• 대한조선학회논문집
• /
• 제41권4호
• /
• pp.85-91
• /
• 2004

The objective of the present paper is to develop an analysis method for the correction of welding deformation of stiffened plate by line heating. In this paper, the equivalent loading method, based on the inherent strain theory, was used to analyze the heat-straightening of a stiffened plate. Equivalent loads were obtained by integrating the inherent strains which were determined from the highest temperature and the degree of restraint. Finally, the obtained equivalent loads were imposed, as applied loads, on the elastic analysis for the prediction of correction of welding deformation in stiffened plate. The proposed method is expected as a basic study in heat-straightening analysis of welding deformation in large scale block.

• Journal of Ship and Ocean Technology
• /
• 제8권3호
• /
• pp.40-49
• /
• 2004

Welding deformations injure the beauty of appearance of a structure, decrease its buckling strength and prevent increase of productivity. Welding deformations of real structures are complicated and the accurate prediction of welding deformations has been a difficult problem. This study proposes a method to predict the welding deformations of large structures accurately and practically based on the simplified thermal elasto-plastic analysis method. The proposed method combines the inherent strain theory with the numerical or theoretical analysis method and the experimental results. The weld joint is assumed to be divided into 3 regions such as inherent strain region, material softening region and base metal region. Characteristic material properties are used in structural modeling and analysis for reasonable simplification. Calculated results by this method show good agreement with the experimental results. It was proven that this method gives an accurate and efficient solution for the problem of welding deformation calculation of large structures.

• 한국정밀공학회지
• /
• 제13권8호
• /
• pp.96-101
• /
• 1996

Glass fiber reinforced polymeric composites hold considerable promise for increased use in low cost high volume applications because of the potential for processing by solid phase forming. Unfortunately, because of the wide variety of such materials, inherent bariability in properties, and complex temperature and strain rate dependence, large strain behavior of these materials has not been well characterized. Of particular importance is failure during processing due to localized necking instability, and it is this phenomenon that is primary focus of this study. The strain rate and temperature dependence is used to predict limiting tensile strains, based on Mackinack imperfection theory. Excellent correlation was obtained between theory and experiment, and the results are summarized in the limit strains as a function of temperature and stain rate.

• 대한용접접합학회:학술대회논문집
• /
• 대한용접접합학회 2009년 추계학술발표대회
• /
• pp.98-98
• /
• 2009

용접에 의해 발생하는 용접잔류응력은 강구조물의 피로성능, 파괴양상 등에 영향을 주고 있으나 이러한 용접잔류응력을 예측하는 것은 쉽지 않다. 이러한 용접잔류응력을 예측하는 방법으로는 열탄소성해석과 같은 수치적 방법과 실험적 방법이 있다. 열탄소성해석의 경우 실제문제를 이상화하는 과정에서 매우 복잡한 모델링 기술이 필요하다. 또한, 측정방법에서는 표면의 잔류응력을 측정할 수 있는 홀드링법과 X-선법 등이 있고, 내부 잔류응력의 측정방법으로는 중성자회절법이 있다. 그러나 홀드링법의 경우, 사용범위의 한계와, 중성자회절법에서의 내부 잔류응력을 측정할 수 있는 두께의 제약이 있어 후판의 잔류응력을 측정하는 것은 한계가 있다. 따라서 본 연구에서는 용접잔류응력의 생성근원인 고유변형도를 측정하고 이것으로부터 맞대기용접에서 발생하는 두께방향의 용접잔류응력을 계측하였다.

• 대한조선학회논문집
• /
• 제37권2호
• /
• pp.127-136
• /
• 2000

선박 건조 시 발생하는 용접변형은 블록의 정도를 떨어뜨리고 교정작업으로 인한 생산성 저하의 요인이 되고 있다. 따라서 설계 단계에서 변형을 최소화 할 수 있는 작업기준을 마련한다면 생산성 증대는 물론 품질의 향상을 가져올 수 있을 것이다. 여기에는 먼저 블록의 조립과정에 따른 변형을 예측할 수 있는 정확하고 효율적인 방법이 마련되어야 한다. 본 논문에서는 고유변형도 이론과 유한요소 해석을 결합한 효율적인 변형예측 기법을 제안하였다. 고유변형도는 간이 열탄소성 해석 결과 최고온도 분포와 구속도에 의해 결정된다. 따라서 용접 열전도 해석과 구조물의 조립과정에 따른 구속도 계산을 수행하여 실제 구조물에 발생하는 고유변형도를 정확히 구하고자 하였다. 이를 이용하여 보강판의 변형 예측을 구현하였고 간단한 선체 블록에 적용할 수 있음을 확인하였다.

