• 제목/요약/키워드: Acceleration section

검색결과 206건 처리시간 0.026초

진동대시험을 이용한 댐의 내진성능평가 (The Evaluation of Seismic Performance of Dam By Shaking Table Tests)

  • 황성춘;오병현;심형섭;강보순
    • 한국지진공학회:학술대회논문집
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    • 한국지진공학회 2005년도 학술발표회 논문집
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    • pp.110-117
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    • 2005
  • This paper deals the shaking table tests with 1/100 scaled model followed by Scott & Iai(1989)'s similitude law for OO dam main desging section to understand nonlinear behavior characteristics of concrete dam body by earthquake wave. As earthquake wave, Hachinohe and Elcentro waves were used and acceleration and displacements are measured to analyze behaviors of dam body. For ground maximum acceleration range ($0.3^{\sim}0.9g$), the results showed linear behavior regardless of ground maximum acceleration and secured safety of structure. To analyze the behavior of dam after tension cracking, 3cm-notch was placed at the critical section of over-flowing section. As results of applying Hachinohe wave(0.8g), Even though tension cracks were formed at over-flowing section by Hachinohe wave(0.8g), it showed that the dam is stable for supporting upper stream part of water tank of dam.

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진동대 시험을 이용한 콘크리트 댐의 동적거동 특성 연구 (A Study on the Dynamic Behavior of Concrete Dam by Shaking Table Tests)

  • 황성춘
    • 한국소음진동공학회논문집
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    • 제15권7호
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    • pp.806-812
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    • 2005
  • This paper adresses the shaking table tests with 1/100 scaled model followed similitude law for OOdam main designing section to understand nonlinear behavior characteristics of concrete dam body by ground motion. As earthquake wave, Hachinohe and El Centre waves were used and acceleration and displacements are measured to analyze behaviors of dam body. For maximum ground acceleration range $(0.3\~0.9 g)$, the results showed linear behavior regardless of maximum 9round acceleration and secured safety of structure. To analyze the behavior of dam after tension cracking, 3 cm-notch was placed at the critical section of over-flowing section. As results of applying Hachinohe wave(0.8 g), Even though tension cracks were formed at over-flowing section by Hachinohe wave(0.8 g), it showed that the dam is stable for supporting upper stream Part of water tank of dam.

경부고속철도 교량의 과도한 가속도의 저감방안에 대한 연구 (A Study on the Solution of Excessive Accelerations on the Bridge for Gyeongbu High-speed Railway)

  • 곽종원;진원종;최은석;조정래;이정우
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2007년도 춘계학술대회 논문집
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    • pp.477-485
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    • 2007
  • When Korean High Speed Train (KTX) runs over a high-speed railway bridge, the high-speed railway bridge gives quite large acceleration response. Local vibration at the large cross section, the impact from equally spaced sleepers, the vibration due to elastomeric bearings, and the vibration from the train itself are the causes of this acceleration response. Maximum peaks of the accelerations measured at the bridges are sometimes going over the limit value. Although it is smaller than 0.35G, the limit from the Korean Bridge Design Manual(BRDM), this acceleration response should be reduced for the safety of running trains with high speed. In this paper, to reduce the acceleration response by controlling excessive local vibration at the large cross section, vibration reduction method is studied. The result shows that the effect of elastomeric bearings on the vibration of the bridge is very large and that the vibration reduction device is effective against wing mode local vibration PSC box girder bridge for the high-speed railway, which usually has very large cross section, although it has little effect on global vibration modes such as flexural and twisting modes. The test of the vibration reduction device on the bridge in service has been performed in this study.

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Seismic response of steel reinforced concrete spatial frame with irregular section columns under earthquake excitation

