• Title/Summary/Keyword: Maximum Vibration Acceleration

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유체-구조 연성 방법에 의한 단순 탱크 슬로싱 해석 (Sloshing Analysis of a Simple Tank using Fluid-structure Interface Method)

  • 강성종;서홍재;김병주
    • 한국기계가공학회지
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    • 제10권4호
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    • pp.31-37
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    • 2011
  • Fuel tank sloshing noise of vehicle is caused by flow impact on the tank wall during sudden braking, and the sloshing vibration of tank wall is a coupled phenomenon of the fuel inside tank and tank wall structure. Therefore, Fluid-Structure Interface(FSI) analysis technology should be adopted to predict accurately the sloshing vibration. In this study, FSI approach was employed to analyze sloshing phenomenon for a simple tank model with velocity change of the actual vehicle test. First, the simulated results for rigid tank model were compared with those for deformable tank model. Next, influence of baffle location and shape of baffle holes on the acceleration magnitude and the maximum stress of tank wall was investigated. In addition, sloshing analysis for tank with another baffle type was carried out.

케이블 진동 감쇠를 위한 반능동 제어 장치 성능의 실험적 평가 (Experimental Verification of Semiactive Control Systems for Stay Cable Vibration)

  • 장지은;정형조;정운;이인원
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2004년도 가을 학술발표회 논문집
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    • pp.52-59
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    • 2004
  • In this paper, the efficacy of the MR damper-based control systems for vibration suppression of stay cables has been experimentally investigated. The performance of the several control strategies for the semiactive control system, such as the clipped-optimal control, the Lyapunov stability theory-based control, the maximum energy dissipation and the modulated homogeneous friction, has been compared with that of the passive-type control systems employing MR dampers. To do this, the full-scale stay cable, which is the same as used for the in-service cable-stayed bridge in Korea, is considered. The acceleration and the displacement of the stay cable as well as the damping force of the MR damper are measured. The velocity of the cable at the damper location, which is needed for some control algorithms, is obtained by differentiating the measured displacement. The damping ratios of the cable system employing the MR damper, which can be estimated by the Hilbert transform-based method, shows effectiveness of each control strategy considered.

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모사터빈 시험기 개발 및 기초가진 시험 (A Development of Turbine Simulator and Foundation Excitation Test)

  • 김영철;이안성;김병옥;김영춘;우성현
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2004년도 춘계학술대회논문집
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    • pp.675-680
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    • 2004
  • In this study, a turbine simuiator is designed and manufactured to investigate the transient response of an actual turbine. The rotor mass and bearing stiffness is reduced to 1/140 of its actual turbine. The dynamic characteristics of turbine simulator are similar to those of the actual turbine. The turbine simulator is excited by an electro-magnetic type exciter in the form of half sine wave. Duration time is con☞oiled by Sms, 10ms, and Isms, and maximum acceleration is applied by 3g. Foundation excitation test is performed in stationary condition and rotating condition(6000rpm). The test results can be used to verify the validif of the theoretical afproach for transient analysis of actual turbine.

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가장 효율적인 음향 압축기의 튜브형상 (Tube Shape for Highly Efficient Sonic Compressor)

  • 전영두;김양한
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2000년도 춘계학술대회논문집
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    • pp.1455-1460
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    • 2000
  • When a tube is oscillated at a resonant frequency, acoustic variables such as density, velocity, and pressure undergo very large perturbation, often described as nonlinear oscillation. In order to analyze these phenomena, nonlinear governing equation has been drived and solved numerically. Numerical simulations were accomplished to study the effect of the tube shape on the maximum pressure we can obtain. The tubes of cylindrical, conical, and cosine-shape, which have same volume and length, were investigated. Results show that the resonant frequency and patterns of pressure waves strongly depend on not only the tube shape but also the amplitude of driving acceleration. The degree of non-linearity of wave patterns was also measured by the newly defined nonlinear energy ratio of the pressure signals. It was found that the 1/2 cosine-shape tube is more suitable to induce high compression ratio than other shapes.

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유통 중 기계적 충격에 의한 배 포장완충재의 응답 특성 (Response Characteristics of the Cushion Materials for Packaging of the Pears by Mechanical Shock during Transportation)

  • 정현모;김만수;김기석;조병관
    • 한국포장학회지
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    • 제13권1호
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    • pp.25-28
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    • 2007
  • Physical damage on fruits and vegetables caused by shock degrades the value of product in the fresh market. In order to design a product/package system to protect the product, the peak acceleration or G force to the product that causes shock damage needs to be determined. Shock cushion packaging is applied to protect goods of all kinds. It can be adapted in their shape to any product to be packed, so that its shock absorbing properties is determined by geometry of the product. The shape of a cushion can be adapted to the expected shock loads. To analyze the response properties of cushion materials for packaging of the pears for optimum packaging design during transportation, shock tests were carried out. Shock acceleration that is happened in pears were appeared very high by $25{\sim}30G$ in the input shock acceleration of 14.1618 G that was measured in transportation road. This means that the pears receive the shock acceleration more than maximum double itself and the damage by this can happen and the shock acceleration increase in case use PE tray cup and PE net in fruits, the use of corrugated fiberboard pad may become one method that it can reduce the damage by the shock in packaging of fruits.

