• 제목/요약/키워드: Fatigue crack length

검색결과 253건 처리시간 0.029초

온도사이클을 받는 Solder Joint의 피로수명에 관한 연구 (A Study on the Fatigue Life Prediction of Solder Joints under Thermal Cyclic Loading)

  • 김진기;이순복
    • 전자공학회논문지A
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    • 제31A권12호
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    • pp.44-55
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    • 1994
  • This study is to apply the theory of fatigue fracture to solder joints under thermal cyclic loading and predict life of solder joint to failure. A 62Sn-36Pb-2Ag solder was used in this study. Tensile tests were preformed at temperatures of 15.dec. C, 50.dec. C and 85.dec. C in order to find terms of crack length "a". plastic strain range ""${\Delta}{\varepsilon}_p$" and temperature "T". Solder joint under thermal cyclic loading was analyzed by FEM. this FEM analysis together with the crack growth rate will provide the capability of the fatigue life prediction of solder joints and enhance the reliability od solder joint.

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미소인공결함의 위치에 따른 마찰용접부의 피로특성 (Fatigue Properties of Friction Weld According to the Location of Small Artificial Defect)

  • 이상열;정재강
    • Journal of Welding and Joining
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    • 제19권6호
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    • pp.608-613
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    • 2001
  • In this study, the rotary bending fatigue test was carried out with two kinds of base metal, martensite stainless steel STR3 and austenite stainless steel STR35 and the dissimilar friction welded material with them. To compare the fatigue fifes according to the notch positions, the small circular defect was worked on the bonded line, 1.0mm and 0.5mm distance form the bonded line. The fatigue limits of the STR3 and STR35 base metal were 429.0MPa and 409.4MPa respectably. In comparison with fatigue life at the same notch positions, the STR35 specimens showed about 190% for base metal, 82% for 1.0mm distance notched specimens higher than that of the STR3. But the fatigue life of the 0.5mm distance notched STR35 specimen showed about 35% lower than that of the STR3 specimen. And the bonded line notched specimen was much lower fatigue life than the other specimens because of separation of the bonded line.

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J-integral and fatigue life computations in the incremental plasticity analysis of large scale yielding by p-version of F.E.M.

  • Woo, Kwang S.;Hong, Chong H.;Basu, Prodyot K.
    • Structural Engineering and Mechanics
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    • 제17권1호
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    • pp.51-68
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    • 2004
  • Since the linear elastic fracture analysis has been proved to be insufficient in predicting the failure of strain hardening materials, a number of fracture concepts have been studied which remain applicable in the presence of plasticity near a crack tip. This work thereby presents a new finite element model to predict the elastic-plastic crack-tip field and fatigue life of center-cracked panels(CCP) with ductile fracture under large-scale yielding conditions. Also, this study has been carried out to investigate the path-dependence of J-integral within the plastic zone for elastic-perfectly plastic, bilinear elastic-plastic, and nonlinear elastic-plastic materials. Based on the incremental theory of plasticity, the p-version finite element is employed to account for the accurate values of J-integral, the most dominant fracture parameter, and the shape of plastic zone near a crack tip by using the J-integral method. To predict the fatigue life, the conventional Paris law has been modified by substituting the range of J-value denoted by ${\Delta}J$ for ${\Delta}K$. The experimental fatigue test is conducted with five CCP specimens to validate the accuracy of the proposed model. It is noted that the relationship between the crack length a and ${\Delta}K$ in LEFM analysis shows a strong linearity, on the other hand, the nonlinear relationship between a and ${\Delta}J$ is detected in EPFM analysis. Therefore, this trend will be depended especially in the case of large scale yielding. The numerical results by the proposed model are compared with the theoretical solutions in literatures, experimental results, and the numerical solutions by the conventional h-version of the finite element method.

