• 콘크리트학회논문집
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• 제12권1호
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• pp.13-22
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• 2000

This paper describes the results obtained from 11 direct tension tests to explore the influence of concrete strength on tension stiffening behavior in reinforced concrete axial members. Three different concrete compressive strengths, 250, 650, and 900kgf/$\textrm{cm}^2$, were included as a main variable, while the ratio of cover thickness-to-rebar diameter was kept constant to be 2.62 to prevent from splitting cracking. As the results, it was appeared that, as higher concrete strength was used, less tension stiffening effect was resulted, and the residual deformation upon unloading was larger. In addition, the spacing between adjacent transverse cracks became smaller with higher concrete strength. The major cause for those results may be attributed to the fact that nonuniform bond stress concentration at both loaded ends and crack sections becomes severer as higher concrete is used, thereby local bond failure becomes more susceptible. From these findings, it would be said the increase in flexural stiffness resulting from using high-strength concrete will be much smaller than that predicted by the conventional knowledge. Finally, a factor accunting for concrete strength was introduced to take account for the effect of HSC on tension stiffening. This proposed equation predicts well the tension stiffening for the effect of HSC on tension stiffening. This proposed equation predicts well the tension stiffening behavior of these tests.

• 한국지반신소재학회논문집
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• 제12권4호
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• pp.57-66
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• 2013

본 연구에서는 산업폐기물인 저회와 폐어망을 각각 뒤채움 재료와 보강재로 재활용하기 위하여 저회와 폐어망 사이의 인발특성을 분석하였다. 이를 위해 저회로 구성된 지반에 망목크기가 다른 3종류의 폐어망(WFN20 : $20mm{\times}20mm$, WFN30 : $30mm{\times}30mm$, WFN40 : $40mm{\times}40mm$)과 지오그리드를 보강재로 사용하여 인발시험을 수행하였다. 인발시험 수행 결과, 지오그리드와 동일한 망목크기를 갖는 WFN20의 인발마찰각은 지오그리드와 유사하게 나타났다. 이것은 WFN20의 인장강도와 강성은 지오그리드 보다 작으나, WFN20의 두께가 지오그리드 보다 커서 횡리브에 의한 지지력이 발현되었기 때문이다. 보강재의 잔류변형률 분포는 연직응력에 의존한다. 연직응력이 증가함에 따라 보강재 선단에 인발력이 크게 집중되어 변형이 크게 나타난다.

• Composites Research
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• 제15권3호
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• pp.30-38
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• 2002

다른 광섬유 센서와 마찬가지로 광섬유 브래그 격자센서도 삽입가능의 장점을 가진다. 삽입가능과 관련된 실제적 가티를 높이기 위해서 본 논문에서는 복합재 평판에 삽입된 브래그 격자센서의 안전성과 스펙트럼특성이 연구되었다. 피복광섬유와 피복이 벗겨진 광성유의 삽입 환경이 현미경 분석에 의해 수행되어졌고 이 현미경 사진들과 성형모니터링 (cure monitoring)의 결과를 기초하여, 저복굴절(Li-Bi) 광섬유에 새겨진 브래그 격자의 단일 브래그 조건을 붕괴하는 주원인이 성형 잔류음력임을 확인했고 이로 인해 광성유가 겪게 되는 응력/변형률 상태를 정략적으로 보고하였다. 또한 성형모니터링은 브래그 공진파장이 어떻 게 분리되어져 가는지 묘사하였고 횡응력 미감도 브래그 격자(TIG)가 재코팅 방법에 의해 쉽게 획득되어짐을 보였다. TIG는 실시간 신호 처리와 관련하여 중요만 장점으로 작용한다.

• 한국구조물진단유지관리공학회 논문집
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• 제17권3호
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• pp.48-55
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• 2013

본 연구에서는 피로 손상된 용접이음의 피로수명 향상을 위한 방법으로 햄머피닝 처리법의 적용성을 검토하기 위하여 면외거셋 필렛 용접이음과 하중비전달형 리브 필렛 용접이음의 피로실험을 실시하였다. 본 실험에서는 면외거셋과 리브를 필렛 용접한 후 햄머피닝 처리를 하지 않은 용접그대로의 시험편, 용접후 햄머피닝 처리한 시험편, 그리고 용접그대로 시험편의 피로수명의 50% 시점에 햄머피닝 처리를 한 시험편의 피로실험을 실시하였다. 그리고 햄머피닝 처리에 의한 면외거셋과 리브 용접토우부의 형상 및 표면응력의 변화를 측정하였다. 그 결과, 햄머피닝처리에 의해 30~83MPa의 압축잔류응력이 도입 되었으며, 이로 인하여 강구조물의 제작시 용접후에 햄머피닝 처리를 실시하면 피로수명을 크게 향상 시킬 수 있을 뿐만 아니라, 이를 공용기간이 예상 피로수명의 50% 이하인 강구조물의 용접이음에 적용하여도 최소 1.3배 이상의 피로수명과 피로한계 향상효과를 기대할 수 있음을 제시하였다.

