• Title/Summary/Keyword: 강제진동 해석

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Computer Simulation of Powertrain Forced Torsional Vibration (차량주행시 동력전달계의 강제진동 해석)

  • 최은오;안병민;홍동표
    • Journal of KSNVE
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    • v.7 no.5
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    • pp.853-860
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    • 1997
  • For this study, the multi-degree of freedom analysis model of torsional vibration was developed. This model is combined with mass moment of inertia and torsional spring in two wheel drive and four wheel drive vehicle. We compared and analyzed torsional vibration characteristics by natural frequencies and mode shapes which are obtained by free vibration analysis of this model. And we studied torsional vibration contribution of driveline elements by performing the forced vibration analysis of engine excitation torque. The validity of this model is demonstrated by the field test. The reduction effect of the torsional vibration along the driveline design factor is presented by the analytical results.

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Soil-Structure Interaction Analysis by Infinite Elements : Simulation of Forced Vibration and Earthquake Responses (무한요소를 이용한 지반-구조물 상호작용해석 : 강제진동 및 지진응답 해석)

  • Yun, Chung-Ban;Yang, Shin-Chu;Kim, Jae-Min
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 1993.04a
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    • pp.199-206
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    • 1993
  • 동적무한요소를 이용한 지반-구조물 상호작용에 대하여 연구하였다. 동적무한요소는 무한원방향으로 전파되어 나가는 여러종류의 지진파 성분을 동시에 모형화 할 수 있도록 개발된 축대칭요소로서, 구조물에서 멀리 떨어진 지반영역(외부영역)을 모형화 하는데 사용되었다. 반면, 구조물에 가까운 지반영역(내부영역)은 재래의 축대칭요소를 사용하여 모형화 하였다. 본 해석방법의 검증은 적충된 반무한 지반위에 놓여진 원형강판의 임피던스함수를 구하여, 이를 이론적 결과와 비교하는 방법으로 수행되었다. 또한, 지반에 일부가 묻힌 원통형구조물에 대하여 수행된 강제진동시험 결과와 실제 지진발생시 구조물의 거동기록을 같은 입력조건에 대하여 본 해법으로 구한 결과와도 비교하였다. 해석결과로 부터 본 해석방법이 구조물의 거동을 타당히 산정하여 줌을 알 수 있었다.

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Studies on Coupled Vibrations of Diesel Engine Propulsion Shafting (2nd Report : Analyzing of Forced Vibration with Damping) (디젤기관 추진축계의 연성진동에 관한 연구 (제2보: 강제 감쇠 연성진동 해석))

  • 이돈출;김의간;전효중
    • Proceedings of the Korean Society of Marine Engineers Conference
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    • 2000.11a
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    • pp.99-107
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    • 2000
  • With the results of calculation for natural frequencies, the forced reponses of coupled vibration of propulsion shafting were analysed by the modal analysis method. For the forced response analysis, axial exciting forces, axial damper/detuner, propeller exciting forces and damping coefficients were extensively investigated. As the conclusion of this study, some items are cleared as next. - The torsional amplitudes are not influenced by the radial excitation forces. - The axial vibrational amplitudes are influenced by the tangential exciting forces. An increase of amplitude is observed for the speed range in the neighbourhood of any torsional critical speed. - The coupling effect becomes larger if torsional and axial critical speed are closer together. - The axial exciting force of propeller is relatively strong, comparing with those of axial forces of cylinder gas pressure and oscillating inertia of reciprocating mechanism. Therefore, as a resume one can say, that- Torsional vibration calculation with the classical one dimension model is still valid. - The influence of torsional excitation at each crank upon the axial vibration is impotent, especially in the neighbourhood of a torsional critical speed. That means that the calculation of axial vibration with the classical one dimension model is insufficient in most of cases. - The torsional exciting torque of propeller can be neglected in most of cases. But, the axial exciting forces of propeller can not be neglected for calculating axial vibration of propulsion shafting.

