• Title/Summary/Keyword: 피로균열성장

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A Study on Probabilistic Fatigue Crack Propagation Model in Mg-Al-Zn Alloys under Maximum Load Conditions (III) : Using Interpolation of Random Variable (Mg-Al-Zn 합금의 최대하중 조건에 따른 확률론적 피로균열전파모델 연구(III) : 확률변수의 내삽 이용)

  • Choi, Seon-Soon
    • Proceedings of the KAIS Fall Conference
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    • 2011.05b
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    • pp.757-760
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    • 2011
  • 본 논문의 주목적은 확률변수의 내삽을 이용하여 Mg-Al-Zn합금에 적합한 확률론적 피로균열전파모델을 평가하여 제시하는 것이다. 모델을 평가하기 위하여 최대하중조건을 변화시키면서 피로균열전파실험을 수행하였으며, 실험을 통해 통계적 피로데이터를 확보하였다. 균열성장의 불확실성을 묘사하기 위하여 실험적 피로균열전파모델에 확률변수를 도입한 확률론적 피로균열전파모델을 제안하였으며, 각 모델의 파라미터는 최우추정법으로 추정하였다. 제안된 모델의 적합성을 평가하기 위하여 균열성장에 따른 확률변수의 내삽데이터를 이용하였으며, 평가한 결과 Mg-Al-Zn합금에 적합한 모델은 '확률론적 Paris-Erdogan모델'과 '확률론적 Walker모델'임을 규명하였다.

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Effect of Loading Variables and Temperature on Fatigue Crack Propagation in SA508 Cl.3 Nuclear Pressure Vessel Steel (원자로압력용기강에서 하중변수와 온도가 피로균열진전에 미치는 영향)

  • Kim, B. S.;Lee, B. H.;Kim, I. S.
    • Nuclear Engineering and Technology
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    • v.27 no.6
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    • pp.825-832
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    • 1995
  • The effect of loading variables and temperature on fatigue crack growth rate in SA508 Cl.3 nuclear pressure vessel steel was investigated in air environment Crack growth rate tests on compact tension specimen of thickness 12mm were conducted by using sinusoidal waveform. The crack length was monitored by compliance method. Test conditions were at 0.1 and 0.5 of load ratio, at 1 and 10 Hz of loading frequency, and at room temperature to 40$0^{\circ}C$. At the lower temperatures, the fatigue crack propagation was not affected by the frequency and temperature, while at the higher temperatures above 12$0^{\circ}C$, fatigue crack growth rate increased with decreasing loading frequency and increasing temperature. This accelerated fatigue crack propagation was associated with the increase of oxidation rate at the ahead of crack tip. Fatigue crack growth rate increased with in-creasing the load ratio. The effect of load ratio was more significant at the lower temperature, while the dependence on load ratio decreased with increasing temperature. The sensitivity of load ratio to temperature can be explained by crack closure with the oxidation process.

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압력용기용 SA-508 III강의 미세조직과 상온 피로균열 성장거동

  • 김선웅;문승호;임영록;이후철;신광선
    • Proceedings of the Korean Nuclear Society Conference
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    • 1995.05b
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    • pp.709-714
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    • 1995
  • 영광 3, 4호기에 사용되고 있는 원전 압력용기용 SA-508 IH 강의 미세구조 및 상온 피로균 열성장 특성을 고찰하였다. 본 강재의 미세구조, 석출물 분포 및 형상을 투과전자현미경을 통하여 관찰하였으며 임계영역에서의 거동 및 균열닫힘에 주목하여 피로균열성장 특성을 연구하였다. 다양한 형태의 (Fe, MR)$_3$C 세멘타이트 및 Mo$_2$C 석출물이 입계, 래스경계면 및 입내에 분포되고 있음을 확인하였다. Paris 영역에서의 피로균열성장 속도는 ASME 기준선과 유사하였으며, 임계 영역에서는 일반적인 저합금강의 경우보다 다소 낮게 나타났다. 파면조사 결과 입내 연성파괴현상이 전 $\Delta$K 영역에서 나타나고 있으며, $\Delta$K$_{th}$ 부터 $\Delta$K가 12 Mpa√m 영역에서는 입계파괴 및 입내 평활면이 관찰되었다.

