• 한국구조물진단유지관리공학회 논문집
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• 제23권6호
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• pp.99-104
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• 2019

본 연구의 목적은 시멘트계 복합재료의 적층을 위해 증점제를 적용하여 개발한 출력배합의 수축 특성을 평가하고, 프린팅 기법을 이용해 제작한 적층시험체와의 수축 특성을 비교하는 데 있다. 증점제 적용 시 수축이 기준배합과 비교하여 평균 25% 저감(56일 기준)되는 것을 확인하였다. 수축이 저감되는 긍정적인 효과에 반해 압축강도는 약 15% 감소(28일 기준)되는 부정적인 효과도 확인되었다. 출력배합을 이용해 제작한 적층시험체와 몰드시험체를 이용하여 수축을 평가한 결과, 적층시험체의 수축변형률이 약 25% 감소(28일 기준)되는 것을 확인하였다. 본 연구결과를 통해 3D 프린팅을 이용한 시멘트계 복합재료의 출력 시 수축의 진전속도와 수축으로 인한 균열의 발생시점을 예측할 수 있을 것으로 판단된다.

• 한국해양공학회지
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• 제6권1호
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• pp.131-139
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• 1992

The understanding and appllication of fatigue crack propagation mechanism in variable amplitude loading is very important for life prediction of the air travel structures. Particularly, the retardation and arrest behavior of fatigue crack propagation by single tension overloading is essential to the understanding and appllication of fatigue crack propagation mechanism in variable amplitude loading. Numerous studies of the retardation behavior have been performed, however investigations of the arrest behavior have not been enough yet. As for the arrest behavior, Willenborg had reported that the overload shut-off ratio $[R_{so}=(K_{OL})/K_{max})_{crack arrest}]$ had been the material constant, but recently several investigators have reported that the overload shut-off ratio depends upon the stress ratio. In this study, authors have investigated the effect of stress ratio on the threshold overload shut-off ratio to generate arrest of fatigue crack growth in high tensile aluminum alloy 7075-T735 which have used in material for air travel structures, It has been $-0.4\leqqR\leqq0.4$ till now, the region of stress ratio investigated. The threshold overload shut-off ratio has decreased as stress ratio has increased in overall region of -$-0.4\leqqR\leqq0.4$ and the linearity has been seen in this material. Moreover, the experimental equation between $R_{so}$ and R has been made; The relation has been $R_{so}=-R+2.6$.

• 한국자동차공학회논문집
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• 제16권5호
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• pp.1-7
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• 2008

A study of new materials that are light-weight, high in strength has become vital to the machinery of auto industries. But then, 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. And Influence of corrosive condition for corrosion fatigue crack was investigated, after immersing in 3.5%NaCl, $10%HNO_3$+3.5%HF, $6%FeCl_3$. The immersion period was performed for 365days. The compressive residual stress was imposed on the surface according to each shot velocity based on shot peening, which is the method of improving fatigue life and strength. Fatigue life shows more improvement in the shot peened material than in the un peened material in corrosion conditions. The threshold stress intensity factor range was decreased in corrosion environments over ambient. Compressive residual stress of surface on the Shot-peen processed operate resistance force of fatigue crack propagation. The fatigue crack growth rate of the Shot-peened material was lower than that of 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.

• 대한조선학회논문집
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• 제60권4호
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• pp.213-221
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• 2023

The demand for Liquefied Natural Gas (LNG) carriers and LNG-fueled ships has significantly increased in recent years due to the sulfur-oxide emission regulations by the International Maritime Organization (IMO). The main goal of this paper is to introduce the process for the Engineering Critical Assessment (ECA) of IMO independent type-B cargo tanks made from 9% nickel alloy. A methodology proposed by the British Standard was used to conduct ECA for any structure with initial flaws. Based on this standard, a Matlab code was developed to perform ECA. Coarse mesh Finite Element Analysis (FEA) was performed on an independent type-B LNG cargo tank with a capacity of 15,000 m³. The location with the highest development of maximum principal stress was identified at the bottom of the cargo tank. Fine mesh FEA was performed to obtain the stress range required for ECA. The dynamic cargo tank loads used for FEA were determined using some ship rules presented by Det Norske Veritas. As a result of performing a 20-year long-term crack propagation analysis with a semi-elliptical surface crack, the fracture-to-yield ratio exceeded the Fracture Assessment Line (FAL) and some structural reinforcement was necessary. Performing a 15-day short-term crack propagation analysis, the fracture-to-yield ratio remained within the FAL, and no significant LNG leaks were expected. This paper is believed to provide a guide for performing ECA of LNG cargo tanks in the future by providing the basic theory and application sample necessary to perform ECA.

• 콘크리트학회논문집
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• 제19권2호
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• pp.171-178
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• 2007

경사 보강근이 철근콘크리트 연속 깊은 보의 구조적 거동에 미치는 영향을 파악하기 위하여 내부 전단경간에 개구부를 갖는 연속 깊은 보 12개가 실험되었다. 주요 변수는 개구부 크기와 경사 보강근 양이다. 개구부 주위의 경사 보강근 양과 개구부 크기의 영향을 동시에 고려하기 위한 유효 경사 보강근 계수가 제시되었다. 실험 결과 개구부를 갖는 연속 깊은 보의 하중 분배, 경사균열 폭 및 치대 내력은 유효 경사 보강근 계수에 의해 결정되었다. 유효 경사 보강근 계수가 클수록 경사균열 폭 및 이들의 진전 속도는 낮았다. 특히 유효 경사 보강근 계수가 0.077 이상인 보의 최대 내력은 동일 개구부 없는 보의 것에 비해 높았다. 내부 전단경간에 개구부를 갖는 연속 깊은 보의 최대 내력을 평가하기 위하여 상계치 이론을 이용한 수치해석 모델이 제시되었다. 제시된 모델로부터 얻은 최대 내력은 실험 결과와 잘 일치하였다.