• 대한기계학회논문집
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• 제11권2호
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• pp.191-197
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• 1987

본 논문에서는 이상과 같이 그 중요성이 인정되는 작은 표면피로균열의 성장 특성을 조사하기 위하여 연강과 중탄소강에 두 종류의 작은 표면결함을 가공한 네가지 종류의 시험편을 제작하고, 응력비 R=-1인 소야식 회전굽힘 피로시험을 통하여 작은 표면결함이 피로강도에 미치는 영향과 그 성장특성을 조사한 후 응력확대계수 K를 사 용하는 방법과 반복전스트레인 확대계수범위 .DELTA. $K_{\epsilon}$t/를 비교 검토하여 그 유효성 을 조사하고 이를 파괴역학적 측면에서 고찰하였다.다.

• 산업기술연구
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• 제21권B호
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• pp.213-222
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• 2001

In the study, the fatigue strength improvement and mechanism have been estimated by the Spot-Heating treatment on welded bead toes. For this, web-gusset specimens were made without residual stresses and the others with residual stresses imposed by Spot-Heating. The 4-point bending tests were performed in order to estimate the effect of spot-heating on fatigue strength and fatigue characteristics quantitatively for non load-carrying fillet welded joints subjected to pure bending. As a result of fatigue test, fatigue strength of As-Welded specimen for non load-carrying fillet welded joints subjected to pure bending has satisfied the grade of fatigue prescribed in specifications of korea, AASHTO and JSSC. As compare with As-Welded specimen and Spot-Heating specimen have increased about 20% for the fatigue strength at $7.7{\times}10^6$ cycles. The Spot-Heating by reformation of the residual stress on welded bead toes has greatly affected the fatigue crack propagation life, but has slightly affected the fatigue crack initiation life.

• 한국산업안전학회:학술대회논문집
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• 한국안전학회 1999년도 춘계 학술논문발표회 논문집
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• pp.19-24
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• 1999

Ti-6A1-4V재는 1950년대에 개발된 이후, 전체 Ti-합금 수요의 50% 이상을 차지하고 있으며 주로 항공기 터빈 엔진 날개나 자동차의 엔진 밸브 등 각종 열기관의 부품으로 사용되어 왔으나 최근에는 인체의 인공관절로도 수요가 증가하고 있다. (중략)

• 한국정밀공학회지
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• 제16권7호
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• pp.168-177
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• 1999

Fatigue damage is the phenomena which is accumulated gradually with loading cycle in material. It is represented by fatigue crack growth rate da/dN and fatigue life ratio $N/N_{f}$. Fracture mechanical parameters estimating large crack growth behavior can calculate quantitative amount of fatigue crack growth resistance in engineering material. But fatigue damage has influence on various load, material and environment. Therefore, In this study, we propose that artificial intelligent fatigue damage model can predicts fatigue crack growth rate da/dN and fatigue life ratio $N/N_{f}$ simultaneously using fracture mechanical and nondestructive parameters.

• 한국강구조학회 논문집
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• 제20권6호
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• pp.723-730
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• 2008

철도교량은 무거운 축하중이 작용하여 구조부재의 전체 강도에서 활하중이 차지하는 비율이 높기 때문에 피로에 의한 손상이 클 뿐만 아니라 계속적으로 변화하는 하중환경에 의해 피로손상이 빠르게 진행될 가능성이 있으므로 이에 대한 안전성을 체계적이고 분석적으로 평가할 수 있는 방법이 요구된다. 철도교량에서 구조부재별 피로균열의 생성위치 및 성장속도는 발생응력의 범위와 횟수, 구조시스템의 강성에 관련되어 있다. 구조시스템의 강성은 계획주체, 설계자, 시공자, 유지관리주체 각각의 특성과 불확실성을 포함하고 있으며, 시간의존적 하중과 저항의 특성에 의해서 추계학적으로 변화하게 된다. 그러므로 이러한 하중 및 저항에서의 각각의 불확실성을 정량적이고 객관적으로 표현할 수 있는 신뢰성에 기초한 평가기법을 개발하였다. 철도 및 지하철교량 등의 피로파괴에 대한 확률론적 평가를 위하여 응답면 기법(Response Surface Method, RSM)과 일계이차 모멘트 기법(First Order Second Moment method, FOSM)을 사용하여 피로균열진전과 잔존수명을 평가하였다. 응력변동 범위를 설계변수로 변화시키면서, 중요한 설계입력 변수로 한계상태 방정식을 구성하고 다양한 피로 수명(100년, 75년 등)후의 파괴확률을 예측하여 설계피로수명에 대한 신뢰성 지수계산 및 발생확률을 분석사례로 제시하였다.