  • Xue, Jianyang;Zhou, Chaofeng;Liu, Zuqiang;Qi, Liangjie
    • Earthquakes and Structures
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    • 제14권4호
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    • pp.337-347
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    • 2018
  • This paper presents some shaking table tests conducted on a 1/4-scaled model with 5-story steel reinforced concrete (SRC) spatial frame with irregular section columns under a series of base excitations with gradually increasing acceleration peaks. The test frame was subjected to a sequence of seismic simulation tests including 10 white noise vibrations and 51 seismic simulations. Each seismic simulation was associated with a different level of seismic disaster. Dynamic characteristic, strain response, acceleration response, displacement response, base shear and hysteretic behavior were analyzed. The test results demonstrate that at the end of the loading process, the failure mechanism of SRC frame with irregular section columns is the beam-hinged failure mechanism, which satisfies the seismic code of "strong column-weak beam". With the increase of acceleration peaks, accumulated damage of the frame increases gradually, which induces that the intrinsic frequency decreases whereas the damping ratio increases, and the peaks of acceleration and displacement occur later. During the loading process, torsion deformation appears and the base shear grows fast firstly and then slowly. The hysteretic curves are symmetric and plump, which shows a good capacity of energy dissipation. In summary, SRC frame with irregular section columns can satisfy the seismic requirements of "no collapse under seldom earthquake", which indicates that this structural system is suitable for the construction in the high seismic intensity zone.

Effects of different roll angles on civil aircraft fuselage crashworthiness

  • Mou, Haolei;Du, Yuejuan;Zou, Tianchun
    • Advances in aircraft and spacecraft science
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    • 제2권4호
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    • pp.391-401
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    • 2015
  • Crashworthiness design and certification have been and will continue to be the main concern in aviation safety. The effects of roll angles on fuselage section crashworthiness for typical civil transport category aircrafts were investigated. A fuselage section with waved-plates under cargo floor is suggested, and the finite element model of fuselage section is developed to simulate drop test subjected to 7 m/s impact velocity under conditions of 0-deg, 5-deg, 10-deg and 15-deg roll angles, respectively. A comparative analysis of failure modes, acceleration responses, and energy absorption of fuselage section under various conditions are given. The results show that the change of roll angles will significantly affect fuselage deformation, seat peak overloads, and energy absorption. The crashworthiness capability of aircraft can be effectively improved by choosing appropriate landing way.

시뮬레이션을 이용한 고속도로 진출입로에서 차량속도와 곡선반경에 따른 상용차량 전복 연구 (A Simulation Study of Commercial Vehicle Rollover in Highway Ramp Section According to Vehicle Speed and Curvature)

  • 박중영;이홍국;장경진;서이정;유송민
    • 자동차안전학회지
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    • 제7권2호
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    • pp.50-54
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    • 2015
  • Rollover accidents are a common occurrence on the highway ramp section. At highway ramp section, unexpected situations might occur due to demand on complex steering control unlike routine driving maneuver in the main streamline. Commercial vehicles have higher risk of rollover due to their high center of gravity. In this study, the lateral acceleration causing rollover would be found. In addition, sections would be classified as dangerous and safe ones by confirming the maximum lateral acceleration for various speed and curvature.

다물체 동역학해석을 이용한 DMT 화차의 주행특성 연구 (Multibody Dynamic Simulation and Running characteristics of DMT Freight)

  • 엄범규;현석;안천헌;이희성
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2008년도 추계학술대회 논문집
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    • pp.1607-1613
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    • 2008
  • The present investigate is a base investigate required in development of DMT wagon train. And it deduced that follows by developing trail analysis model about Modalohr wagon train and examining traveling movement specific using analysis model developed. Vibration acceleration of all direction was increased with addition of travel speed and first suspension. But in case of right and left vibration acceleration, that could influenced by nonlinear specific of first suspension. Therefore checking about those is needed. Frequency of $2{\sim}3\;Hz$ and $7{\sim}8\;Hz$ generated in Right and left, up, down vibration of vehicle. And right and left vibration of bogie generated $25{\sim}35\;Hz$ in low speed section and frequency of $40{\sim}50\;Hz$ in high speed section, $25{\sim}35\;Hz$ in low speed section, $10{\sim}15$ or $40{\sim}50\;Hz$ in high speed section.

