• Journal of Welding and Joining
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• v.15 no.3
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• pp.1-11
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• 1997

용접이음부에서는 피로크랙 전파거동이 모재와 다르다는 것은 이미 알려져 있으며 그 원인으로서는 용접부에 있어서의 금속조직의 변화와 잔류응력 등이 일컬어 진다. 금속조직의 변화에 따른 영향에 대하여서는 비교적 그 영향이 작으며 또한 피로 크랙 전파속도에 대해서 안전한 쪽으로 역할을 한다고 보고되어져 있다. 따라서 용접 이음부에 있어서의 피로크랙 전파에 대하여서는 주로 잔류 응력의 영향에 주목하여, 잔류응력이 피로크랙의 전파속도에 어떻게 영향을 미치는가를 파악하여야 한다. 이러 한 관점에서 지금까지 용접잔류응력장을 전파하는 피로크랙을 대상으로 하여 잔류응력 이 피로크랙 전파에 미치는 영향을 정량적으로 평가하고자 하느 시도가 많은 연구진에 의해 수행되어 왔다. 표1에 이러한 연구의 흐름을 평가방법과 평가에 고려된 사항을 중심으로 나타내었다. 이러한 배경으로부터, 본고에서는 피로크랙 전파거동에 미치는 잔류응력의 영향에 대해서 지금까지 수행된 연구의 내용을 연구 발전형태에 주목하여 검토하였다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.8 no.4
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• pp.289-297
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• 1984

본 연구에서는 이상과 같은 점을 고려하고 흠함이 존재하기 쉬운 용접부 표면 에 인공적으로 1/4원형에 해당하는 표면피로크랙을 시험편 모서리에 넣고 이러한 시험 편에 굽힘응력을 가하여 다음과 같은 사항들을 고찰하였다. 피로크랙의 표면 및 측 면에서의 전파과정, 피로크랙의 모양비(b/a)의 변화, 피로크랙의 표면 및 측면의 전파 속도와 크랙길이와의 관계등을 알아보았다. 여기에서 크랙의 표면길이란 흠함이 시 험편 모서리에 존재할 때 그것을 기점으로 표면에 전파하는 크랙의 길이를 말하며, 크 랙의 측면길이란 그것을 기점으로 측면의 표면에 전파하는 크랙의 길이를 말한다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.13 no.1
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• pp.115-124
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• 1989

Near-threshold fatigue crack-growth behavior at room temperature for a duplex stainless steel weldments was investigated to evaluate the effect of load ratio, microstructural change, and residual stresses. Near-threshold fatigue crack propagation behavior is found to show a marked sensitivity to .alpha./.gamma. phase ratio, and little residual stress effects. Threshold values in the heat affected zones are higher than those of base metals and threshold values for crack growth decrease with increasing the load ratio in the base metals and weldments. The fractrographic features in base metals, weldments and heat affectred zones were discussed in terms mechanism of crack growth.

• Journal of Ocean Engineering and Technology
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• v.5 no.2
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• pp.76-84
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• 1991

본 연구는 피로수명 평가를 위한 새로운 파괴역학적 parameter의 확립에 관한 연구이다. 실질적으로 피로파괴가 일어나는 피로 균열선단의 국소영역에서 변형분포를 미소원형격자측정법을 이용하여 실험적으로 명확히 밝혀내었다. 그리고 이 결과를 기초로 하여 국소피로 변형율장을 대표할 수 있는 피로변형율 확대계수 $\Delta$A를 제안하였다. 또한 새로운 parameter $\Delta$A의 유효성을 여러 피로조건에서 검토한 결과, 균열선단 국소 영역에서 피로 변형율 확대계수 $\Delta$A에 의하여 피로 균열전파 속도평가를 일의적으로 나타낼 수 있음을 확인하였다.

