• 제목/요약/키워드: Thick-Plate Weldments

검색결과 12건 처리시간 0.026초

PREDICTION AND CONTROL OF ANGULAR DISTORTION IN THICK WELDMENTS

  • Kim, Sang-Il;Kang, Joong-Kyoo;Han, Yong-Sub
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2002년도 Proceedings of the International Welding/Joining Conference-Korea
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    • pp.700-705
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    • 2002
  • The welding distortion of a hull structure in the shipbuilding industry is inevitable at each assembly stage. The geometric inaccuracy caused by the distortion tends to preclude the introduction of automation and mechanization and needs the additional man-hours for the adjusting work at the following assembly stage. To overcome this problem, a distortion control method should be applied. For this purpose, it is necessary to develop an accurate prediction method which can explicitly account for the influence of various factors on the welding distortion. In order to minimize the weld-induced angular distortion in thick weldments, this paper proposes the optimum groove design for various plate thicknesses as the distortion control method. The validity of this method has been substantiated by a number of numerical simulations and experiments.

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후판 구조의 각변형 예측 및 제어에 관한 연구 (A Study on the Prediction and Control of Angular Distortion in Thick Weldments)

  • 허주호;김상일
    • Journal of Welding and Joining
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    • 제21권5호
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    • pp.518-524
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    • 2003
  • The block assembly of ship consists of a series of heat processes such as cutting, bending, welding, residual stress relaxation and fairing. With the fast development of computers, the thermal elasto-plastic analysis method has become a versatile tool for practical applications in the ship production. If numerical analysis is proved to be an advantageous tool to predict the residual deformation due to various heat processes, the optimum methods which can remove the welding distortion can be presented at each assembly stage, which will result in great progress in improving the accuracy of block assembly. In order to minimize the weld-induced angular distortion in thick weldments, this paper proposes the optimum groove design for various plate thickness as the distortion control method. The validity of this method has been substantiated by a number of numerical simulations and experiments.

후판 구조의 각변형 예측 및 제어에 관한 연구 (A Study on the Prediction and Control of Angular Distortion in Thick Weldments)

  • 김상일
    • 한국해양공학회지
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    • 제22권6호
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    • pp.100-105
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    • 2008
  • The block assembly of ship consists of a series of heat processes such as cutting, bending, welding residual stress relaxation and fairing With the fast development of computers, the thermal elasto-plastic analysis method has become a versatile tool for practical applications in the ship production. If numerical analysis is proved to be an advantageous tool to predict the residual deformation due to various heat processes, the optimum methods which can remove the welding distortion can be presented at each assembly stage, which will result in great progress in improving the accuracy of block assembly. In order to minimize the weld-induced angular distortion in thick weldments, this paper proposes the optimum groove design for various plate thickness as the distortion control method. The validity of this method has been substantiated by a number of numerical simulations and experiments.

DEVELOPMENT OF A PRACTICAL METHOD FOR THE ESTIMATION OF WELD INDUCED CRACK IN THICK PLATE WELDMENTS

  • Lee, Jae-Myung;Yoon, Dong-Ryul;Heo, Hee-Young;Jang, Tae-Won;Lee, Jae-Won
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2002년도 Proceedings of the International Welding/Joining Conference-Korea
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    • pp.396-401
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    • 2002
  • A practical method for evaluating the possibility of the occurrence of cracking in actual thick-plate T-joint weldments is presented in this study. Systematic experiments based on the method of the design of experiment are conducted in order to investigate the crack tendency in relation to typical welding parameters such as diffusible hydrogen, restraint intensity, preheating temperature and so on. The elastic analysis using the [mite element techniques is employed to quantify the restraint intensities of the specimens. The defined restraint intensities are treated in numerical way for the sake of considering the most uncertain factor among some major factors that govern the cracking phenomena due to welding. The critical plane for judgment of the crack occurrence or crack density is presented as a function of typical welding parameters including determined restraint intensities. The results of numerical estimation by the proposed method for the experimental specimens show the usefulness as a practical tool in welding induced crack problem having extensive uncertainties.

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Fatigue Strength Depending on Position of Cracks for Weldments

  • Lee Hae-Woo;Park Won-Jo
    • Journal of Mechanical Science and Technology
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    • 제20권5호
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    • pp.675-680
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    • 2006
  • This is a study of fatigue strength of weld deposits with transverse cracks in plate up to 50 mm thick. It is concerned with the fatigue properties of welds already with transverse cracks. A previous study of transverse crack occurrence, location and microstructure in accordance with welding conditions was published in the Welding Journal (Lee et al., 1998). A fatigue crack develops as a result of stress concentration and extends with each load cycle until fatigue occurs, or until the cyclic loads are transferred to redundant members. The fatigue performance of a member is more dependent on the localized state of stress than the static strength of the base metal or the weld metal. Fatigue specimens were machined to have transverse cracks located on the surface and inside the specimen. Evaluation of fatigue strength depending on location of transverse cracks was then performed. When transverse cracks were propagated in a quarter-or half-circle shape, the specimen broke at low cycle in the presence of a surface crack. However, when the crack was inside the specimen, it propagated in a circular or elliptical shape and the specimen showed high fatigue strength, enough to reach the fatigue limit within tolerance of design stresses.

