• 제목/요약/키워드: Fatigue load

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변동 하중을 받는 구조물에서의 피로 파손 해석 (The Analysis of Fatigue Damage in Structure under Variable Load)

  • 한문식;조재웅
    • 한국자동차공학회논문집
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    • 제12권4호
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    • pp.85-93
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    • 2004
  • The variable fatigue load is simulated in this study, The stability and the life of the material are analyzed theoretically by the program of Ansys workbench. These results are successfully applied to the practical structures to predict the prevention of fracture and the endurance, The life and the damage on the every part of the fatigue specimen can be predicted. As the available lives are compared for every loading variation, the rainflow and damage matrix results can be helpful in determining the effects of small stress cycles in any loading history. The rainflow and damage matrices illustrate the possible effects of infinite life. The safety and stability of fatigue specimen according to the variable load can be estimated by using the results of this study.

Special cases in fatigue analysis of wind turbines

  • Gunes, Onur;Altunsu, Elif;Sari, Ali
    • Wind and Structures
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    • 제32권5호
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    • pp.501-508
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    • 2021
  • The turbine industry demands a reliable design with affordable cost. As technological advances begin to support turbines of huge sizes, and the increasing importance of wind turbines from day to day make design safety conditions more important. Wind turbines are exposed to environmental conditions that can affect their installation, durability, and operation. International Electrotechnical Commission (IEC) 61400-1 design load cases consist of analyses involving wind turbine operating conditions. This design load cases (DLC) is important for determining fatigue loads (i.e., forces and moments) that occur as a result of expected conditions throughout the life of the machine. With the help of FAST (Fatigue, Aerodynamics, Structures, and Turbulence), an open source software, the NREL 5MW land base wind turbine model was used. IEC 61400-1 wind turbine design standard procedures assessed turbine behavior and fatigue damage to the tower base of dynamic loads in different design conditions. Real characteristic wind speed distribution and multi-directional effect specific to the site were taken into consideration. The effect of these conditions on the economic service life of the turbine has been studied.

로터 블레이드 결빙에 의한 타워 피로하중 평가 (Evalulation of the Tower Fatigue Loads by Ice Formation on Rotor Blades)

  • 김정기;박선호;방조혁;정종훈;김상덕;류지윤
    • 풍력에너지저널
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    • 제5권1호
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    • pp.43-49
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    • 2014
  • Primarily, tower loads of a wind turbine arise from aerodynamic effect and a top head mass. But sometime asymmetric loads of rotor also affect on the tower loads. Especially ice formation on two blades out of three causes the asymmetric loads, because the ice formation on blades lead to large rotating mass imbalance. This rotating mass imbalance of rotor affects tower fatigue loads. So design load cases of ice formation on blade should be considered in the fatigue design loads of the tower according to GL guideline 2010. This paper describes the change of tower fatigue loads following increase of tower height in the condition of ice formation. Finally, the optimal operation strategy is examined in order to reduce tower fatigue design loads.

불규칙 진동하중을 받는 쇽 타워의 피로수명을 고려한 점용접 위치 최적설계 (A Study on Optimal Spot-weld Layout Design of the Shock Tower Structure Considering Fatigue Life under Random Vibration Load)

  • 이용훈;이승윤;배복수;임홍재
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2011년도 춘계학술대회 논문집
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    • pp.538-543
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    • 2011
  • In this paper, optimal spot weld layout design of the shock tower structure is performed for increasing fatigue life of spot weld and fatigue life of shock tower simultaneously. To predict the fatigue life, linear static analysis is conducted then fatigue analysis is performed by applying random vibration load. To optimize the spot weld layout, design variables that have an effect on spot weld fatigue life are selected. Based on the DOE table, spot weld fatigue analysis is conducted. Finally, response surface model is made from fatigue analysis results and optimized spot weld layout model which increases fatigue life of sport weld and fatigue life of shock tower is determined.

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Assessment of load carrying capacity and fatigue life expectancy of a monumental Masonry Arch Bridge by field load testing: a case study of veresk

  • Ataei, Shervan;Tajalli, Mosab;Miri, Amin
    • Structural Engineering and Mechanics
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    • 제59권4호
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    • pp.703-718
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    • 2016
  • Masonry arch bridges present a large segment of Iranian railway bridge stock. The ever increasing trend in traffic requires constant health monitoring of such structures to determine their load carrying capacity and life expectancy. In this respect, the performance of one of the oldest masonry arch bridges of Iranian railway network is assessed through field tests. Having a total of 11 sensors mounted on the bridge, dynamic tests are carried out on the bridge to study the response of bridge to test train, which is consist of two 6-axle locomotives and two 4-axle freight wagons. Finite element model of the bridge is developed and calibrated by comparing experimental and analytical mid-span deflection, and verified by comparing experimental and analytical natural frequencies. Analytical model is then used to assess the possibility of increasing the allowable axle load of the bridge to 25 tons. Fatigue life expectancy of the bridge is also assessed in permissible limit state. Results of F.E. model suggest an adequacy factor of 3.57 for an axle load of 25 tons. Remaining fatigue life of Veresk is also calculated and shown that a 0.2% decrease will be experienced, if the axle load is increased from 20 tons to 25 tons.