• Journal of Ocean Engineering and Technology
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• v.5 no.2
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• pp.216-216
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• 1991

• Transactions of the Korean Society of Mechanical Engineers
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• v.16 no.7
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• pp.1373-1380
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• 1992

The local cyclic strain distribution near the crack tip has been investigated by the fine Dot Grid Strain Measurement Method, which had been suggested strain measurement method to resolve experimental difficulties by authors. It has been found that the magnitude of the local cyclic strain distribution(.DELTA..epsilon.$_{eq}$ )near a crack tip has been varied by the applied cyclic load level and material, but the shape of the local cyclic strain distribution near the crack tip has been experimentally scrarcely altered : that is .DELTA..epsilon.$_{eq}$ = .DELTA.A.f(.theta.). $r^{-1}$ . Consequently, the local cyclic strain field near the crack tip could be favorably characterized by a single parameter fatigue strain intensity factor .DELTA.A. In addition, with the viewpoint that .DELTA.A depends on material and load level, .DELTA.A has been applied to evaluate the fatigue crack propagation rate and usefulness of the result has been considered. As a result, it has been ascertained that .DELTA.A has been a useful parameter to evaluate the fatigue crack propagation rate.

• Journal of Advanced Marine Engineering and Technology
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• v.19 no.2
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• pp.36-46
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• 1995

In this paper, fatigue crack propagation behaviors were investigated experimentally for the materials, carbon steel forgings (SF45A, SF50A, SF60A) which are used in the marine propeller shaft. The results obtained are as follows: The number of cycles required to grow crack length 1.30mm from microcrack initiation was about 60% of the total fatigue life. Fatigue crack propagation rate was expressed by the equation d(2a)/dN_B 2a/$N_f$ and the result was agreed well with the experimented data. And the equation d(2a)/dN=$C{\sigma}_a^m(2a)^n$ was evaluated also. Obtained material property m and n are 3~5 and 1-1.5 respectably, and the result was reasonably agreed to the data obtained from experiments.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.21 no.5
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• pp.842-849
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• 1997

The aim of this study is an investigation of the interaction of two micro hole defects affecting fatigue crack initation life and propagation behavior. The locatio of two micro hole defects was considered as an angle of alignment and the distance between the centers of two micro hole defects. The fatigue cracking behavior is experimented under bending. When micro defects are located close to each other, the fatigue crack initiation lives are varied with their relative locations. In the experiments, the area of local plastic strain strongly played a role in the fatigue crack initiation lives. Therefore we introduce a parameter which contains the plastic deformation area at stress concentrations and propose a fatigue crack initiation life prediction curve. In addition, the directions and propagation rates of fatigue cracks initiated at two micro hole defects are studied experimentally.

• Journal of Ocean Engineering and Technology
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• v.1 no.2
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• pp.83-92
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• 1987

Inorder ot estimate the running life of turbine rotors, fatigue crack propagation low, da/dN = C(${\DELTA}K)^m$, proposed by paris et al. has been widely applied. In this study, fatigue crack propagation rates for 16 samples of 1% Cr-Mo-V rotor steel were measured and statistical characteristics of m and C values in above equation were reviewed. The results are summarized as follows. 1. C and m follow a log-normal distribution and normal distribution, respectively. And the relation of C and shows a strong negative correlation. 2. Fatigue crack propagation equation can be expressed as da/dN=$4.11{\times}10^{-4}({\Delta}K/153.8)^m$, introducing the ralationship C=$C_oK_o^{-m}$. In this case, contribution of $C_o$ distribution to the distribution of log C shows very small compared to degrees of contribution by m.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 1994.10a
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• pp.820-825
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• 1994

It is improtant to examine life or crack propagation behavior of structures because of its safety evaluation. The purpose of this study is to investigate the effect of crack-crack interaction to evaluate fatigue life and crack behavior. In this study, the behavior of the interaction of two cracks is studied by experiment. The vertical distance of two cracks is varied to make different interaction stress field. In addition, the effect of plastic zone is considered to examine crack propagation path and propagation rate.