For low-rise piloti-type buildings that suffered significant damage in the Pohang earthquake, the seismic performance of those designed by codes issued before and after the earthquake has been recently revised. This study started with the expectation that many of the requirements presented in the current codes may be excessive, and among them, the spacing of column stirrup could be relaxed. In particular, the recently revised design code of concrete structures for buildings, KDS 41 20 00, suggests that the column stirrup spacing is 1/2 of the minimum cross-sectional size or 200 mm, which is strengthened compared to KBC 2016, but relaxed than the current KDS, 41 17 00, which is 1/4 of the minimum size or 150 mm. As a result of the study, it was found that the target performance level was sufficiently satisfied by following the current standards and that it could be satisfied even if the relaxed spacing was followed. Therefore, the strict column stirrup spacing of KDS 41 17 00 could be relaxed if a wall other than core walls is recommended in the current guideline for the structural design of piloti-type buildings.

본 논문은 철계형상기억합금(Fe-SMA) stirrup으로 전단보강된 철근콘크리트 보의 전단거동을 예측하기 위한 해석적 연구이다. 전단거동 예측을 위해 변형률 적합조건 및 하중 평형조건을 만족하는 휨해석이 수행되었으며, 이후 수정압축장이론 (MCFT)에 기반한 전단해석이 수행되었다. 부재의 처짐을 계산하기 위해 휨 및 전단에 의해 발생된 처짐이 모두 고려되었다. 제 안된 해석모델의 검증은 Ji et al.(2022)의 실험결과를 비교하여 수행되었다. 비교결과 제안된 해석모델과 실험결과의 극한하중, 극한하중 시 처짐의 오차는 평균 4.77%, 6.62%로 Fe-SMA Stirrup으로 전단보강된 철근콘크리트 보의 전단 거동을 비교적 정확 하게 예측하는 것으로 나타났다.

Experimental evaluation of torsional behavior, which is possible behavior of seismic beams of RC structures, was carried out. Concrete strength and stirrup spacing were set as experimental variables to investigate the torsional strength of RC beams. Based on the experimental results, the torsional strength of RC beams was compared and analyzed. From the experimental results, the concrete strength was caused a difference of about 30% in the torsional strength of the maximum torque of the RC beam specimen, and the stirrup spacing was found to be about 2.8 times and 5 times that of the peak torque. Therefore, this study will be an important study to understand the effect of both concrete strength and stirrup spacing for the torsional strength or torsional behavior of RC beams.

In this study, pure torsion tests were performed for a square cross-section reinforced concrete beams. Stirrup spacing and yield strength of the material was used to the experimental variables. From the test results, large torsional strength were occurred in specimens, which have small stirrup spacing. when, stirrup spacing was greater than the cross-sectional depth, regardless of the stirrup strength, maximum torsional strengths were nearly the same. Contrary, stirrup spacing was less than the cross-sectional depth, according to the stirrup strength, maximum torsional moment were largely. Lastly, the cracks of the beam much occurred in smaller stirrup spacing specimens.

The existing commercially available CFRP stirrups with circular section have inherent weakness of premature failure due to fiber kinks and stress concentration at bend. In order to overcome this weakness, a novel stirrup was developed with CFRP chord in the shape of spiral (CSCS). Results from B.5 tests have shown that CSCS were superior to CFRP stirrups with circular section in resisting stresses at bend.

최근 탄소섬유판 매립공법의 콘크리트 구조물의 보강에 적용되고 있다. 그러나 탄소섬유판 표면매립공법은 피복부 콘크리트의 강도 부족과 높이 부족 등으로 인하여 그 적용의 제한이 발생하기도 한다. 본 연구에서는 이와 같은 이유로 인하여 전단 스터럽을 절단하고 탄소섬유판을 주철근의 위치에 표면매립 보강하는 공법에 대하여 고찰하였다. 일반적인 표면매립공법과 스터럽을 절단하고 표면매립공법을 적용한 보에 대한 휨 실험을 수행하였으며, 결과를 서로 비교하였다. 탄소섬유판의 길이를 실험변수로 하였다. 실험결과에 따르면, 전단 스터럽을 절단한 보강 보의 휨거동은 일반적인 표면매립공법이 적용된 실험체의 거동과 유사한 전형적인 휨 거동을 나타내었으며, 스터럽의 절단으로 인한 구조거동상의 문제는 발생하지 않았다. 따라서, 일반적인 현장 여건에 의하여 탄소섬유판의 적용이 곤란한 경우에는 스터럽을 절단하는 본 공법의 적용이 가능한 것으로 판단된다.