• 한국자동차공학회논문집
• /
• 제4권5호
• /
• pp.206-214
• /
• 1996

Because of the wide variety of the composite materials, inherent variability in properties, and complex temperature and strain rate dependence, large strain behavior of these materials has not been well characterized. Large strain behavior under uniaxial tension is characterized over a range of temperatures and strain rates, and a modified simple linear viscoelastic model is fit to the observed data. Of particular importance is the strain rate and temperature dependence of these composites, and it is the primary focus of this study. The strain rate and temperature dependence is then used to predict limiting tensile strains, based on Marciniak imperfection theory. Excellent correlation was obtained between model and experiment and the results are summarized in maps of forming limit as a function of strain rate and temperature.

• 소성∙가공
• /
• 제9권1호
• /
• pp.59-65
• /
• 2000

Most studies of failure analysis in ductile metals have been based on the classical plasticity theory using the local constitutive relations. These frequently yields a physically unrealistic solution, in which a numerical prediction of the onset of a deformation localization shows an inherent mesh-size sensitivity. A one way to remedy the spurious mesh sensitivity resulted in the unreasonable results is to incorporate the non-local plasticity into the simulation model, which introduce an internal (material) length-scale parameter into the classical constitutive relations. In this paper, a non-local version of the modified Gurson constitutive relation has been introduced into the finite element formulation of the simulation for plane strain compression of the visco elastic-plastic void material. By introducing the non-local constitutive relations we could successfully removed the inherent mesh-size sensitivity for the prediction of the deformation localization. The effects of non-local constitutive relation are discussed in terms of the load-stroke curve and the strain distributions accross the shear band.

• Journal of Ship and Ocean Technology
• /
• 제7권4호
• /
• pp.41-49
• /
• 2003

Welding deformation reduces the accuracy of ship hull blocks and decreases productivity due to the need for correction work. Preparing an error-minimizing guide at the design stage will lead to higher quality as well as higher productivity. Therefore, developing a precise method to predict the weld deformation is an essential part of it. This paper proposes an efficient method for predicting the weld deformation of complicated structures based on the inherent strain theory combined with the finite element method. A simulation of a stiffened panel confirmed the applicability of this method to simple ship hull blocks.

• International Journal of Railway
• /
• 제2권4호
• /
• pp.175-179
• /
• 2009

The welding deformation and its prediction method at the HAZ (Heat-Affected Zone) are presented in this paper. The inherent strain method is well known as analytical method to predict welding deformation of large scale welded structure. Depend on the size of welding deformation in welding joints, the fatigue life, the stress concentration factor and the manufacturing quality of welded structure are decided. Many welded joints and its manufacturing control techniques are also required to railway rolling stock and its structural parts such as railway carbody and bogie frame. Proposed methods in this paper focus on the two different the inherent strain area at HAZ. This is main idea of proposed method and it makes more reliable result of welding deformation analysis at the HAZ.

• Journal of Welding and Joining
• /
• 제7권4호
• /
• pp.22-29
• /
• 1989

In this paper weld distortion both in butt and fillet welds by flux cored arc welding has been investigated by changing welding parameters such as heat input and plate thickness, and the weld distortion was expressed as a function of welding parameters adopting the inherent strain theory as proposed by Watanabe and Satoh in 1961. As results of the research it is proposed that transverse shrinkage in root pass butt welds in proportional to ln[(Q/t_-tan.theta.] where Q is heat input(cal/mm), t is plate thickness(mm), and 2.theta. is groove angle(degree), and angular distortion .phi.(radian) in one pass of fillet welds has the following relationship: .phi..var.(Q/ $t^{1.5}$)$^{3}$exp[-(Q/ $t^{1.5}$ )$^{2}$3/] These equations provide us with basic tools to predict the amount of weld distortion in welded structures.