• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2001년도 봄 학술발표회 논문집
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• pp.877-882
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• 2001

Lap splice in plastic hinge region of RC bridge piers is inevitable because of the constructional joint between footing and column. RC circular columns with lap-splice in plastic hinge region are widely used in Korean highway bridges. It is, however, believed that there are not many experimental research works for nonlinear behavior of these columns subjected to earthquake motions. This study has been performed to verify the effect of axial force, lap splice and confinement steel ratio for the seismic behaviour of reinforced concrete bridge piers. Quasi-static test have been done to investigate the physical seismic performance of RC bridge piers, such as displacement ductility and enemy absorption.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 1997년도 추계학술대회 논문집
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• pp.127-131
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• 1997

In systematic and orderly estimation of fatigue strength of the spot welded lap joints, because the influence of residual stress of fatigue crach initiation and growth is not negligible, there need to estimate fatigue strength considered residual stress at near spot weld part of the lap joints. Therefore, in this thesis, peformed stress distribution and residual stress analysis at near the spot weld part by F.E.M and X-ray diffraction method, and obtained the maximum principal stress considered residual stress at nugget edge by superposing residual stress at nugget edge by superposing their results. From the results obtained above, we could find that fatigue strength of the IB-type spot welded lap joints was rearranged by the maximum principal stress considered residual stress at nugget edge and was entirely low about 13 percents compare with that neglected residual stress.

• 대한기계학회논문집A
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• 제24권8호
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• pp.2022-2031
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• 2000

Since the surface roughness of adherends affects much the strength of adhesivelybonded joints, the effect of surface roughness on the fatigue life of adhesively bonded tubular single lap joints was investigated analytically and experimentally by fatigue torsion test. The stiffness of the interfacial layer between adherends and adhesive was modeled as a normal statistical distribution function of surface roughness of adherends. From the investigation, it was found that the optimum surface roughness of adherends for the fatigue strength of tubular single lap joints was dependent on bondthickness and applied load.

• 한국산학기술학회논문지
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• 제19권5호
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• pp.570-576
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• 2018

철근콘크리트 구조물에서 철근의 이음은 철근을 겹쳐서 결속선으로 결속한 겹침이음과 커플러에 의한 기계적 이음이 일반적이다. 국내 설계기준(콘크리트구조기준)에서는 일반철근(비용접 철근)에 대해 용접 겹침이음을 제한하고 있으나, 해외기준(AWS D1.4)에서는 예열을 통한 일반철근의 용접 겹침이음을 허용하고 있다. 본 연구에서는 국내외 규격 및 설계기준을 조사하고, 건설현장에서 가장 많이 사용되는 SD400 강종의 일반철근을 대상으로 용접 겹침이음 인장실험을 수행하여 인장강도를 평가하였다. 용접 겹침이음 시험체의 용접길이는 KS규격(KS B ISO 17660-1)에 제시된 최소용접길이인 8d를 적용하고, 예열온도는 AWS D1.4에 따라 D19이하는 $150^{\circ}C$, D22이상은 $260^{\circ}C$로 설정하였다. 인장실험 결과, 용접 겹침이음된 일반철근은 콘크리트구조기준에서 요구하는 인장강도(항복강도의 125%)를 발현하였으며, 모두 철근 모재에서 파단이 발생되었다. 예열 유무에 따른 영향을 검토하기 위해, 일반철근을 예열한 후 용접한 것과 예열 등의 열처리하지 않은 것을 비교한 결과, 인장강도는 큰 차이를 보이지 않았다. 실험시 사용한 일반철근을 대상으로 화학성분을 분석하여 탄소당량(Ceq)을 확인한 결과, 0.45% 이하로 낮았다. AWS D1.4에 따르면, 탄소당량이 0.45% 이하면 예열이 필요하지 않은 조건이다. 결과적으로 예열의 영향이 미비한 것은 일반철근의 탄소당량이 낮았기 때문인 것으로 확인되었다.

• 한국구조물진단유지관리공학회 논문집
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• 제16권5호
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• pp.68-77
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• 2012

기존의 격자형 강합성 바닥판 이음부 상세는 후크형태의 철근 겹침이음 및 채움 콘크리트로 구성된다. 본 연구에서는 콘크리트 전단키와 고장력볼트로 구성된 이음부 형식에 대해 콘크리트 전단키 보강 유무를 실험변수로 휨성능평가 실험을 하였고, 그 결과를 기존 철근겹침 이음부의 휨성능과 비교 평가함으로써 기계적 연결방법에 의한 이음부 형식의 적용 가능성을 검토하였다. 실험결과의 비교 분석에 의하면, 기계적 연결방식에 의한 이음부의 최대내력이 약 30% ~ 60% 정도 더 큰 것으로 나타나서 강도 측면에서 더 우수함을 확인하였다. 모멘트-곡률 관계로부터 구한 휨강성을 비교해 보면, 철근겹침 이음부의 경우 초기 거동에서는 비교적 더 우수한 거동을 보였으나, 콘크리트 균열파괴가 발생한 이후에는 다소 급격한 단면성능의 감소를 보였다. 한편, 콘크리트 전단키의 강판 보강 유무에 따른 변수 분석 결과에 의하면 강판 보강구조가 최대내력 향상 및 휨강성 증가에 효과적임을 확인할 수 있었다.

