• Title/Summary/Keyword: 관성진동

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New Dynamic Model of Large-Scale 20-Ton MR Fluid Damper (대용량 20톤 MR 유체 감쇠기의 새로운 동적 모델)

  • ;;Yang, Guangqiang
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2002.04a
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    • pp.141-148
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    • 2002
  • MR 유체 감쇠기는 구조물의 진동을 감소시키기 위한 가장 유망하고 새로운 제진 (制振) 장치 중 하나이다. 이 장치는 기계적인 단순성, 높은 동적 범위, 적은 전력 요구량, 커다란 감쇠 능력, 강인성 등의 장점을 가지고 있기 때문에, 토목 구조 시스템의 내진(耐震) 및 내풍(耐風) 성능을 향상시키는데 매우 유용하다. 많은 연구자들이 MR 유체 감쇠기의 유사-정적 모델을 연구했지만 그 모델이 감쇠기의 설계를 위해서는 유용하다고 하더라도, 동적 하중에 대한 감쇠기의 거동을 모사하는 데는 충분하지 않다. 논문에서는 대용량 20톤 MR 유체 감쇠기의 동적하중에 대한 응답 해석 결과를 이용하여, Bouc-Wen 모델을 기반으로 하는 새로운 역학적 모델을 제안하였다. 이 모델은 MR 유체의 stiction현상과 관성 및 shear thinning 효과를 잘 묘사한다. 또한, 제안된 MR 유체 감쇠기의 동적 모델이 실험 결과와 매우 잘 일치함을 보였다.

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Controller Design of Hybrid Tuned Mass Damper (하이브리드 제진장치 콘트롤러 설계기술)

  • Joo, Seok-Jun;Lee, Sung-Kyung;Shin, Koon-Jae;Kwon, June-Yeop
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2010.04a
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    • pp.392-395
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    • 2010
  • 최소질량형 제진장치는 초고층건물의 풍진동 제어시 질량체의 관성력을 최대한 효율적으로 이용하여 이동질량의 크기를 최소화한 제진장치라 할 수 있다. 본 연구의 최종목표는 순수 국내기술에 의한 능동제어(active control)와 수동제어(passive control)의 특성이 결합된 하이브리드 제진장치(hybrid control device)의 콘트롤러 설계기술 개발이다. 이를 위한 1차적인 목표로 여기에서는 국내에 설치된 기존의 능동진동제어장치의 전체적인 설계과정을 살펴본다.

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A Study on Torsional Vibration Suppression of 2-Mass Motor (2관성계 전동기 구동 시스템의 축 진동 억제에 관한 연구)

  • Ji, Jun-Keun
    • Proceedings of the KIEE Conference
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    • 1996.11a
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    • pp.454-456
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    • 1996
  • This paper deals with the comparison study of speed controller for torsional vibration suppression of 2-mass motor drive system. Firstly conventional methods suggested were classified systematically and the features of each method were also compared. Especially the speed controller based on Kalman filter and LQ state feedback was proposed and the response characteristics of it were compared with those of some other methods. Through various computer simulations and the experiments of real 22[KW] field oriented controlled AC motor drive system having 2-mas mechanical system, it was confirmed that the characteristic of proposed speed controller using Kalman filter and LQ is the best among them.

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The Study on the Added Moment of Inertia of Two Dimensional Cylinder induced by the Torsional Vibration coupled with the Flexural Vibration (자유수면(自由水面)에서의 비틀림 수평(水平)굽힘의 연성진동(連成振動)을 하는 선체단면형(船體斷面形)의 이차원적(二次元的) 부가관성(附加慣性) Moment에 관(關)한 연구(硏究))

  • S.S.,Kim
    • Bulletin of the Society of Naval Architects of Korea
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    • v.7 no.2
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    • pp.3-18
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    • 1970
  • An investigation was made for the added mass moment of inertia induced by the rotational motion of the cylinder with hull section on water in order to obtain the information to estimate the natural frequency of the torsional vibration of ships. The special consideration to the effect of the draught upon the added mass moment of inertia is taken into account in the study. In this paper, the general expression for the added mass coefficients of moment of inertia of arbitary two dimensional forms induced by the torsional vibration, was derived by the author. Hence, the coefficients for these forms are represented as functions of parameters, the section area coefficient and draft beam ratio, from which the added mass coefficients for arbitrary forms can be obtained. The result was shown in a chart for estimation of the added mass moment of inertia induced by the torsional vibration, as first trial, for the convenience of practical use.

