrence of initial oblique crack by fretting decreased or phased out, so that fracture surfaces were formed by plain fatigue crack occurrence, and such tendency was notable as stress amplitude increased. (5) Tire tracks and rubbed scars were observed in the fracture surface and contacted surface.

고강도콘크리트의 피로거동에 관한 실험적 연구 (Experiments for the Fatigue Behavior of High Strength Concrete)

  • 김진근;김윤용
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 1992년도 가을 학술발표회 논문집
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    • pp.161-166
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    • 1992
  • In this paper, the effect of compressive strength on the fatigue behavior of plain concrete was studied. The fatigue behavior of plain concrete in uniaxial compression is somewhat affected by the compressive strength of the concrete. Concrete cylindrical specimens(100$\times$200mm) with compressive strength of 265kg/$\textrm{cm}^2$, 530kg/$\textrm{cm}^2$ , 860kg/$\textrm{cm}^2$ and 1053kg/$\textrm{cm}^2$ were tested and analyzed on the fatigue strength, In addition to fatigue strength, the deformation characteristics of the concrete subjected to fatigue loading was investigated. The fatigue strength was decreased for the high-strength concrete. The deformation studies indicated that the irrecoverable strain in normal strength concrete is greater than that in high strength concrete.

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Glass/Epoxy 복합재료의 피로강도평가 및 피로수명예측 (The Fatigue Strength and the Fatigue Life Prediction in Plain Woven Glass/Epoxy Composite Plates)

  • 김정규;김도식
    • 대한기계학회논문집
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    • 제17권10호
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    • pp.2475-2482
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    • 1993
  • The effects of the hole size(2R) and the specimen width(W) on the fatigue strength and the fatigue life in plain woven glass/epoxy composite plates are experimentally investigated under constant amplitude tensile fatigue loading. It is shown in this study that the notch sensitivity under fatigue loading is lower than that under static loading. It can be explained by the fact that the stress concentration is relaxed by the damage developed at the boundary of circular hole. To predict the fatigue strength at a specific cycle, the modified point stress criterion represented as a function of the geometry of the specimen(2R and W) is applied. It is found that the model used in the prediction of the notched tensile strength predicts the fatigue strength with reasonable accuracy. A model for predicting the fatigue life in the notched specimen, based on the S-$N_f$, curve in the smooth specimen, is suggested.

회전굽힘 피로 하에서의 철도 차축재료 프레팅 피로거동 평가 (The Evaluation of Fretting Fatigue Behavior on Rotary Bending Fatigue for Railway Axle Material)

  • 최성종;권종완
    • 한국자동차공학회논문집
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    • 제18권2호
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    • pp.74-82
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    • 2010
  • Fretting damage can be observed in automobile and railway vehicle, fossil and nuclear power plant, aircraft etc. In the present study, railway axle material RSA1 used for evaluation of fretting fatigue life. Plain and fretting fatigue tests were carried out using rotary bending fatigue tester with proving ring and bridge type contact pad. Through these test, the following results are obtained: 1) it is found that the fretting fatigue limit of standard specimen decreased about 37% compared to the plain fatigue limit. 2) The early crack of Shinkansen type specimens initiated in contact area and final fractured below samp=214 MPa. 3) The early crack of all TGV type specimens initiated in rounded area and fractured. 4) Tire tracks and rubbed scars were observed in the oblique crack region and fatigue crack growth region of fracture surface. 5) The wear debris is observed on the contact surface, and oblique cracks at an earlier stage are initiated in contact area. These results can be used as useful data in a structural integrity evaluation of railway axle.

Degradation reliability modeling of plain concrete for pavement under flexural fatigue loading

  • Jia, Yanshun;Liu, Guoqiang;Yang, Yunmeng;Gao, Ying;Yang, Tao;Tang, Fanlong
    • Advances in concrete construction
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    • 제9권5호
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    • pp.469-478
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    • 2020
  • This study aims to establish a new methodological framework for the evaluation of the evolution of the reliability of plain concrete for pavement vs number of cycles under flexural fatigue loading. According to the framework, a new method calculating the reliability was proposed through probability simulation in order to describe a random accumulation of fatigue damage, which combines reliability theory, one-to-one probability density functions transformation technique, cumulative fatigue damage theory and Weibull distribution theory. Then the statistical analysis of flexural fatigue performance of cement concrete tested was carried out utilizing Weibull distribution. Ultimately, the reliability for the tested cement concrete was obtained by the proposed method. Results indicate that the stochastic evolution behavior of concrete materials under fatigue loading can be captured by the established framework. The flexural fatigue life data of concrete at different stress levels is well described utilizing the two-parameter Weibull distribution. The evolution of reliability for concrete materials tested in this study develops by three stages and may corresponds to develop stages of cracking. The proposed method may also be available for the analysis of degradation behaviors under non-fatigue conditions.

평직복합재의 노치강도 및 피로특성에 미치는 보조원공의 영향 (Effects of defence holes on notched strength and fatigue properties in plain woven composite)

  • 김정규;심동석;한민규
    • 대한기계학회논문집A
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    • 제21권11호
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    • pp.1965-1971
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    • 1997
  • The relaxation of stress concentration in notched members can be very significant in the improvement of notched strength and fatigue life. This paper investigated the relationship of stress concentration factor, and notched strength and fatigue life. The stress concentration factors were analyzed by FEM. Uniaxial tensile and fatigue tests were carried on plain woven composite specimens which have a main hole and two defence holes. From experimental results, the notched strength and the fatigue limit increased up to about 50% and 30% respectively due to the reduction in stress concentration. The fatigue lives predicted by Juvinall's approach were underestimated than test results and this trends were remarkable as nothed strength increased. This is because of the underestimation of a coefficient. A in S-N curve (.sigma.$_{ar}$ =A $N_{f}$ $^{B}$). Therefore, considering notched strength the coefficient A was modified. The fatigue lives by this process were agreed well with the experimental results.sults.

탄소강의 열간 연성에 미치는 저주기 피로 시기와 냉각속도의 영향 (Effects of Onset Time of Fatigue and Cooling Rate on Hot Ductility of Plain Carbon Steel)

  • 박태은;이운해;손광석;이성근;김인수;임창희;김동규
    • 대한금속재료학회지
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    • 제48권3호
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    • pp.210-217
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    • 2010
  • The effects of cooling rate and onset time of fatigue test on hot ductility of plain carbon steels containing 0.06$\sim$0.8 wt.% carbon were investigated at various temperatures. The tensile tested specimen after fatigue strain during cooling showed higher hot ductility than the specimen fatigued and tensile-strained after cooling. With a decreasing cooling rate from solutionizing temperature to test temperature, hot ductility was increased in all temperature ranges, typically in the trough region, and the minimum point of ductility moved to a lower temperature. Also, the depth and width of the trough decreased with lowering the cooling rate.