수평축 풍력발전 시스템용 복합재 회전날개의 피로수명 설계에 관한 연구 (A Study on Fatigue Life Design for Horizontal Axis Wind Turbine Composite Blade)

  • 공창덕;방조혁;정종철;강명훈;정석훈;류지윤;김기범
    • 한국추진공학회지
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    • 제3권3호
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    • pp.47-52
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    • 1999
  • 피로시험은 구조설계에 있어서 필수적인 과정으로서, 구조물의 요구수명 만족여부를 판단하기 위해 수행된다. 본 연구에서는 750㎾급 수평축 풍력발전 시스템용 복합재 회전날개가 요구수명 20년이상 안전하게 운용되어질 수 있는지에 대한 검토를 수행하였다. tan Bond의 실험식과 S-N선형 손상 방법을 사용하여 요구 피로강도를 계산하였으며, 설계된 복합재 회전날개의 유한요소 해석 결과와 비교하기 위해 측정하중 스펙트럼과 Spera의 피로하중 실험식을 이용하여 회전날개에 적용시킬 피로하중을 계산하였다. 계산된 피로하중에 대한 유한요소 해석을 수행하여 검토한 결과, fan Bond의 실험식을 이용하여 예측한 최대 요구 피로강도보다 낮은 범위에 있음을 확인하였다.

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플라스틱 기어의 피로수명 평가 및 수명 예측 (Fatigue Life Evaluation of the Plastic Gear)

  • 정태형;강성규;하영욱
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2005년도 춘계학술대회 논문집
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    • pp.239-245
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    • 2005
  • Through the fatigue test of plastic gears using polyacetal polymer, this research aims at providing basic data for not only specifying operation conditions of plastic gears, but also designing dimensions of plastic gears with giving fatigue life and the estimated equation of fatigue life of plastic gears. That is, from the fatigue life curves, the estimated equation of fatigue life of plastic gears is taken out. For the estimated equation of fatigue life of plastic gears, this research provides two test methods; one is preserving non-limited temperature of tooth flank, the other is preserving limited temperature of tooth flank. As results, how the temperature of tooth flank affects the fatigue life is shown. In addition, based on the endurance limit, the essential factors of the unit load and K-factor are determined, which are needed in the design of gear by bending strength and surface durability.

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혼합모드(I+II)에서 피로 하중에 의한 균열진전 거동 (Crack Growth Behavior by Fatigue Load under Mixed Mode(I+II))

  • 공병채;최성대
    • 한국생산제조학회지
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    • 제21권2호
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    • pp.276-282
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    • 2012
  • This study looked for Mode status of each for fatigue crack growth behavior about the repeat load of mode I and the static load of mode II. The experiment was performed in the state of the repetition frequency of the sine wave 10Hz, the stress ratio 0.1, maximum load 300kg.f, a static load 0, 100, 200, 300kg.f, As the experimental results, in mode of static load, while the load value increases, the crack growth rate is slower as the energy of a crack mixing grows. Mode I and the power mode II get an influence each other in the direction of crack propagation path, but as they eventually get closer to the breaking point of the crack growth, it is dominated by the mode I.

피로하중을 받는 강섬유보강콘크리트의 인장변형에 관한 연구 (Tensile Strain of Steel Fiber Reinforced Concrete under Fatigue Load)

  • 장동일;채원규;박철우;민인기
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 1992년도 가을 학술발표회 논문집
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    • pp.82-87
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    • 1992
  • In this thesis, the fatigue tests were performed on a series of SFRC (steel fiber reinforced concrete)to investigate the flexural tensile behavior of SFRC varying with the steel fiber contents and the steel fiber aspect ratios. Beam specimens of 10$\times$10$\times$60cm are used. the specimen series are classified according to the steel fiber contents varying 0.5. 1.0, 1.5%, and to the steel fiber aspect ratios varying 60, 80, 100. The three point loading system was used in the fatigue tests. The minimum value of repeated loading was fixed at 10.0kgf and maximum value was 75% to static ultimate strength for periodically using concrete strain gages located at the lower end of the mid-span, and the stress-strain curves were drawn for each specimens, respectively. From the tests result, it was found that the larger steel fiber content and the smaller the steel fiber aspect ratio is , the tensile strain of SFRC under fatigue load proportionally increases. By the regression analysis on these results, the empirical formulae to predict the tensile strain of SFRC were suggested. In comparison of the tensile elastic modulus under fatigue load, it was also found that the larger steel fiber content and the smaller steel fiber aspect ratio is , the smaller decreasing rate of the stiffness of SFRC under fatigue load decreased.

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Effects of TiN Coating on the Fatigue Fracture of Dental Implant System with Various Cyclic Loads

  • Jung, Da-Un;Chung, Chae-Heon;Son, Mee-Kyoung;Choe, Han-Cheol
    • 한국표면공학회지
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    • 제48권6호
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    • pp.283-291
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    • 2015
  • The purpose of this study was to investigate effects of TiN coating on the fatigue fracture of dental implant system with various cyclic loads. TiN coated abutment screw, the fixture, and abutment of internal hex type were prepared for fatigue test. The fatigue test was carried out according to ISO 14801:2003(E) using tensile and compression tester with repeated load from 30% to 80% of static fracture force. Morphology and fractured surface was observed by field emission scanning electron microscope(FE-SEM) and energy dispersive X-ray spectroscope(EDS). The fracture cycle drastically decreased as repeated load increased. Especially, in the case of TiN-coated abutment screw, fracture cycle increased compared to non-coated abutment screw. The fatigue crack was propagated fast as repeated load increased. The plastic deformation region decreased, whereas, cleavage fracture region increased as repeated load increased.