Turbine Blade재료의 부식민감성과 부식피로특성에 관한 연구 (A Study on the Corrosion Susceptibility and Corrosion Fatigue Characteristics on the Material of Turbine Blade)

  • 조선영;김철한;류승우;김효진;배동호
    • 대한기계학회논문집A
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    • 제24권3호
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    • pp.603-612
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    • 2000
  • Corrosion characteristics on the 12Cr alloy steel of turbine blade was electro-chemically investigated in 3.5wt% NaCI and 12.7wt% Na2S04 solution, respectively. Electro-chemical polarization test, Huey test and Oxalic acid etching test were previously conducted to estimate corrosion susceptibility of the material. And, using the horizontal corrosion fatigue tester, corrosion fatigue characteristics of 12Cr alloy steel in distilled water, 3.5wt% NaCI solution, and 12.7wt%(1M) Na2S04 solution were also fracture-mechanically estimated and compared their results. Parameter considered was room temperature, 60'C and 90'C. Corrosion fatigue crack length was measured by DC potential difference method.Obtained results are as follows,1) 12Cr alloy steel showed high corrosion rate in 3.5wt% NaCI solution and Na2S04 solution at high tempratue.2) Intergranular corrosion sensitivity of 12 Cr alloy was smaller than austenitic stainless steel.3) Corrosion fatigue crack growth rate in 3.5wt% NaCI and 12.7wt%(IM) Na2S04 solution is entirely higher than in the distilled water, and also increased with the temperature increase.

GFRP 복합구조의 피로신뢰성 해석모형에 관한 연구 (Fatigue Reliability Analysis Model for GFRP Composite Structures)

  • 조효남;신재철;이승재
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 1991년도 가을 학술발표회 논문집
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    • pp.29-32
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    • 1991
  • It is well known that the fatigue damage process in composite materials is very complicated due to complex failure mechanisms that comprise debounding, matrix cracking, delamination and fiber splitting of laminates. Therefore, the residual strength, instead of a single dominant crack length, is chosen to describe the criticality of the damage accumulated in the sublaminate. In this study, two models for residual strength degradation established by Yang-Liu and Tanimoto-Ishikawa that are capable of predicting the statistical distribution of both fatigue life and residual strength have been investigated and compared. Statistical methodologies for fatigue life prediction of composite materials have frequently been adopted. However, these are usually based on a simplified probabilistic approach considering only the variation of fatigue test data. The main object of this work is to propose a fatigue reliability analysis model which accounts for the effect of all sources of variation such as fabrication and workmanship, error in the fatigue model, load itself, etc. The proposed model is examined using the previous experimental data of GFRP and it is shown that it can be practically applied for fatigue problems in composite materials.

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퍼스널 컴퓨터에 의한 疲勞試驗自動化 및 疲勞擧動 測定의 精密化 (Personal computer-based fatigue testing automation and improvements in fatigue behavior monitoring)

  • 박준래;송지호;엄윤용;김정엽;강기주
    • 대한기계학회논문집
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    • 제12권1호
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    • pp.123-130
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    • 1988
  • 본 연구에서는 비교적 데이터 처리속도가 빠른 80286계의 CPU를 사용한 16bit 퍼스널 컴퓨터를 이용하는 경우보다, 가격면에서는 훨씬 유리하면서도, 성능은 거의 뒤지지 않는 피로시험 자동화 및 피로거동 고정밀 측정을 위한 시스템을 완성하였다. 본 연구에서 사용한 방법 및 작성한 소프트웨어등은 사용시험기, 피로연구 대상등에 거의 관계없이 이용이 가능하나, 여기서는 편의상, 시험기로서는 폐루우프(closed-loop)유압서어보 피로시험기를 사용하였으며, 피로거동의 측정에 대해서는 주로 피로균열지전을 대상으로 하였다.

Experimental evaluation of fatigue strength for small diameter socket welded joints under vibration loading condition

  • Oh, Chang-Young;Lee, Jun-Ho;Kim, Dong-Woo;Lee, Sang-Hoon
    • Nuclear Engineering and Technology
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    • 제53권11호
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    • pp.3837-3851
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    • 2021
  • To investigate how the fabrication and repair of socket welded joints could be used to enhance fatigue resistance under vibration condition, experimental test data of installation conditions that potentially influence fatigue strength were analyzed with the S-N curve. It was found that the decreasing fatigue strength of stainless steel socket welded joints was attributed to the effect of high heat input of welding process. The effect of welding method, slip-on gap and radial-gap conditions on fatigue strength was insignificant. The test data of repair technique application, 2 × 1 leg length and of socket weld overlay, clearly showed higher fatigue strength but there was a limitation for higher stress region because of the weld toe crack.