• 대한용접접합학회:학술대회논문집
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• 대한용접접합학회 2009년 추계학술발표대회
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• pp.97-97
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• 2009

The use of thin plate increases due to the need for light weight in large ship. Thin plate is easily distorted and has residual stress by welding heat. Therefore, the thin plate should be carefully joined to minimize the welding deformation which costs time and money for repair. For one effort to reduce welding deformation, it is very useful to predict welding deformation before welding execution. There are two methods to analyze welding deformation. One is simple linear analysis. The other is nonlinear analysis. The simple linear analysis is elastic analysis using the equivalent load method or inherent strain method from welding experiments. The nonlinear analysis is thermo-elastic analysis which gives consideration to the nonlinearity of material dependent on temperature and time, welding current, voltage, speed, sequence and constraint. In this study, the welding deformation is analyzed by using thermo-elastic method for PCTC(Pure Car and Truck Carrier) which carries cars and trucks. PCTC uses thin plates of 6mm thickness which is susceptible to welding heat. The analysis dimension is 19,200mm(length) * 13,825mm(width) * 376mm(height). MARC and MENTAT are used as pre and post processor and solver. The boundary conditions are based on the real situation in shipyard. The simulations contain convection and gravity. The material of the thin block is mild steel with $235N/mm^2$ yield strength. Its nonlinearity of conductivity, specific heat, Young's modulus and yield strength is applied in simulations. Welding is done in two pass. First pass lasts 2,100 second, then it rests for 900 second, then second pass lasts 2,100 second and then it rests for 20,000 second. The displacement at 0 sec is caused by its own weight. It is maximum 19mm at the free side. The welding line expands, shrinks during welding and finally experiences shrinkage. It results in angular distortion of thin block. Final maximum displacement, 17mm occurs around welding line. The maximum residual stress happens at the welding line, where the stress is above the yield strength. Also, the maximum equivalent plastic strain occurs at the welding line. The plastic strain of first pass is more than that of second pass. The flatness of plate in longitudinal direction is calculated in parallel with the direction of girder and compared with deformation standard of ${\pm}15mm$. Calculated value is within the standard range. The flatness of plate in transverse direction is calculated in perpendicular to the direction of girder and compared with deformation standard of ${\pm}6mm$. It satisfies the standard. Buckle of plate is calculated between each longitudinal and compared with the deformation standard. All buckle value is within the standard range of ${\pm}6mm$.

• 한국건설순환자원학회논문집
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• 제6권4호
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• pp.311-318
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• 2018

이 연구에서는, 기둥 횡방향 철근의 화재 후 잔존 역학적 특성 규명 연구의 일환으로, 횡철근비와 기둥의 고온 노출면 수 차이에 따른 횡방향 철근의 손실강도 보상효과를 잔존 압축강도, 변형률 및 탄성계수와 하중-변위 곡선의 상대적 비교분석을 통해 규명하였다. 실험변수로 띠철근의 간격과 고온 노출면 수를 변수로 한 실험체를 제작하여 가열실험을 수행하였다. 이때 전기로 온도를 $400^{\circ}C$, $600^{\circ}C$ 및 $800^{\circ}C$로 설정하여 $13.33^{\circ}C$/분의 속도로 가열하고 2시간동안 그 온도를 유지시켰다. 냉각된 실험체에 대해 응력-변형률 곡선을 구하기 위한 압축실험을 수행하고, 이로부터 탄성계수, 잔존 내력 및 변형률 등의 잔존 역학적 특성을 분석하였다. 실험결과, 고온 노출 면이 많은 기둥이 수열온도 증가에 따라 탄성계수 감소율이 크게 나타나고, 횡철근비가 크면 수열온도 증가에 따라 탄성계수 감소율이 작게 나타났는데, 이로부터 기둥위치와 횡철근비 등이 내화설계나 화재 안전진단 시 고려되어 합리적인 내화성능 평가가 이루어져야 할 것으로 여겨진다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제9권3호
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• pp.315-325
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• 2017