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추진시스템 종합성능시험에서의 엔진부 비상정지 설정 (Emergency Blockage Application of Engine Part for Integrated Propulsion Performance Test)

  • 하성업;이정호;권오성;김병훈;강선일;한상엽
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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    • pp.171-176
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    • 2003
  • 추진시스템 종합성능시험을 위한 시험시설이 구축되었으며, 최소계측을 통하여 최대한의 안전을 확보하기 위한 비상정지시스템이 검토되었다. 이에 연소실압력과 가속도신호를 이용한 비상정지시스템이 구축되었고, 이 측정변수를 통하여 점화지연 및 실패, 소화, 추진제공급상태, 불안정연소, 과도 구조진동 등을 감시할 수 있었으며, 시험 중 빠른 판단 및 조치에 의하여 시험의 안전을 확보할 수 있었고, 목적한 종합성능시험을 안전하게 완료할 수 있었다.

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지진을 받는 단자유도 진동계의 포화 슬라이딩 모드 제어 (Saturated Sliding Mode Control of SDOF System under Earthquake Leadings)

  • 민경원;이상현;이영철;이승준;박민규
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2003년도 봄 학술발표회 논문집
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    • pp.477-484
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    • 2003
  • Recently, sliding mode control(SMC) method has been investigated for control of building structures under earthquake loadings. SMC keeps responses of a structure in sliding surface while the structure is stable. This control method uses both linear controller and nonlinear controller such as bang-bang controller. This paper presents vibration control of a structure using saturated sliding mode controller, whose maximum conrtol force is limited. The effectiveness of SMC method with controler saturation is investigated based on two performance evaluation criteria: root mean square(RMS) and maximum values of floor drifts and accelerations. Simulation results indicate that SMC method is effective in reduction of displacement and acceleration utilizing the saturated controller's capacity efficiently.

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간접 충격을 이용한 압전 방식 진동형 에너지 하베스터 (Piezoelectric Vibration Energy Harvester Using Indirect Impact)

  • 주선아;지창현
    • 전기학회논문지
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    • 제66권10호
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    • pp.1499-1507
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    • 2017
  • This paper presents an impact-based piezoelectric vibration energy harvester using a freely movable metal sphere and a piezoceramic fiber-based MFC (Macro Fiber Composite) as piezoelectric cantilever. The free motion of the metal sphere, which impacts both ends of the cavity in an aluminum housing, generates power across a cantilever-type MFC beam in response to low frequency vibration such as human-body-induced motion. Impacting force of the spherical proof mass is transformed into the vibration of the piezoelectric cantilever indirectly via the aluminum housing. A proof-of-concept energy harvesting device has been fabricated and tested. Effect of the indirect impact-based system has been tested and compared with the direct impact-based counterpart. Maximum peak-to-peak open circuit voltage of 39.8V and average power of $598.9{\mu}W$ have been obtained at 3g acceleration at 18Hz. Long-term reliability of the fabricated device has been verified by cyclic testing. For the improvement of output performance and reliability, various devices have been tested and compared. Using device fabricated with anodized aluminum housing, maximum peak-to-peak open-circuit voltage of 34.4V and average power of $372.8{\mu}W$ have been obtained at 3g excitation at 20Hz. In terms of reliability, housing with 0.5mm-thick steel plate and anodized aluminum gave improved results with reduced power reduction during initial phase of the cyclic testing.

재분배기법을 이용한 고층건물의 풍응답 가속도 조절 설계기법 (Design Method to Control Wind-Induced Vibration of High-Rise Buildings Using Resizing Algorithm)

  • 서지현;박효선
    • 한국전산구조공학회논문집
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    • 제23권5호
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    • pp.465-473
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    • 2010
  • 건물의 높이와 세장비가 증가함에 따라 건물의 최대 횡변위와 풍응답 가속도와 같은 사용성 요구조건을 만족시키는 것이 고층건물 구조설계에 있어서 중요한 설계요소가 되고 있다. 풍응답 가속도는 거주자에게 불쾌함을 유발시키는 직접적인 원인이 되지만, 초기 구조 설계단계에서 구조 설계자가 풍응답을 조절할 수 있는 실용적인 방법은 개발되어 있지 못하다. 본 연구에서는 재분배기법을 이용하여 건물의 강성을 조절함으로써 고층건물의 풍응답 가속도를 조절할 수 있는 방법을 제안하였다. ASCE 7-02, NBCC 95, ISO 6897 등의 설계 코드 및 기준에 의하면 고층건물의 풍응답 가속도는 1차 고유주기에 반비례한다는 사실에 근거하여 본 연구에서는 물량을 재분배하여 건물의 1차 고유주기를 조절함으로서 풍응답 가속도를 조절하는 실용적 풍응답 가속도 조절 설계법을 제안한다. 제안된 설계법은 42층 건물의 풍응답 가속도 조절 설계에 적용하여 그 적용성과 효율성을 평가하였다.

비행체 탑재 회로카드 조립체의 내충격 향상을 위한 설계 (Design for improving the impact resistance of a vehicle equipped with the circuit card assembly)

  • 이창민;강동석;신영훈;이기선
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2014년도 추계학술대회 논문집
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    • pp.48-53
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    • 2014
  • Rocket, held using the CCA for the mission, a plurality of recording devices, and navigation equipment. In case of a projectile which is entered the water after fired into the air, after performing stages and fairing separated in flight to enter the underwater. It is caused by the explosion of gunpowder mainly, vibration phenomenon of a large transition is induced structurally very, also on entering the water, have a significant shock structurally separated. If shock is transmitted directly to the CCA through the body, it can be caused malfunction of payloads, resulting in failure of the mission of the projectile. In order to ensure the stability against shock, in this paper, Calculating a target resonacne frequency of the CCA, and verified through modal test and analysis. Maximum acceleration position of CCA is checked by SRS analysis. In addition, effectiveness of shock isolation system through shock analysis.

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