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Design of Flexure Mounts for Satellite Primary Mirrors (인공위성 주반사경의 플렉셔 마운트 설계)

  • 엄태경;박강수;조지현;이완술;이준호;윤성기;이응식;우선희;이승훈
    • Proceedings of the Optical Society of Korea Conference
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    • 2003.07a
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    • pp.138-139
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    • 2003
  • 반사경을 지지하는 데에 있어서의 기계적, 열적 변형이 광학 부품에 미치는 영향을 최소화 하도록 광학 요소를 이러한 영향으로부터 차단하는 기계 장치를 플렉셔(flexure)라고 한다. 기계적 영향은 중력, 관성, 진동에 의한 하중 및 조립 시의 오차에 의한 응력 등에 의해 발생하는 변형을 말한다. 또한 열적 영향은 열적 평형 상태와 과도 상태 하에서 주위 환경의 온도변화에 의한 변형을 말한다. 예를 들어 작은 열팽창 계수를 가진 반사경 또는 렌즈와 큰 열팽창 계수를 갖는 지지구조가 어떤 온도 하에서 조립된 후 처음 온도와 다른 온도에 놓이는 경우를 생각해 보자. (중략)

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Variation of Dynamic Earth Pressure Due to Sliding of Retaining Walls (옹벽의 활동에 따른 배면 동적토압의 변화)

  • Yoon Suk-Jae;Kim Sung-Ryul;Hwang Jae-Ik;Kim Myoung-Mo
    • Journal of the Korean Geotechnical Society
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    • v.21 no.8
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    • pp.55-61
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    • 2005
  • Mononobe-Okabe method is generally used to evaluate dynamic earth pressure for the seismic design of retaining walls. However, Mononobe-Okabe method does not consider the effects of dynamic interactions between backfill soil and walls. In this research, shaking table tests on retaining walls were performed to analyze the phase and magnitude of dynamic earth pressure. The unit weight of walls, the amplitude of input acceleration and the base friction coefficient of walls were varied to analyze the influence of these factors on the dynamic earth pressure. Test results showed that the dynamic earth pressure was 180 degrees out of phase with the wall inertia force for the low sliding velocity of the wall, whereas small peaks of the dynamic earth pressure, which are in phase with the wall inertia force, were developed for the high sliding velocity of the wall. The amplitude of dynamic earth pressure was proportional to that of wall acceleration and the unit weight of the wall. In addition, the dynamic earth forces calculated by the Mononobe-Okabe method were the upper limit of the dynamic earth pressures.

Attitude Estimation of Agricultural Unmanned Helicopters using Inertial Measurement Sensors (관성센서를 이용한 농용 무인 헬리콥터의 자세 추정)

  • Bae, Yeonghwan;Oh, Minseok;Koo, Young Mo
    • Current Research on Agriculture and Life Sciences
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    • v.32 no.3
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    • pp.159-163
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    • 2014
  • Agricultural unmanned helicopters have become a new paradigm for aerial application. Yet, such agricultural helicopters require easy and affordable attitude control systems. Therefore, this study presents an affordable attitude measurement system using a DCM (direction cosine matrix) algorithm that would be applied to agricultural unmanned helicopters. An IMU using a low-cost MEMS and an algorithm to estimate the attitude of the helicopter were applied in a gimbals structure to evaluate the accuracy of the attitude measurements. The estimation errors in the attitude were determined in comparison with the true angles determined by absolute position encoders. The DCM algorithm and sensors showed an accuracy of about 1.1% for the roll and pitch angle estimation. However, the accuracy of the yaw angle estimation at 3.7% was relatively larger. Such errors may be due to the magnetic field of the stepping motor and encoder system. Notwithstanding, since the intrinsic behavior of the agricultural helicopter remains steady, the determination of attitude would be reliable and practical.