The design dimension may not be satisfactory at the final stage due to the welding during the assembly stage, leading to cutting or adding the components in large structure constructions. The productivity is depend on accuracy of the welding quality especially at assembly stage. Therefore, it is of utmost importance to decide the component dimension during each assembly stage considering the above situations during the designing stage by exactly predicting welding deformation before the welding is done. Further, if the system that predicts whether welding deformation is equipped, it is possible to take measures to reduce deformation through FE analysis, helping in saving time for correcting work by arresting the parts which are prone to having welding deformation. For the FE analysis to predict the deformation of a large steel structure, calculation time, modeling, constraints in each assembly stage and critical welding length have to be considered. In case of fillet welding deformation, around 300 mm is sufficient as a critical welding length of the specimen as proposed by the existing researches. However, the critical length in case of butt welding is around 1000 mm, which is far longer than that suggested in the existing researches. For the external constraint, which occurs as the geometry of structure is changed according to the assembly stage, constraint factor is drawn from the elastic FE analysis and test results, and the magnitude of equivalent force according to constraint is decided. The comparison study for the elastic FE analysis result and measurement for the large steel structure based on the above results reveals that the analysis results are in the range of 80-118% against measurement values, both matching each other well. Further, the deformation of fillet welding in the main plate among the total block occupies 66-89%, making welding deformation in the main plate far larger than the welding deformation in the longitudinal and transverse girders.

• 한국해양공학회지
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• 제3권2호
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• pp.125-137
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• 1989

To check technical improvement in the soundness and strength of 12% Cr steel rotor, a 25 tons of rotor with 65 tons of ingot was made in real size and was cut to pieces to take test samples, and the various mechanical tests such as impact, tensile, creep, and fatigue were carried out. The strengths are compared with those of 1% Cr-Mo-V rotor of same size. Microstructures of the samples are examined and reviewed. The results can be summarized as follows. 1) Fracture appearance transition temperatures are 80.deg. C at the center part and 60.deg. C near surface of 12% Cr rotor, and 8.deg. C near surface of 1% Cr-Mo-V rotor. 2) Comparative rapid softening occurs at higher temperatures above 600.deg. C for 12% Cr steel and 550.deg. C for 1% Cr-Mo-V steel in tension tests. 3) Fatigue crack propagation rate of 12% Cr steel is almost same as that of 1% Cr-Mo-V steel at the same corresponding surface part of the rotors. The crack growth rate of center part of 12% Cr rotor is faster than near surface part of the rotor, and the crack growth rate at the load condition of R=0.04 is slower than that of the load condition of R=0.5 for both 12% Cr steel and 1% Cr-Mo-V steel. 4) Crack growth rate of radial direction near surface of 12% Cr rotor is faster than that of transverse direction at the same part because of the difference in residual stresses. 5) Both creep and fatigue strengths of 12% Cr steel are superior to those of 1% Cr-Mo-V steel and the difference is thought the effect of climb and glide controlled creep by solid solution of alloying elements and dispersion of carbides.

• 한국해양공학회지
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• 제3권2호
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• pp.625-625
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• 1989

To check technical improvement in the soundness and strength of 12% Cr steel rotor, a 25 tons of rotor with 65 tons of ingot was made in real size and was cut to pieces to take test samples, and the various mechanical tests such as impact, tensile, creep, and fatigue were carried out. The strengths are compared with those of 1% Cr-Mo-V rotor of same size. Microstructures of the samples are examined and reviewed. The results can be summarized as follows. 1) Fracture appearance transition temperatures are 80.deg. C at the center part and 60.deg. C near surface of 12% Cr rotor, and 8.deg. C near surface of 1% Cr-Mo-V rotor. 2) Comparative rapid softening occurs at higher temperatures above 600.deg. C for 12% Cr steel and 550.deg. C for 1% Cr-Mo-V steel in tension tests. 3) Fatigue crack propagation rate of 12% Cr steel is almost same as that of 1% Cr-Mo-V steel at the same corresponding surface part of the rotors. The crack growth rate of center part of 12% Cr rotor is faster than near surface part of the rotor, and the crack growth rate at the load condition of R=0.04 is slower than that of the load condition of R=0.5 for both 12% Cr steel and 1% Cr-Mo-V steel. 4) Crack growth rate of radial direction near surface of 12% Cr rotor is faster than that of transverse direction at the same part because of the difference in residual stresses. 5) Both creep and fatigue strengths of 12% Cr steel are superior to those of 1% Cr-Mo-V steel and the difference is thought the effect of climb and glide controlled creep by solid solution of alloying elements and dispersion of carbides.