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Fatigue Crack Growth Retardation Using Ring Indentation (링압인을 이용한 피로균열의 성장지연효과)

  • Im,Won-Gyun;Song,Jeong-Hun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.10
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    • pp.27-33
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    • 2003
  • A method for the retardation of fatigue crack growth using ring indentation at the vicinity of a crack is examined. Residual stresses near crack tip are evaluated using fracture mechanics approach using the Bueckner weight function. The motivation is to develop a simple and effective method for obtaining an increase in fatigue lives to total failure of materials with crack. Fatigue testing of aluminum specimen showed that the retardation effects are observed after the application of the method.

Fatigue Crack Growth of Welded-Structural Steel under Simple-Variable Loading (단순변동하중(單純變動荷重)을 받는 용접구조용강(鎔接構造用鋼)의 피로균열성장(疲勞龜裂成長))

  • Chang, Dong Il;Bak, Yong Gul;Lee, Bong Hak
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.7 no.4
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    • pp.103-113
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    • 1987
  • Fatigue tests using a single-peak loading and a two-step loading were carried out to examine the fatigue crack growth behaviar and to find the appropriate analysis method. C-T specimens were made using structural steel SWS58 for the tests. From this, just after a single-peak loading acceleration effect was occured and after some times retardation effect was found. And eminent retardation effect was found after High-Low two-step loading. The transition effect of crack growth due to this variable loading was occured owing to the residual stress and the plastic zone size at the crack tip. And the behaviors of these are well explained by Elber's Crack Closure Model. Also I could find that the Wheeler's Retardation Model is a simple and appropriate theory among analysis methods of fatigue crack growth under the variable loading.

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PWR 원전환경에서 오스테나이트 스테인리스강의 피로균열성장특성에 미치는 질소의 영향

  • Min, Gi-Deuk;Kim, Dae-Hwan;Lee, Bong-Sang;Kim, Seon-Jin
    • Proceedings of the Materials Research Society of Korea Conference
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    • 2011.10a
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    • pp.39.1-39.1
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    • 2011
  • 가압경수로의 압력경계기기는 약 $300^{\circ}C$, 150기압의 고온고압수환경에서 가동되고 있다. 특히 가압기 밀림관은 고온수와, 저온수가 교차하는 부분으로 열성층 형성으로 열적, 기계적 피로 및 수화학환경이 더해진 부식피로 등에 의하여 손상을 받는다. PWR 원전에서 수화학환경은 대표적으로 용존산소(DO) 5ppb, pH 6~8, 용존수소(DH) <30 cc/kg, 온도 $316^{\circ}C$의 환경을 유지하게 된다. 가압기 밀림관에는 오스테나이트계 스테인리스강이 사용되는데, 오스테나이트계 스테인리스강은 고온 수화학환경에 민감한 것으로 알려져 있다. 따라서 오스테나이트계 스테인리강을 공기중에서의 기계적특성 및 피로특성을 향상시키기 위하여 질소를 첨가한 스테인리스강을 제조하여 PWR 원전환경에서의 피로균열성장특성을 평가하였다. 실험에 사용된 재료는 PWR 원전 가압기 밀림관 소재인 Type 347 스테인리스강에 0.0005 wt%가 첨가된 상용재와 0.11 wt% 질소가 첨가된 재료이다. 사용된 시편형상은 두께 5 mm, 폭 25.4 mm의 CT 시편이다. 수화학환경은 150기압, 온도 $316^{\circ}C$, 용존산소(DO) 5ppb, 용존수소(DH) 30 cc/Kg, pH는 약 7로 유지 하였으며, 응력비 0.1, 하중 반복속도 10Hz의 기계적 조건에서 하중제어로 시험을 진행하였다. 균열길이는 직류전위차법(Direct Current Potential Drop: DCPD)을 이용하여 측정하였다. 질소함량이 증가할수록 동일 사이클에서 균열길이가 늦게 성장하였고, 피로균열성장속도도 약간 늦어지는 것으로 나타났다. 각 스테인리스강의 피로파면 관찰결과 상용재는 약 1 ${\mu}m$의 산화물들이 생성되는 반면 질소첨가 스테인리스강은 약 0.1 ${\mu}m$정도 산화물이 생성되었다. 산화막의 두께도 질소가 첨가됨으로써 상용재에 비해 얇게 생성되었다. 따라서 질소가 첨가됨으로써 부식환경에서 내산화성이 향상되었으며, 이는 피로균열성장특성에 영향을 미치는 것으로 판단된다.