A Simplified Method to Estimate Welding Induced Crack of Weldments with Initial Structural Restraints

  • Lee, J.M.;Paik, J.K.;Kim, M.H.;Kang, S.W.;Heo, H.Y.
    • International Journal of Korean Welding Society
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    • 제4권1호
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    • pp.38-45
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    • 2004
  • A practical method for evaluating the possibility of the occurrence of cracking in actual thick-plate T-joint weldments is presented in this study. Systematic experitrients based on the method of the design of experiment are conducted in order to investigate the crack tendency in relation to typical welding parameters such as diffusible hydrogen, restraint intensity, preheating temperature and so on. The elastic analysis using the fmite element techniques is employed to quantify the restraint intensities of the specimens. The defined restraint intensities are treated in numerical way for the sake of considering the most uncertain factor among some major factors that govern the cracking phenomena due to welding. The critical plane for judgment of the crack occurrence or crack density is presented as a function of typical welding parameters including determined restraint intensities. The results of numerical estimation by the proposed method for the experimental specimens show the usefulness as a practical tool in welding induced crack problem having extensive uncertainties.

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J-적분을 이용한 용접구조물의 파괴해석 (Fracture Analysis of Welded Plates using the J-integral)

  • 심용래
    • 전산구조공학
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    • 제9권4호
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    • pp.173-179
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    • 1996
  • 용접구조물의 파괴거동을 분석하기 위해서는 용접중의 열전달 해석, 잔류응력 해석, 그리고 파괴해석이 같이 병행되어야 한다. 잔류응력이 존재하면 J-적분은 적분 경로에 관계없이 일정한 값을 갖는 특성을 잃게 된다. 그러므로 용접부의 J-적분 해석을 위해서는 별도의 프로그램을 개발하여야 한다. 본 연구에서는 균열선단에서의 J-적분을 계산하기 위한 이론식 및 프로그램을 개발하였으며 적용사례로 박판 및 후판의 다층용접에 대한 J-적분값을 계산하였다.

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J-적분을 이용한 용접부 강도 해석 (A Strength Analysis of Welded Plates Using the J-integral)

  • 이민호;양영수
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2000년도 추계학술대회 논문집
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    • pp.326-329
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    • 2000
  • Study of Weldment fracture behavior mcludes thermal analysis, residual stress analysis, and fracture analysis The 1-integral loses its path-independency in a res~dual stress field Therefore, it id necessary to develop a program to calculate the J-integral in a welded plate. m this study, theoretical formulation and program were developed for the evaluation of the 1-integral at the crack tip o i weldments. To verify equations and program, welded thin plate and thick plate were used to calculate residual stress and the J-integral.

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대전류 및 용가재 직경에 따른 Al5083 아크 용접부 마그네슘 기화 및 기계적 성질 (Effects of High Current and Welding Wire Diameter on the Magnesium Vaporization and Mechanical Properties of Al5083 Arc Welds)

  • 권혜미;박철호;홍인표;강남현
    • Journal of Welding and Joining
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    • 제31권6호
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    • pp.84-89
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    • 2013
  • The demand of LNG tank and the constituting material, i.e., the Al5083 thick plate, increased due to the rapid growth LNG market. To weld the Al5083 thick plate, the gas metal arc welding (GMAW) of high current is necessary to increase manufacturing productivity incurred by the multi pass welding. However, the arc welding vaporizes the volatile element such as magnesium (Mg). This phenomenon changes the Mg composition of the weld metal and the mechanical properties. The study investigated the weldability of Al5083 alloys after conducting high current GMAW. The Al5083 alloy was welded by using different size of welding wires and high current (800-950A). As the arc current increased from 800A to 950A, the mechanical strength decreased and the secondary dendrite arm spacing (SDAS) increased. Even though the arc current increased SDAS, the mechanical strength decreased due to the Mg loss in the weldment. The large diameter of welding wire decreased the dilution of the weld, therefore increasing the Mg content and the strength of the weld. For the reason, the content of Mg in welds was a major parameter to determine the mechanical property for the high current GMAW. For the arc current between 800A and 950A, the yield strength of the weldments showed a relationship with the weight percent of Mg content ($X_{Mg}$): Y.S = 27.9($X_{Mg}$)-11.