• Title/Summary/Keyword: 진동억제

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An Analysis on Combustion Instability in Solid Rocket Motor of 230mm Grade (230mm급 고체 추진기관의 연소불안정 거동 현상 분석)

  • Kwon, Tae-Hoon;Rho, Tae-Ho;Suh, Hyuk
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.05a
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    • pp.177-180
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    • 2009
  • A Possibility of combustion instability on longitudinal mode has a high level at large scale of L/D. Solid propellant has a metal particle and a grain of control to pressure oscillation. Solid rocket motor in slotted-tube grain controls pressure oscillation of longitudinal mode. If slot length is shot, pressure oscillation of longitudinal mode is amplified by cylinder part after middle phase of total burn time. A study has analyzed pressure oscillation of longitudinal mode at spectrum and acoustic modal analysis at pressure of result on static firing test.

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Suppression of Machine Tool Spindle Vibration by using TiC-SKH51 Metal Matrix Composite (TiC-SKH51 금속 복합재를 이용한 공작기계 주축 진동 억제에 관한 연구)

  • Bae, Wonjun;Kim, Sungtae;Kim, Yangjin;Lee, Sang-Kwan
    • Composites Research
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    • v.33 no.5
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    • pp.262-267
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    • 2020
  • With increasing demands for high-speed machining and lightweight design of machine tools, increasing likeliness of generation of machine tool spindle vibrations has become an important issue. Spindle vibration has a significant impact on the surface finish of the workpiece in ultra-precision machining. It is necessary to resolve the machine tool spindle vibration in various machining processes to improve machining accuracy. In this paper, a TiC-SKH51 metal-matrix composite was used to suppress the vibration of the machine tool spindle. To confirm the dynamic characteristic of the TiC-SKH51 composite, impact hammer tests were conducted. After verifying the reliability of a finite element analysis (FEA) by comparing the results of the impact hammer test with the modal analysis using FEA, the analysis of the machine tool spindle model was performed. The FEA results show that the TiC-SKH51 composite applied machine tool spindle can be utilized to suppress the vibration generation.

Rotational Performance Test for the Flywheel Energy Storage System (플라이휠 에너지 저장장치 회전 성능 평가)

  • Lee, Jeong-Phil;Han, Snag-Chul;Han, Young-Hee;Park, Byeong-Cheol;Jung, Se-Yong;Park, Byung-Jun;Sung, Tae-Hyun
    • Proceedings of the KIEE Conference
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    • 2009.07a
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    • pp.692_693
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    • 2009
  • 본 논문은 초전도 플라이휠 에너지 저장장치(Superconductor Flywheel Energy Storage System : SFES)의 고속회전 시험을 통하여 휠의 진동 특성을 평가 하였다. 초전도 베어링(Superconductor Magnetic Bearing : SMB)은 동작시키기 않고 플라이휠의 외부 외란이나 예측하지 못한 진동을 억제할 수 있도록 설치된 전자석 댐퍼(Electric Magnetic Damper : EMD) 만을 이용해 휠을 부양하고 고속회전 시험을 수행하였다. 이를 통하여 플라이휠의 고속 회전 운전영역에서 EMD는 충분한 진동억제 능력을 보임을 확인 하였다.

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Vibration Suppression Control of Constrained Spatial Flexible Manipulators (구속받는 3차원 유연 매니퓨레이터의 진동억제 제어)

  • 김진수;우찌야마마사루
    • Journal of the Korean Society for Precision Engineering
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    • v.17 no.7
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    • pp.189-195
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    • 2000
  • For free motions, vibration suppression of flexible manipulators has been one of the hottest research topics. However, for constrained motions, a little effort has been devoted for vibration suppression control. Using the dependency of elastic deflections of links on contact force under static conditions, vibrations for constrained planar two-link flexible manipulators have been suppressed successfully by controlling the contact force. However, for constrained spatial multi-link flexible manipulators, the vibrations cannot be suppressed by only controlling the contact force. So, the aim of this paper is to clarify the vibration mechanism of a constrained, multi-DOF, flexible manipulator and to devise the suppression method. We apply a concise hybrid position/force control scheme to control a flexible manipulator modeled by lumped-parameter modeling method. Finally, a comparison between simulation and experimental results is presented to show the performance of our method.

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Torsional Vibration Control of a Rotating Shaft in Starting and Stopping Process (회전축의 기동.정지시의 비틀림 진동제어)

  • 김중배;이상조;박영필
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.16 no.3
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    • pp.459-467
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    • 1992
  • 본 연구에서는 비틀림 진동계에 있어서의 비틀림 진동현상을 억제하도록 제어 하기 위하여 최적제어 이론에 기초한 모델추종법을 비틀림 진동계에 적용하였다. 디 지탈 컴퓨터에 의한 제어를 위하여 제어 알고리즘은 디지탈 설계로 되어 있다. 제어 는 각속도와 비틀림 진동제어의 양면으로 수행되며, 축의 각속도는 모델의 출력을 추 종하게 되며 이와 동시에 비틀림각도 감소하게 된다.