Fuel Droplet Entrainment and Low Frequency Instability in Hybrid Rocket Combustion (하이브리드 로켓 연소에서 연료액적의 발생과 저주파수 연소불안정)

  • Kim, Jina;Lee, Changjin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.7
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    • pp.573-580
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    • 2021
  • Paraffin wax is attracting many attentions for promising solid fuel of hybrid rocket because of its higher regression than other fuels. However, even with paraffin fuel combustion, unsteady low-frequency oscillation of combustion pressure is still observed. And, this is related to the formation of liquid layer and the entrainment of fuel droplets entering the axial combustion gas flow. This study investigates the effect of additional combustion of fuel droplets on the occurrence of low-frequency combustion instability. On the other hand, the formation of fuel droplets depends on Weber Number (the ratio of the inertial force to the surface tension of the liquid) and Reynolds Number of the oxidizer flow. Therefore, a laboratory-scale hybrid rocket was used to monitor the occurrence of combustion instability while changing We number. A series of combustion tests were conducted to control We number by changing the oxidizer flow rate or adding LDPE (low density polyethylene) to base fuel. In the results, it was confirmed that there is a critical We number above which the low-frequency combustion instability occurs.

Vibration Analysis of Large Structures by the Component-Mode Synthesis (부분구조진동형 합성방법에 의한 대형구조계의 진동해석)

  • B.H. Kim;T.Y. Chung;K.C. Kim
    • Journal of the Society of Naval Architects of Korea
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    • v.30 no.3
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    • pp.116-126
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    • 1993
  • The finite element method(FEM) has been commonly used for structural dynamic analysis. However, the direct global application of FEM to large complex structures such as ships and offshore structures requires considerable computational efforts, and remarkably more in structural dynamic optimization problems. Adoption of the component-mode synthesis method is an efficient means to overcome the above difficulty. Among three classes of the component-mode synthesis method, the free-interface mode method is recognized to have the advantages of better computational efficiency and easier implementation of substructures' experimental results, but the disadvantage of lower accuracy in analytical results. In this paper, an advanced method to improve the accuracy in the application of the free-interface mode method for the vibration analysis of large complex structures is presented. In order to compensate the truncation effect of the higher modes of substructures in the synthesis process, both residual inertia and stiffness effects are taken into account and a frequency shifting technique is introduced in the formulation of the residual compliance of substructures. The introduction of the frequency shrift ins not only excludes cumbersome manipulation of singular matrices for semi-definite substructural systems but gives more accurate results around the specified shifting frequency. Numerical examples of typical structural models including a ship-like two dimensional finite element model show that the analysis results based on the presented method are well competitive in accuracy with those obtained by the direst global FEM analysis for the frequencies which are lower than the highest one employed in the synthesis with remarkably higher computational efficiency and that the presented method is more efficient and accurate than the fixed-interface mode method.

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A Study on Vibration & Noise Reduction of Fast Back Feeding Device for Manufacturing Process (제조공정용 Fast Back 이송장치 진동·소음 저감에 관한 연구)

  • Han, Doo-Hee;Lee, Seung-Hun;Son, Yung-Deug
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.20 no.8
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    • pp.642-648
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    • 2019
  • This paper presents a fast back-type transfer device for snack food processing that uses the inertia of transferred material. A conventional conveying system is a drive system that uses a belt conveyor and mechanical crank, which generate noise and vibration and cause environmental pollution. Vibration and noise are reduced in the proposed fast back feeding device by using a counterweight. The crank drive unit was replaced with a linear servomotor, and an equilibrium device was designed to balance the force due to acceleration. This makes it is possible to adjust the forward and backward speed and acceleration through PLC control. A vibration damper device offsets the vibration force of the periodic shock form. The main cause of the vibration was identified through vibration analysis, and reduction measures were established. We verified the effectiveness of the vibration by making a prototype and performing about 10 vibration tests. Because no mechanical transducer is needed, energy loss, noise, and vibration do not occur, and the operating speed is not limited.