• 한국안전학회지
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• 제31권6호
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• pp.52-57
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• 2016

In this study, a restoring viscous damper is introduced for X-type damper system which is designed for the seismic response control of large spatial structures. A nonlinear numerical model for its behavior is developed using the result of dynamic loading tests. The X-type damper system is composed of restoring viscous dampers and connecting devices such as adjustable wire bracing, where the damping capacity of the system is controllable by changing the number of the dampers. The restoring viscous damper is devised to exert main damping force in tension direction, which is effective to prevent the buckling of bracing subjected to compressive axial force. To evaluate the performance of the proposed damper, dynamic cyclic loading tests are performed by using manufactured dampers at full scale. In order to construct the numerical model of the damper system, its model parameters are first identified using a nonlinear curve fitting method with the test data. The numerical simulations are then performed to validate the accuracy of the numerical model in comparison with the experimental test results. It is expected that the proposed system is effectively applicable to various building structures for seismic performance enhancement.

• Journal of Biosystems Engineering
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• 제18권3호
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• pp.239-251
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• 1993

Data acquisition system and computer program developed in this study could be well used in engine vibration analysis. The system and program developed were also operated to be able to control measuring interval, number of channels, number of data. The flywheel was specially studied to provide the proper weight with rubber damper for the engine design at low level of vibration. This study was conducted to obtain basic data which affect the engine vibration. The experiment of this study was performed on original weight flywheel, weight-reduced flywheel, weight-reduced and rubber-coated flywheel, weight-reduced and damper-attached flywheel. Avarage of peak value, maximum vibration, power spectrum density based on FFT analysis are major factors of this experiment. Results were obtained as follows : 1. When rubber was inserted in the flywheel rim of which weight was reduced from 32.2kgf to 24.4 kgf, maximum vibration of the engine was decreased 48.3% at X axis, 35.5% at Y axis and 34.6% at Z axis in comparison with the flywheel of original weight. 2. When the flywheel of rubber damper was compared with the original flywheel, the average of absolute vibration for rubber damped flywheel was decreased at X, Y, Z axis and especially its decreasing rate was so high at X-axis comparing with the other flywheel, which implied that rubber damper was very useful to reducing the vibration of the engine at X axis. 3. Hysteresis losses of X, Y, Z axis were greatly decreased in the flywheel with rubber damper on rim. 4. Damped oscillation effect on X and Y axis vibration above average peak vibration by the flywheel of rubber damper on rim was larger than those by the other flywheels. 5. Power spectrums of vibration at real and imaginery part were bi-mode type. The vibration frequency of rubber dampered flywheel which weight is decreased was slightly increased as compared with original flywheel.

• Earthquakes and Structures
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• 제16권4호
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• pp.437-453
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• 2019

This study investigates a new optimal placement method for viscous dampers between structures in order to prevent pounding of adjacent structures with different dynamic characteristics under earthquake effects. A relative displacement spectrum is developed in two single degree of freedom system to reveal the critical period ratios for the most risky scenario of collision using El Centro earthquake record (NS). Three different types of viscous damper design, which are classical, stair and X-diagonal model, are considered to prevent pounding on two adjacent building models. The objective function is minimized under the upper and lower limits of the damping coefficient of the damper and a target modal damping ratio. A new algorithm including time history analyses and numerical optimization methods is proposed to find the optimal dampers placement. The proposed design method is tested on two 12-storey adjacent building models. The effects of the type of damper placement on structural models, the critical period ratios of adjacent structures, the permissible relative displacement limit, the mode behavior and the upper limit of damper are investigated in detail. The results of the analyzes show that the proposed method can be used as an effective means of finding the optimum amount and location of the dampers and eliminating the risk of pounding.

• 농업과학연구
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• 제20권1호
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• pp.68-87
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• 1993

본(本) 실험(實驗)은 개발(開發)한 시스템과 분석(分析) 프로그램을 이용(利用)하여 플라이휠의 형태별(型態別)로 진동량변화(振動量變化)를 분석(分析)하였다. 플라이휠의 형태(型態)는 원래(元來)의 것과 중량(重量)을 8kgf감소(減少)시킨것, 그리고 중량(重量)을 감소(減少)시키고 립부(部)의 외부(外部)와 중간(中間)에 고무댐퍼를 부착(附着)시킨 것으로 각각(各各)의 진동량변화(振動量變化), PAV율(率), 최대진동량(最大振動量), FFT 등(等)을 분석(分析)하여 비교(比較)하였으며 그 결과(結果)를 요약(要約)하면 다음과 같다. 1. 최대진동량(最大振動量)은 플라이훨 중간(中間)에 고무댐퍼를 부간(附看)한 것이 원래(元來)의 플라이휠에 비(比)하여 X축(軸) 방향(方向)은 48.3%, Y축(軸) 방향(方向)은 35.5% 그리고 Z축(軸) 방향(方向)으로는 34.6% 감소(減少)된 것으로 나타났다. 2. 절대진동량(絶對振動量)의 평균(平均)은 모든 공시(供試)플라이휠에서 부하(負荷)의 증가(增加)에 따라 감소(減少)하는 경향(傾向)이었으며 플라이휠의 림 중간(中間)에 고무댐퍼를 부착(附着)하는 것이 원래(元來)의 플라이휠보다 X축(軸) 방향(方向)은 46.7%, Y축(軸) 방향(方向)은 11.5% 그리고 Z축(軸) 방향(方向)에서는 7.1%가 감소(減少)되어 X축(軸) 방향(方向)의 진동감소(振動減少)는 고무댐퍼의 효과(效果)가 매우 높은 것으로 나타났다. 3. 히스테리시스 손실(損失)은 고무댐퍼를 림 중간(中間)에 부착(附着)한 플라이휠의 X축(軸) 방향(方向)에서 크게 감소(減少)하는 경향(傾向)으로 나타났다. 4. 피크진동량(振動量)의 평균(平均)보다 큰 X, Y축(軸) 방향(方向)의 진동(振動)은 고무댐퍼를 림 중간(中間)에 부착(附着)한 플라이휠에서 감쇠효과(減衰效果)가 크게 나타났다. 5. Power spectrum 분석결과(分析結果)는 실수부(實數部), 허수부(虛數部) 모두에서 가우슨분포곡선(分布曲線)과 일치(一致)하지 않는 bi-mode형태(形態)인 것으로 나타났다. 진동(振動)의 주파수(周波數)는 원래(元來)의 플라이휠은 43.2Hz이고 그외의 경우에서는 49Hz로 약간(若干) 증가(增加)하였다.

• 드라이브 ㆍ 컨트롤
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• 제9권4호
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• pp.62-69
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• 2012

Recently, hydraulic motor is getting the spotlight. It is resulted from rapid civil engineering public works by a lot of developing countries around the world. In this study, we divided the valves which are affixed in the hydraulic motor into some parts, implemented them through computer simulation, verified validation of each component, and analyzed behavior adding driving condition. Through the analyzed results with general driving condition, we found the reason why behavior became unstable as the motor had started spinning. Through the analyzed results with tough driving condition, we verified that the valve works well with it's production purpose.