부분 소음원들의 포함과 삭제를 위한 STSF 기법에서의 Reference의 사용

  • Hald, J.
    • Journal of KSNVE
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    • v.2 no.1
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    • pp.3-14
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    • 1992
  • 음장의 공간적 변환(Spatial Transformation of Sound Field; STSF)기법의 주요 원리를 간단히 소개한 뒤, STSF에서 Reference 신호의 사용을 보다 상세히 취급하고자 한다. Reference의 보통의 형태(표준 Reference)는 음장 모델에 포함될 전체음장의 일부분, 즉 이 Reference의 연관이 있어 포함될 부분을 결정한다. 결국 한 개 의 표준 Reference는 항상 적용되어져야 한다. 2번째 Reference의 형태(삭제용 Reference)는 모델로부터 원치 않는 무관한 음장성분을 제거하는데 적용된다. 이 Reference와 밀접한 음장 부분이 모델로부터 제거될 것이고, 그렇지 않는 경우는 포함된다. 실제 예에서는 삭제용 Reference가 암소음의 억제와, 음원의 어떤 독립 적인 성분의 억제를 위해 어떻게 적용되는가를 보인다.

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Vibratory Loads Reduction of a Rotor in Slow Descent using Higher Harmonic Control Technology (고조파제어(HHC) 기법을 이용한 저속 하강 비행중인 로터의 진동하중 억제에 관한 연구)

  • You, Younghyun;Jung, Sung Nam
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.6
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    • pp.440-447
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    • 2013
  • In this paper, a higher harmonic control (HHC) methodology is applied to find the optimum input scenario for the vibratory hub loads reduction. A comprehensive aeroelastic analysis code, CAMRAD II, is used to model the HART (Higher-harmonic-control Aeroacoustic Rotor Test) II rotor, and parametric study is conducted for the best HHC inputs leading to a minimum vibration (MV) condition. The resulting outcomes are compared with the earlier HART II test results. It is indicated that the control input adopted in the MV condition showed less satisfactory results. The new MV condition obtained in the present investigation can achieve 45% lower vibration level than the baseline uncontrolled condition. The optimum HHC input results lead to 3/rev harmonic input having $0.8^{\circ}$ amplitude and $350^{\circ}$ phase angle. About 5% reduction in the required power is possible but accompanies with the increase of vibration level.

Study on the Vibration Control of Footbridge by Using Tuned Mass Damper(TMD) (Tuned Mass Damper(TMD)를 이용한 보도교의 진동제어에 대한 연구)

  • 권영록;최광규
    • Journal of the Earthquake Engineering Society of Korea
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    • v.7 no.6
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    • pp.9-15
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    • 2003
  • This paper describes a vibration control by using tuned mass damper(i.e., TMD) for an existing footbridge. The footbridge is the simple steel box girder bridge with main span length of 47.7m. This bridge has light weight, low damping and the 1st bending frequency of 1.84㎐. Its frequency is close to a walking cycle, which is 2㎐. Therefore the uncomfortable resonant vibrations due to a pedestrian walking have occurred frequently. The vibration control by means of TMD for suppressing the pedestrian induced vibration was conducted. Taking into account economical benefits and the easiness of installation, a compact TMD installed within a handrail was designed. From field tests of the TMD, it was confirmed that the structural damping of the bridge via. the compact TMD was enhanced by 13 times and the resonant vibration due to pedestrian walking was suppressed.

3-Axis Modeling and Small Angle Maneuver Including Vibration Suppression for a Satellite (인공위성의 3축 모델링과 진동억제를 포함한 소각선회)

  • Lee, D.W.;Cho, K.R.
    • Journal of Advanced Navigation Technology
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    • v.4 no.2
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    • pp.103-113
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    • 2000
  • There are several methods in the mathematical modeling of a satellite with flexible appendages. In this paper, the hybrid Lagrange's equations of motion using assumed modes method are derived. The assumed modes method is one of approximate methods which have shorter calculation time due to low-dimension compare with FEM. These consist of three-equations about angular velocities and two-equations about flexible deformations, and physically represent interaction between hub and solar panel. In an attitude control, a control law is designed to minimize a given performance index considering not only control input but also vibration suppression. For these purpose, this paper applies LQG and LQG/LTR schemes to this model and finally show the capability for attitude control including vibration suppression. Especially, this paper shows the method of assumption as nonsingular system through singular value division for LQG/LTR design.

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A Study on the Dynamic Stability and Vibration Control of Cantilevered Pipes Conveying Fluid (유체유동을 갖는 외팔 송수관의 동적 안정성과 진동제어에 관한 연구)

  • 류봉조;정승호;강용철
    • Journal of KSNVE
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    • v.8 no.1
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    • pp.171-179
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    • 1998
  • The present paper deals with the dynamic stability and vibration suppression of a cantilevered flexible pipe having a tip mass under an internal flowing fluid. The equations of motion are derived by energy expressions using extended Hamilton's principle, and some analytical results using Galerkin's method are presented. Finally, the vibration suppression technique by means of an internal fluid flow is demonstrated experimentally.

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