• 대한기계학회논문집A
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• 제37권5호
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• pp.649-655
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• 2013

이종금속용접부에 대한 실제 용접 공정 중 용접부에서 결함이 발견되면 이를 제거하고 보수용접이 수행된다. 일반적으로 보수용접을 수행하면 용접부에서 인장 잔류응력이 크게 증가될 수 있는 것으로 알려져 있다. 따라서 Alloy 82/182를 사용하여 보수용접이 수행된 이종금속용접부의 일차수 응력부식 균열 현상을 평가하기 위해서는 보수용접에 의한 용접부의 응력 변화를 정확하게 평가해야 한다. 본 논문에서는 비선형 유한요소해석을 수행하여 보수용접에 의한 원자력 이종금속 맞대기 용접부의 응력 분포를 평가하였다. 특히 보수용접 공정 모사를 위한 여러 유한요소 해석방법이 이종금속용접부의 응력분포에 미치는 영향을 평가하였다.

• 수산해양기술연구
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• 제36권4호
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• pp.322-328
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• 2000

남해안 연근해에서 조업하는 정치망 어선에 양망작업시 보조기계로 사용되는 캡스턴의 드럼에서 용접부 온도분포 및 구배를 해석한 결과의 주요 사항은 다음과 같다. 1. 용융부 근처는 냉각개시 1초 이내에 950$^{\circ}C$/sec, 10초 이내는 40$^{\circ}C$/see 정도의 급격한 냉각속도가 형성되었다. 2. 열영향부(HAZ)는 용접 후 1초가 경과할 때 370$^{\circ}C$/sec의 가열속도로 온도가 증가한 후, 이 후 25$^{\circ}C$/sec 냉각속도로 온도가 감소한다. 용접종료 10초 후 모재 내부에는 1.64$^{\circ}C$/mm, 40초가 지났을 때는 0.26$^{\circ}C$/mm 정도의 온도구배가 형성되었다. 3. 용접부 근처는 길이 방향을 따라 격심한 온도편차를 보이고 있으나 두께방향으로는 거의 나타나지 않는다. 이 결과는 향후 캡스턴 드럼의 용접부 최적설계시, 탄소성 열응력 및 열변형 거동을 해석하는 연구의 기초자료로 활용될 수 있을 것이다.

• 한국자동차공학회논문집
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• 제24권4호
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• pp.425-431
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• 2016

The usage of Friction Stir Welding(FSW) technology has been increasing in order to reduce the weight in automobile industries. Previous studies that investigated on the FSW have focused on the aluminum alloy. In this study, Al6061-T6 alloy plates having 5 mm of thickness were welded under nine different conditions from three tool rotation speeds: 900, 1000 and 1100 rpm, and three feed rates: 270, 300 and 330 mm/min. Specimen size of Micro Shear Punch(MSP) test was $10{\times}10{\times}0.5mm$. The mechanical properties were evaluated by MSP test and Analysis of Variance (ANOVA). The specimens were classified by advancing side(AS), retreating side(RS), and center(C) of width of tool shoulder. The optimal welding condition of FSW based on micro strengh was obtained when the tool rotation speed was 1100 rpm and the feed rate was 300 mm/min. The maximum load measured AS, RS, and C in the weldment was measured 554.7 N, 642.9 N, and 579.2 N, respectively.

• Journal of Welding and Joining
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• 제33권3호
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• pp.62-67
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• 2015

A very large shell-structure built in shipyards like ship hulls or offshore structures are joined by welding through full process. As the welding contains a high thermal cycle at a local area, the welded structures should be distorted unavoidably. Because a distorted ship block should be revised to the designed value before the next stage, the ability to predict and to control the weld distortion is an accuracy level of the yard itself. Despite the ship block size, several present thermal distortion methodologies can deal those sizes, but it is a different story to deal full ship size model. Even a fully constructed ship hull not remaining any welding can have an accuracy issue like outfitting installation problems. Any present thermal distortion methodology cannot accept this size for its recommended element size and the number. The ordinary welding breadth at erection stage is about 20~40 mm. It can hardly be a good choice to make finite element model of these sizes considering human effort and computational environment. The finite element model for structure analysis of a ship hull is prepared at front-end engineering design stage which is the first process of the project. The element size of the model is as fine as the longitudinal space, and it is not proper to obtain a weld distortion at the erection stage. In this study, a methodology is suggested that a weldment can be shrunk at original place instead of using structural finite element model. We cut the original shell elements at erection weld-line and put truss elements between the edges of cut elements for weld shrinkage. Additional truss elements are used to facsimile transverse weld shrinkage which cannot be from the weld-line truss element shrink. They attach to weld-line truss element like twigs from barks. The capacity of developed elements is verified through an accuracy check of erection process of a container vessel at the apt. hull. It can be a useful tool for verifying a centering accuracy after renew and for block-separating planning considering accuracy.