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Forced Response Analyses of a Bladed Disk with Friction Dampers (마찰감쇠기가 있는 블레이드디스크의 강제진동해석)

  • Yoo, Jae-Han;Lee, In
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.5
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    • pp.15-23
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    • 2010
  • To reduce the vibration levels, additional dissipation elements such as dry friction dampers are sometimes integrated into bladed disk assembly. In this study, forced response analysis systems for a tuned bladed disk with friction dampers were developed and verified. For the efficient nonlinear vibration analysis, multi-harmonic balanced method and cyclic boundary condition were used. Also, mode shapes obtained using fictitious mass method were used to describe the motion of the structures with the concentrated structural nonlinearity, friction damper. The relative convergence of fictitious mass and traditional unconstrained modes were compared.

Dynamic Behaviour of Resilient Mounting System for the Marine Diesel Engine (선박용 디젤엔진 탄성지지계의 동적거동)

  • 김성춘;이돈출;김의간
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1993.04a
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    • pp.80-85
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    • 1993
  • 본 논문에서는 디젤 엔진의 탄성지지계에 작용하는 엔진 기진력에 대하여 검토하고, 탄성지지계의 진동 양상과 탄성지지를 통하여 선체로 전달되는 힘 을 계산하는 과정을 정식화하였다. 또한 이 결과를 고무형 탄성지지를 갖는 선박 추진용 디젤엔진과 발전기용 디젤엔진에 적용하여 탄성지지계의 자유 진동과 강제진동 해석을 수행하고 발전기용 디젤엔진의 탄성지지계에 대해 서는 계측을 행하여 계산 결과와의 비교 검토를 행하고자 한다.

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IV. 원심펌프 회전축계의 불평형응답에 미치는 유체력의 영향

  • 양보석;최원호
    • Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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    • 1986.06a
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    • pp.26-29
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    • 1986
  • 회전축계의 강제진동으로 가장 전형적이고 공업상 중요한 것은 넓은 의미로서 불평형 진동이다. 불평형은 회전체의 제작상 피할 수 없으며 진동이 전혀 문제가 되지 않는 정도로 제작하는 것은 경제적인 면에서도 불가능하다. 지금까지 미끄럼 베어링으로 지지된 회전축계의 불평형 응답 특성에 대하여는 여러 연구자에 의해 연구가 진행되고 있다. 수중에서 운전되는 펌프는 물의 감쇠작용 때문에 축진동 문제는 적다고 생각되어 펌프의 축진동에 관한 보고는 별로 없다. Black은 펌프의 축진동을 연구하여, 시일부분이 축진동 응답에 큰 영향을 미치는 것을 보였다. 그러나 시일형상에 따른 유체력 평가가 충분히 구명되지 않았기 때문에 환상 시일부분의 틈새,폭경비 및 압력차 등이 펌프진동에 어느 정도 영향을 미치는가가 충분히 검토 되어 있지않다. 이에 저자는 펌프용 시일의 유체력에 의한 진동 특성에 관한 일련의 연구를 진행하여 각종 시일의 유체력을 해석하였고, 이 유체력이 회전축계의 안정성에 미치는 영향을 검토하였으며 범용 안정성해석 프로그램을 개발하였다.

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Non-Linear Vibration Analysis of Mechanical Structures Using Component Mode Synthesis (부분구조합성법을 이용한 기계구조물의 비선형진동해석)

  • Kim, Jin-Wook;Iwatsubo, T.;Yang, Bo-Suk
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1996.04a
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    • pp.370-375
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    • 1996
  • 부분구조합성법의 하나인 구분모드합성법을 이용하여, 비선형 진동해석을 행하는 새로운 방법을 제안하였다. 제안하는 방법은 비선형 운동방정식에 섭동법을 이용하여 미소변동량에 관하여 정리한 각 차수의 운동방정식에 구분모드합성법을 적용하였다. 여기서 1차의 운동방정식의 외력항은 0차의 변위로 표현하는 것에 의해 각차의 운동방정식을 풀었다. 또한, 제안한 방법을 이용하여 문형구조모델의 비선형 강제진동 시각역응답을 구하고, 그 계산결과에 관해서 검토했다. 그 결과, 본 해석방법을 특히 감쇠가 없는 경우에 있어서 비선형이 실현되고 있는 것이 확인되었다.