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궤도 진동기반의 침목플로팅궤도 침목방진패드 스프링강성 추정 기법 연구 (Estimation Method of Resilience Pads Spring Stiffness for Sleeper Floating Tracks based on Track Vibration)

  • 최정열;박상욱;정지승
    • 문화기술의 융합
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    • 제9권6호
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    • pp.1057-1063
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    • 2023
  • 본 연구대상인 도시철도 침목플로팅궤도(STEDEF)는 구조물로 전달되는 진동을 저감시키기 위한 방진궤도이다. 현재 침목플로팅궤도의 침목방진패드 교체주기(정적 스프링강성 변화율, 25±2%)는 하중기반(궤도충격계수와 궤도지지강성)으로 설정되어 운영중인 실정이다. 그러나 대부분의 선행연구는 침목방진패드의 피로수명평가와 스프링강성 증가에 따른 궤도충격계수 및 궤도지지강성의 증가 등 하중기반의 구조적 안전성 측면의 연구가 진행되었다. 따라서 본 연구에서는 분석 구간별 도상 진동가속도를 측정하고 700만회 피로시험결과를 이용하여 구간별 침목방진패드 스프링강성을 산출하고자 한다. 구간별 산출한 침목방진패드 스프링강성을 해석제원으로 설정하여 도상 진동가속도를 해석적으로 도출하였다. 구간별 해석 도상 진동가속도가 현장측정 도상 진동가속도 범위 이내로 나타나 해석모델링의 적정성이 검증되었다. 도출된 스프링강성 변화에 따른 진동가속도 선도(g-k curve)를 이용하여 측정 도상 진동가속도로 침목방진패드 스프링강성을 추정하고자 한다. 따라서 측정 도상 진동가속도를 이용한 운행선로의 침목방진패드 스프링강성을 추정할 수 있는 기법을 제시하고자 한다.

가속차로의 길이 제어와 고속도로 접속부 혼잡저감 효과 (Longitudinal Control of Acceleration Lanes and its Impact on Congestion Alleviation)

  • 신치현;김규옥
    • 대한교통학회지
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    • 제23권5호
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    • pp.169-176
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    • 2005
  • 고속도로 합류부의 반복정체는 모든 이의 일상이지만 정체가 발생한 이후에 마땅히 시도할 대책이 없는 것이 작금의 현실이다. 본 연구는 접속부에 혼잡이 발생한 후 상황에 따라 가속차로 길이를 동적으로 제어하여 본선에 대한 상대적인 우월성을 억제함으로써 혼잡구간의 정체를 저감시키는 기법을 제안하고 있다. 가속차로의 동적 제어가 미치는 교통영향 분석을 위해서 car-following 이론에 토대를 둔 미시 모형인 CORSIM을 사용하였으며, 본선의 수요는 LOS D/E로 유지하는 가운데 연결로 수요를 변화시킴으로서 접속부의 혼잡을 점진적으로 연출하고 본선과 가속차로의 운영속도가 역전되는 시점에 가속차로의 유효길이를 축소하는 기능을 구현하였다. 동적 제어의 대상이 되는 가속차로 길이는 세 가지로 제한하였으며 평가척도는 통행시간과 통과교통량으로 하였다. 또 경부고속도로에 신갈 JC서의 유사 운영 결과와 비교를 통해 모의실험 결과를 뒷받침하였다.

극저온 자연순환회로의 가속 및 저중력 구간 유량 분석 (Analysis of the Flow Rate for a Natural Cryogenic Circulation Loop during Acceleration and Low-gravity Section)

  • 백승환;정영석;조기주
    • 한국추진공학회지
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    • 제23권5호
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    • pp.43-52
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    • 2019
  • 극저온 유체를 사용하는 발사체는 극저온 유체의 자연순환회로를 이용하여 발사체의 엔진 입구를 냉각한다. 자연순환회로의 질량유량은 순환시스템을 구성하는 배관의 길이 및 직경과 시스템으로 들어오는 열유입에 의하여 결정된다. 극저온 유체의 자연순환회로의 순환 검증 및 질량유량 측정을 위하여 실험을 진행하였으며, 이론적 계산 결과와 비교하였다. 비교 결과 12%의 오차가 있음을 확인하였다. 이 결과를 바탕으로 발사체 상단에서 저중력 구간 및 가속 구간에서의 자연순환 질량유량을 예측한 내용을 포함한다. 가속구간에서는 산화제탱크가 100 kPa 내외로 유지하는 것이 자연순환유량 증가에 이로웠으며, 저중력구간에서는 중력가속도의 크기에 따른 최적 압력으로 조절해야 자연순환유량의 최고값을 유지할 수 있었다.