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The Fatigue Crack Growth Behavior of Concrete (콘크리트의 피로균열 성장거동에 관한 연구)

  • 김진근;김윤용
    • Magazine of the Korea Concrete Institute
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    • v.9 no.3
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    • pp.127-135
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    • 1997
  • In this study, the wedge splitting tcst (WST) was carried out for the fatigue wack growth behavior of concrete. Selected test variables were concrete compressive strength of 28, 60 and 118 MI%, and stress ratio with 2 levels (6. 13%). In oder to make the designed stress ratio, the maximum and thr minimum fatigue loading level were 75-85% and 5- 10% of ultimate static load, respectively. Fatigue testing was preceded by crack mout.h opening displacement (CMOI)) compliance calibration tcst, and then the fatigue crack growth was computed by crack lcngth vs. (lMOI) compliance relations acquisited by the CMOD compliance calibration technique. To evaluate thc validity of CMOD compliancc calibration techniquc, the crack length p~mlicted by this method was cornpard with the crack length by linear elastic fracture mechanics(LEFIbl) and dyeing test. On the basis of the experimental results, a LRFhl-based c.mpirica1 model for f'at,igue crack growth rate(da/dN-AKI relationships) was presented. The fat,igut. crack growth ratc increased with the strength of concwtc. It appcars that t.he da/tiN-AKI relationships was influenced by stress ratio, however, the effect is diminished with an increase of strength. The comparisons between CblOl) compliance calibration technique anti the other. methods gave the validity of' ('MOD compliance calibration technique for the LZXT.

Evaluation of Probabilistic Fatigue Crack Propagation Models in Mg-Al-Zn Alloys Under Maximum Load Conditions Using Residual of Random Variable (최대하중조건에 따른 Mg-Al-Zn 합금의 확률변수 잔차를 이용한 확률론적 피로균열전파모델 평가)

  • Choi, Seon Soon
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.39 no.1
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    • pp.63-69
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    • 2015
  • The primary aim of this paper is to evaluate the probabilistic fatigue crack propagation models using the residual of a random variable and to present the probabilistic model fit for the probabilistic fatigue crack growth behavior in Mg-Al-Zn alloys under maximum load conditions. The models used in this study were prepared by applying a random variable to empirical fatigue crack propagation models such as the Paris-Erdogan model, Walker model, Forman model, and modified Forman model. It was verified that the good models for describing the stochastic variation of the fatigue crack propagation behavior in Mg-Al-Zn alloys under maximum load conditions were the 'probabilistic Paris-Erdogan model' and 'probabilistic Walker model'. The influence of the maximum load conditions on the stochastic variation of fatigue crack growth is also considered.

Finite Element Analysis of Stage II Crack Growth and Branching in Fretting Fatigue (프레팅 피로에서 2단계 균열성장과 분지 유한요소해석)

  • Jung, Hyun Su;Cho, Sung-San
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.39 no.11
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    • pp.1137-1143
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    • 2015
  • The stage II fretting fatigue crack growth and branching, i.e., the process of fretting fatigue crack growth starting in an inclined direction and then changing to the normal direction, is analyzed using the finite element method. The fretting fatigue experiment data of A7075-T6 are used in the analysis. The applicability of maximum tangential stress intensity factor, maximum tangential stress intensity factor range, and maximum crack growth rate as the crack growth direction criteria is examined. It is revealed that the stage II crack growth before and after the branching cannot be simulated with a single criterion, but can be done when different criteria are applied to the two stages of crack growth. Moreover, a method to determine the crack length at which the branching occurs is proposed.

Fatigue Creak Growth Properties of Welded Joint for the Railway Bridge Steel (철도교량(鐵道橋梁)의 용접부(鎔接部)에서 피로(疲勞)균열의 성장특성(成長特性))

  • Chang, Dong Il;Yong, Hwan Sun
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.4 no.1
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    • pp.125-136
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    • 1984
  • In the weled structures, fatigue fracture mainly depends upon crack growth behavior. Specially anisotropy of crack growth orientation and welding direction become important factor of fracture in the welding jone. When fatigue stressed steel welded with nonfatigue stressed steel, at the low stress intensity factor range, residual stress become more important factor of growth behavior then properties of base metal but when the crack growth in the weld metal, toughness of weld metal become the most important factor. Especially nonhomgeniety of toughness for the weld metal make more scatter the relations of $da/dN-{\Delta}K$.

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