• 한국자동차공학회논문집
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• 제12권1호
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• pp.196-202
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• 2004

The development of new materials with light weight and high strength has become vital to the machinery, aircraft and auto industries. However, there are a lot of problems with developing such materials that require expensive tools, and a great deal of time and effort. Therefore, the improvement of fatigue strength and fatigue life are mainly focused on adopting residual stress(in this thesis). The compressive residual stress was imposed on the surface according to each shot velocity(57, 70, 83, 96 m/sec) based on Shot-peening, which is the method of improving fatigue life and strength. By using the methods mentioned above, the following conclusions have been drawn. 1. The fatigue crack growth rate(da/dN) of the Shot-peened material was lower than that of the Un-peened material. And in stage I, ΔKth, the threshold stress intensity factor, of the shot-peen processed material is high in critical parts unlike the Un-peened material. Also m, fatigue crack growth exponent and number of cycle of the Shot-peened material was higher than that of the Un-peened material. That is concluded from effect of da/dN. 2. Fatigue life shows more improvement in the Shot-peened material than in the Un-peened material. And compressive residual stress of surface on the Shot-peen processed operate resistance force of fatigue crack propagation.

• 한국해양공학회지
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• 제17권2호
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• pp.47-53
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• 2003

The development of new materials with light weight and high strength has become vital to the machinery, aircraft and auto industries. However, there are a lot of problems with developing such materials that require such expensive tools, as well as a great deal of time and effort. Therefore, the improvement of fatigue life through, the adoption of residual stress, is the main focus. The compressive residual stress was imposed on the surface according to each shot velocity(1800, 2200, 2600, 3000rpm) based on Shot-peening, which is the method of improving fatigue life and strength. By using the methose mentioned above, we arrived at the following conclusions; 1. The fatigue crack growth rate(da/dN) of the Shot-peened material was lower than that of the Un-peened material. In stage I, $\Delta$K$_{th}$, the threshold stress intensity factor, of the shot-peen processed material is high in critical parts, unlike the Un-peened material. Also m, fatigue crack growth exponent and number of cycle of the Shot-peened material was higher than of the Un-peened material. That is concluded from effect of da/dN. 2. Fatigue life shows more improvement in the Shot-peened material than in the Un-peened material. Compressive residual stress of the surface on the Shot-peen processed operate resistance force of fatigue crack propagation.

• 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.

• 한국해양공학회:학술대회논문집
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• 한국해양공학회 2003년도 춘계학술대회 논문집
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• pp.313-318
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• 2003

The development of new materials with light weight and high strength has become vital to the machinery, aircraft and auto industries. However, there are a lot of problems with developing such materials that require expensive tools, and a great deal of time and effort. Therefore, the improvement of fatigue strength and fatigue life are mainly focused on by adopting residual stress(in this thesis). The compressive residual stress was imposed on the surface according to each shot velocity(57, 70, 83, 96 m/sec) based on Shot-peening, which is the method of improving fatigue lift: and strength. By using the methods mentioned above, I arrived at the following conclusions 1. The fatigue crack growth rate(da/dN) of the Shot-peened material was lower than that of the Un-peened material. And in stage I, ${\Delta}K_{th}$, the threshold stress intensity factor, of the shot-peen processed material is high in critical parts unlike the Un-peened material. Also m, fatigue crack growth exponent and number of cycle of the Shot-peened material was higher than that of the Un-peened material. That is concluded from effect of da/dN. 2. Fatigue life shows more improvement in the Shot-peened material than in the Un-peened material. And compressive residual stress of surface on the Shot-peen processed operate resistance force of fatigue crack propagation.