• 산업기술연구
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• 제22권A호
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• pp.3-8
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• 2002

In this study, extremely low cycle fatigue tests were carried out under push-pull loading conditions using graphite cast iron (GCD). In order to clarify the fatigue fracture mechanism of GCD in an extremely low cycle fatigue regime successive observations of internal fatigue damage were performed. The results obtained are as follows. (1) The process of extremely low cycle fatigue can be classified into three stages which are composed of the generation, growth and coalescence of microvoids inside materials. (2) In an extremely low cycle fatigue regime, microvoids originate from debonding of graphite-matrix interface.

• 대한기계학회논문집
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• 제18권7호
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• pp.1722-1729
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• 1994

At early stage of creep-fatigue crack growth tests, initial transient behavior which implies high crack growth rate has been generally observed by some researchers. Since the influence of the initial transient crack growth behavior on the remaining life of components is significant, cause of it should be further studied. In this study, characteristics of the initial transient behavior of 1Cr-1Mo-0.25V steel is studied experimentally by performing creep-fatigue crack growth tests at $538^{\circ}C$ in air under trapezoidal waveshapes. It is verified that the cause of the initial transient behavior is not high ${(C_t)}_{avg}$ values due to the small scale creep condition at the early stage of test, but oxidation-dominated crack growth mechanism during the transient period which is different from the creep-dominated crack growth mechanism in steady crack growth period.

• 한국강구조학회 논문집
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• 제8권3호통권28호
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• pp.3-11
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• 1996

To investigate the effect of fatigue crack growth due to the surface residual stress, it is measured the residual stress distribution by x-ray diffraction at the crack tip each constant crack growth in the notch specimens, and quantitively assessed the effect of crack closure caused to the distribution of compressive stress at the crack tip from evaluating crack openning stress using the finite element analysis. It is concluded that the degree of the residual stress distribution at the crack tip is decreased with increasing the crack length. From the fact that it is similar to the crack openning stress ratio, it is found that the compressive residual stress distribution and size is related to the crack closure effect and surface residual stress field with propagating crack in the notch specimens depends on the stress intensity factor range at the crack tip.

• 한국해양공학회지
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• 제18권1호
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• pp.28-34
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• 2004

It is well known that tensile peak overloads may significantly delay suubsequent constant amplitude fatigue crack growth in many materials. Since real structures are usually subjected to complex load histories, the ability to predict accurate crack growth under realistic service conditions is of major engineering interest. This paper describes experiments on fatigue track growth in the integrally stiffened panel of 7075-T6 aluminum alloy. The effect of shape parameters and overload position on the fatigue crack growth behavior of integrally stiffened panels are discussed. Based on the experimental results, the following conclusions have been drawn: the overall fatigue crack growth retardation resulting from single overload in the stiffened panels was generally larger in the larger thickness ratio, although the retardation trends, according to the change in overload positions, were similar to those exhibited in the non-stiffened panels.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집A
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• pp.73-78
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• 2000

On this study, the fatigue crack propagation of super duplex stainless steel is investigated in conditions of various volume fraction of austenite phase by changing heat treatment temperature. And we analysed acoustic emission signals during the fatigue test by time-frequency analysis methods. As the temperature of heat treatment increased, volume fraction of austenite decreased and coarse grain was obtained. The specimen heat treated at $1200^{\circ}C$ had longer fatigue life and slower rate of crack growth. As a result of time-frequency analyze of acoustic emission signals during fatigue test, main frequency was $200{\sim}300kHz$ having no correlation with heat treatment and crack length, and 500kHz was obtained by dimple and separate of inclusion