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Studies on Coupled Vibrations of Diesel Engine Propulsion Shafting(2nd Report: Analyzing of Forced Vibration with Damping) (디젤기관 추진축계의 연성진공에 관한 연구(제2보 : 강제 감쇠 연성진동해석))

  • 전효중;이돈출;김의간;김정렬
    • Journal of Advanced Marine Engineering and Technology
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    • v.25 no.3
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    • pp.563-572
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    • 2001
  • With the results of calculation for natural frequencies the reponses of forced coupled vibration of propulsion shafting system were investigated by the modal analysis method. For the forced vibration response analysis, the axial exciting forces, the axial damper/detuner, propeller exciting forces and damping coefficients were extensively considered. As the conclusion of this study, some items are cleared as follows.-The torsional vibration amplitudes are not influenced by the radial excitation forces of the crank shaft. -The axial vibration amplitudes are influenced by the tangential exciting forces as well as the radial exciting forces of the crank shaft. The increase of the amplitudes is observed in the speed range at the neighbourhood of any torsional critical speed. 1The closer the torsional and axial critical speed. the larger coupling effect becomes. -The axial exciting force of propeller is relatively strong comparing with axial exciting forces of cylinder gas pressure and oscillating inertia of reciprocating mechanism. Therefore, the following conclusions are obtained. -Torsional vibration calculation with the classical one dimensional model is still valid. -The influence of torsional excitation at each crank upon the axial vibration is improtant. especially in the neighbourhood of a torsional critical speed. That means that the calculation of axial vibration with the classical one dimensional model is inaccurate in most of cases.

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Forced Vibration Analysis of Lattice Type Structure by Transfer Stiffness Coefficient Method (전달강성계수법에 의한 격자형 구조물의 강제진동 해석)

  • 문덕홍;최명수
    • Journal of KSNVE
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    • v.8 no.5
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    • pp.949-956
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    • 1998
  • Complex and large lattice type structures are frequently used in design of bridge, tower, crane and aerospace structures. In general, in order to analyze these structures we have used the finite element method(FEM). This method is the most widely used and powerful method for structural analysis lately. However, it is necessary to use a large amount of computer memory and computational time because the FEM requires many degrees of freedom for solving dynamic problems exactly for these complex and large structures. For analyzing these structures on a personal computer, the authors developed the transfer stiffness coefficient method(TSCM). This method is based on the concept of the transfer of the nodal dynamic stiffness coefficient matrix which is related to force and displacement vector at each node. And we suggested TSCM for free vibration analysis of complex and large lattice type structures in the previous report. In this paper, we formulate forced vibration analysis algorithm for complex and large lattice type structures using extened TSCM. And we confirmed the validity of TSCM through computational results by the FEM and TSCM, and experimental results for lattice type structures with harmonic excitation.

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A Study on Forced Vibration Tests on a Structure with Stud Type of Vibration Control Damper (스터드형 진동제어 강재댐퍼가 장착된 3층 강구조 골조의 강제진동실험에 관한 연구)

  • Lee, Seung-Jae
    • Journal of Korean Association for Spatial Structures
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    • v.6 no.2 s.20
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    • pp.115-121
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    • 2006
  • In recent years vibration control damper made of low yield point steel is expected to play an important role in controlling structural vibration induced earthquake and wind. But their dynamic characteristics and energy dissipation effects on the whole structure model are not clarified. In this paper, firstly, we presents the results of cyclic tests on low yield steel dampers. Secondly, forced vibration tests on existence three stories steel structure model with low yield point steel dampers are presented. Lastly, it is estimated energy amount which is dissipated through the hysteresis dampers by using two types of analytical models, hysteresis model and equivalent linear model.

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