• 한국전산구조공학회논문집
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• 제32권1호
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• pp.1-5
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• 2019

본 연구는 접착조인트의 파손모드 및 파손강도 연구를 위해 단일 겹침 시편(Single lap shear joint)을 이용하여 해석을 실시하였다. 알루미늄과 스틸, Araldite 접착제를 이용, 시편을 제작하여 인장시험을 진행하였으며 시험데이터를 이용, 유한요소해석 결과와 비교 분석하였다. 알루미늄과 스틸, 접착제 모두 비선형해석을 통해 정확한 거동을 묘사하고자 하였다. 시험결과 파단강도는 Overlap length와 Width가 증가함에 따라 선형적으로 증가하였다. 또한 이종재료 조인트의 경우 동종재료 조인트와 비교 시 10~17% 정도의 파손강도 증가를 보였다. 이는 강성이 강한 스틸을 함께 사용함으로써 판재의 굽힘변형이 줄어들고 이를 통해 본드의 응력집중을 막는 효과를 가져왔기에 나타난 현상으로 분석된다. 유한요소해석을 통한 응력분포 및 변형률 분포를 분석한 결과 동종재료의 경우 본드 양 끝단, 이종재료의 경우 강성이 약한 판재와 가까운 부분에서 집중이 발생하였다. 응력집중 및 파손의 주요 인자를 확인하기 위해 본드의 각 성분 별 응력 값을 측정해 본 결과 1-3방향 전단응력 이 파손의 가장 큰 인자로 분석되었다.

• Advances in aircraft and spacecraft science
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• 제11권1호
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• pp.83-103
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• 2024

Adhesive bonding is currently widely used in many industrial fields, particularly in the aeronautics sector. Despite its advantages over mechanical joints such as riveting and welding, adhesive bonding is mostly used for secondary structures due to its low peel strength; especially if it is simultaneously exposed to temperature and humidity; and often presence of bonding defects. In fact, during joint preparation, several types of defects can be introduced into the adhesive layer such as air bubbles, cavities, or cracks, which induce stress concentrations potentially leading to premature failure. Indeed, the presence of defects in the adhesive joint has a significant effect on adhesive stresses, which emphasizes the need for a good surface treatment. The research in this field is aimed at minimizing the stresses in the adhesive joint at its free edges by geometric modifications of the ovelapping part and/or by changing the nature of the substrates. In this study, the finite element method is used to describe the mechanical behavior of bonded joints. Thus, a three-dimensional model is made to analyze the effect of defects in the adhesive joint at areas of high stress concentrations. The analysis consists of estimating the different stresses in an adhesive joint between two 2024-T3 aluminum plates. Two types of single lap joints(SLJ) were analyzed: a standard SLJ and another modified by removing 0.2 mm of material from the thickness of one plate along the overlap length, taking into account several factors such as the applied load, shape, size and position of the defect. The obtained results clearly show that the presence of a bonding defect significantly affects stresses in the adhesive joint, which become important if the joint is subjected to a higher applied load. On the other hand, the geometric modification made to the plate considerably reduces the various stresses in the adhesive joint even in the presence of a bonding defect.

• 한국표면공학회지
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• 제45권5호
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• pp.181-187
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• 2012

The Friction Stir Welding (FSW) has mainly been used for making butt joints in Al alloys. The development of Friction Stir Lap Welding (FSLW) would expand the number of applications. In this study, microstructures and mechanical properties of FSLW in A5052 alloy were investigated under varying rotating speed and probe length. Investigating the characteristics as FSLWed conditions were as below ; Failure Maximum load by shear fracture was increased proportional to the width of joint area, which was increased by input heat, stirring intensity in the case of 2.3 mm probe length. Tensile fracture occurred, and maximum load was determined due to side worm hole of joint area and softening of microstructure in the case of 3.0 mm probe length. In the case of 3.7 mm probe length, material hook and bottom worm hole were appeared at the end interface of joint area. The most sound FSLW condition with no defects was 3.0 mm probe length and 1500 rpm-100 mm/min. No defects were showed in 1500 rpm-100 mm/min and 1800 rpm-100 mm/min, but Vickers microhardness distribution in TMAZ/HAZ which was fracture zone was lower in 1800 rpm-100 mm/min than in 1500 rpm-100 mm/min. In this condition highest tensile strength, 215 MPa (allowable rate 78% of joint efficient) was obtained.

• 한국해양공학회:학술대회논문집
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• 한국해양공학회 2000년도 추계학술대회 논문집
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• pp.171-177
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• 2000

It is essential to understand the creep behavior, which shows how long the characteristics of material maintains because press joined molding GMT-Sheet for recycle is usually used in the severe environment. In this study, we predict joining strength of GMT-Sheet for recycle, when lap length was changed. and we will investigate how compression ratio have an effect on creep behavior in press joined molding. The result of experiment of forming condition concerned with joining problem of GMT-Sheet is as followings joining efficiency. of GMT-Sheet, increases as lap joint length I, increases. Increase of compression ratio causes decrease o f joining efficiency after of GMT-Sheet joining. As the result of creep test, GMT-Sheet is easily damaged in high temperature range, because it is sensitive to the temperature

• Journal of Mechanical Science and Technology
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• 제15권1호
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• pp.44-51
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• 2001

One of the recent issues in design of the spot-welded structure such as the automobile body is to develop an economical prediction method of the fatigue design criterion without additional fatigue test. In this paper, as one of basic investigation for developing such methods, fracture mechanical approach was investigated. First, the Model I, Mode II and Mode III, stress intensity factors were analyzed. Second, strain energy density factor (S) synthetically including them was calculated. And finally, in order to decide the systematic fatigue design criterion by using this strain energy density factor, fatigue data of the ΔP-N(sub)f obtained on the various in-plane bending type spot-welded lap joints were systematically re-arranged in the ΔS-N(sub)f relation. And its utility and reliability were verified by the theory of Weibull probability distribution function. The reliability of the proposed fatigue life prediction value at 10(sup)7 cycles by the strain energy density factor was estimated by 85%. Therefore, it is possible to decide the fatigue design criterion of spot-welded lap joint instead of the ΔP-N(sub)f relation.