용접(鎔接) 강부재(鋼部材)의 피로균열성장(疲勞龜裂成長)에 대한 잔류응력특성(殘留應力特性)에 관한 연구(硏究) (Experimental Investigation of the Residual Stress on Fatigue Crack Growth of Welded Steel Members)

  • 장동일;김두환
    • 대한토목학회논문집
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    • 제7권2호
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    • pp.99-106
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    • 1987
  • 용접(鎔接) 강구조물(鋼構造物)의 피로균열성장거동(疲勞龜裂成長擧動)에 관(關)한 용접잔류응력(鎔擬殘留應力)의 거동(擧動)을 파악(把握)키 위하여 열처리(熱處理)를 실시(實施)하고 피로균열성장(疲勞龜裂成長) 및 검토(檢討)한 결과(結果) 용접부(鎔接部)는 경화(硬化)되어 늑성(勒性)이 감소(減少)되므로 소재부(素材部)보다 피로균열성장율(疲勞龜裂成長率)이 높았으며 이를 열처리(熱處理)한 결과(結果) 경도(硬度)나 저항력(抵抗力)이 증가(增加)되어 개선(改善)되었으며 $650^{\circ}C$ 정도(程度)에서 가장 이상적(理想的) 이었다. Elber 식(式)은 Paris-Erdogan 식(式)에 비(比)해 균열(龜裂)닫힘현상(現狀)을 고려(考廬)하므로 더 낮은 균열성장율(龜裂成長率)을 가지며 각(各) 열처리(熱處理)에 의한 곡선(曲線)들이 서로 비슷하므로 잔류응력(殘留應力)의 효과(効果)를 고려(考慮)할 수 없었다. 균열(龜裂)길이에 따른 개구하중(開口荷重)은 경도(硬度)가 높을수록 큰 값을 가지나 열처리(熱處理) 후(後)는 경도(硬度)값의 저하(低下)로 피로균열(疲勞龜裂) 성장율(成長率)이 낮아지며 흡수(吸收)에너지와 파괴늑성(破壞勒性)을 증대(增大)시켜 균열저지능력(龜裂沮止能力)을 가져 파괴(破壞)의 위험성(危險性)을 감소(減少)시킨다.

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항공기 터빈 디스크용 니켈기 초내열 분말야금 합금의 고온 피로균열진전 거동 비교 평가 (Evaluation of Fatigue Crack Propagation Behavior of Nickel-based Powder Metallurgy Superalloy for Aircraft at Elevated Temperature)

  • 윤동현;나성현;김재훈;김홍규;김동훈
    • 대한기계학회논문집A
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    • 제41권8호
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    • pp.751-758
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    • 2017
  • 항공기 터빈 디스크에 사용될 수 있는 니켈기 초내열 분말야금 합금의 피로균열진전 거동이 실제운전 환경을 고려하여 상온 및 $650^{\circ}C$에서 연구되었다. ASTM E647에서 제시하는 직류전위차법을 이용하여 실시간으로 균열의 진전을 측정하였다. 또한 피로균열진전 시험은 응력비 0.1과 0.5의 두가지 조건에서 수행되었다. 시험결과들은 응력비와 온도 조건 모두 피로균열진전 거동에 영향이 있음을 보여주었으며, 응력비와 온도가 증가함에 따라, 니켈기 초내열 분말 야금 합금의 피로균열성장 속도는 증가하게 관찰되었다. 본 연구에서 사용된 니켈기 초내열 분말 야금 합금은 현재 개발 중인 소재로써 보다 정량적인 시험결과의 분석을 위해, 본 연구의 피로균열진전 시험결과와 기존에 연구된 Inconel-100 소재의 피로균열진전거동에 대한 상호 비교분석이 수행되었다. 피로균열진전 파단면의 분석은 SEM 촬영을 통하여 수행하였다.

하중진폭이 작은 인장과대 하중의 균열성장 거동 (Crack Growth Behavior of Tensile Overload for Small Load Amplitude)

  • 유헌일
    • 한국생산제조학회지
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    • 제7권2호
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    • pp.54-61
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    • 1998
  • This paper examines the crack growth behavior of 7075-T651 aluminum alloy for small tensile overload under high-low block loading condition. The cantilever beam type specimen with a chevron notch is used in this study. The crack growth and closure are investigated by compliance method. The applied initial stress ratios are R=-0.5 R=0.0 and R=0.25 Crack length, effective stress intensity factor range, ratio of effective stress intensity factor range and crack growth rate etc, are inspected with fracture mechanics estimate.

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