• Journal of the Korean Society for Railway
• /
• v.14 no.1
• /
• pp.39-48
• /
• 2011

The paper describes four practical cases of railway structure concerning a three-dimensional numerical approach to analyse dynamic soil-structure interaction(SSI)of railway tracks on layered soil under transient load in the time domain. The SSI-Model has been implemented in TDAPIII accounting for nonlinear properties of the track and soil. The approach can be also be used to calculate vibration propagation in the soil and its effect on nearby buildings and structure. The Method is applied to analyse the dynamic response of railway tracks due to a moving wheel set. Finally some sample are given in order to reduce the vibration at the point of emission, at the transmission path and the structure itself.

• Journal of Astronomy and Space Sciences
• /
• v.6 no.2
• /
• pp.91-100
• /
• 1989

The mean orbital elements for geosynchronou8s satellite are developed in terms of non-singular orbital elements. The true satellite position oscillates about the position calculated from the mean elements due to short period perturbations to the satellite motion. The displacement of a geostationary satellite from this mean orbit position is less than 1800m. The mean elements of ec are obtained.

• Journal of KSNVE
• /
• v.9 no.6
• /
• pp.1259-1266
• /
• 1999

The objective of this investigation is to develop a compliant track link model and apply this model to the multi-body dynamic analysis of high mobility tracked vehicles. Two major difficulties encountered in developing the compliant track models. The first one is that the integration step size must be kept small in order to maintain the numerical stability of the solution. This solution deals with high oscillatory signals resulting from the impulsive contact forces and stiff compliant elements to represent the joints between the track links. The second difficulty is due to the large number of the system equations of motion of the three dimensional multibody tracked vehicle model. This problem was sloved by decoupling the equations of motion of the chassis subsystem and the track subsystems. Recursive methods are used to obtain a minimum set of equations for the chassis subsystem. Several simulation scenarios were tested for the high mobility tracked vehicle including accelaeration, high speed cruising, braking, and turning motion in order to demonstrate the effectiveness and validity of the methods proposed in this investigation.

• Bulletin of the Korean Space Science Society
• /
• 2009.10a
• /
• pp.46.4-47
• /
• 2009

인공위성은 지상에서 설계 제작된 후에 발사체에 탑재되어 궤도에 진입되어 위성에 부여된 고유임무를 수행하게 된다. 위성체가 임무를 수행하는 우주공간은 고진공 환경과 태양 복사열에 의한 고온 환경 및 극저온이 반복되는 가혹한 환경으로 특징지어진다. 때때로 위성체는 이러한 가혹한 우주환경의 영향으로 인해 주요 부품의 기능장애가 초래되기도 하며 이는 결국 임무의 실패로 이어지도 한다. 따라서 고진공과 극저온 환경으로 일컬어지는 우주환경을 지상에서 모사하여 위성체의 안정성 및 신뢰성을 시험하기 위해서 열진공 시험장비를 이용한 열진공시험을 수행한다. 한국항공우주연구원에서는 인공위성의 탑재체인 광학카메라의 국산화 개발을 위하여 우주공간의 고진공과 극저온 상태를 모사할 수 있는 $\varphi4m\timesL10m$ 규모의 광학탑재체 전용 열진공챔버를 국산화 제작하였다. 관측 위성용 광학카메라는 초고정밀 장비로서, 이를 테스트하기 위한 광학탑재체용 진공챔버는 특히 진동환경에 매우 민감한 하여 10-7 grms 이하의 진동레벨을 허용하고 있다. 그러나 진공용기는 지진 및 외부 환경으로부터의 시스템외부진동과 진공펌프 및 기타 장비들로부터의 내부 진동환경에 항상 노출되어 있으며, 가진 주파수가 구조물 자체의 고유진동수와 일치될 경우 공진이 발생하여 시스템에 큰 영향을 미칠 수 있으므로, 외부 진동 및 챔버 자체 진동이 광학계에 전달되지 않도록 진동차단장치가 필요하다. 이 논문에서는 광학탑재체 궤도환경시험용 챔버에 대한 진동차단장치의 개발 및 활용 예를 논의하고자 한다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 2002.05a
• /
• pp.911-916
• /
• 2002

One of important roles of concrete track is to reduce vibration transmitting to subgrade. In this paper, a numerical method for evaluating the effects of vibration reduction of concrete track is presented. Using the method, high frequency dynamic analyses and track-tunnel-soil interaction analyses are carried out for three types of concrete track in order to investigate the vibration reduction effects compared with normal ballast track.

• The Journal of the Convergence on Culture Technology
• /
• v.10 no.3
• /
• pp.833-838
• /
• 2024

The urban railway sleeper floating track(STEDEF) is a structure that structurally separates the sleepers and the concrete bed using sleeper boots and resilience pads to reduce vibration transmitted to the concrete bed. Recently, the resilience pads of sleeper floating tracks that have been in use for more than 20 years are deteriorating. Accordingly, in order to evaluate the performance of the resilience pad, a static spring stiffness test is being performed after extracting the resilience pad. This evaluation technique is performed after replacing the resilience pad in use. However, the track natural frequency can change depending on the resilience pad spring stiffness and the uplift and subsidence of the concrete bed. In this study, modal testing technique was used to evaluate the track natural frequency. For this purpose, the sleeper boots material, resilience pad spring stiffness, and track natural frequency according to concrete bed uplift and subsidence were measured using modal tests at a laboratory scale. It was analyzed that the natural frequency of the sleeper floating track was directly affected by changes in the spring stiffness of the resilience pad. In addition, the change in natural frequency due to the uplift and subsidence of the concrete bed was also found to be large. Therefore, it is believed that the modal test technique presented in this study can be used to evaluate the resilience pad deterioration and voided sleepers.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 1997.04a
• /
• pp.75-80
• /
• 1997

1999년 한반도 상공에 발사되어 21세기 한국의 우주 시대를 열어나갈 국내 최초의 다목적 실용위성인 KOMPSAT의 개발이 한국 항공 우주 연구소를 주관 기관으로 국내외의 여러 기업 및 연구기관들이 참여한 가운데 현재 진행 중이다. 본 논문에서는 위성체의 설계, 제작 및 시험의 국산화 일환으로 국내에서 제작된 이중 추진 장치(Dual Thrust Module)의 발사 환경 시험에 대한 과정 및 결과에 대하여 언급코자 한다. 일반적으로 목표 궤도에서 발사체로부터 분리된 위성체는 자세 제어를 수행하며, 또한 저궤도 위성의 경우 궤도상에 존재하는 공기등의 저항으로 인하여 빈번한 궤도수정이 필요하다. DTM은 이러한 궤도수정 업무를 담당하는 중요한 위성체의 부품이다. 그러나, 지상에서 발사시 발사체로부터 전달되는 진동 및 소음의 영향으로 인하여 기능 장애를 일으킬 우려가 있음에 따라, 제작된 DTM은 위성 본체에 장착되기 전 반드시 발사 시와 동일한 환경하에서 고유의 기능을 성공적으로 수행할 수 있는지에 대한 검증 절차가 필요하다. 본 연구에서는 DTM의 발사 환경 시험을 성공적으로 수행함으로써 위성체 및 부품의 시험기술을 축적하여 국내 위성 개발 분야에 기여코자 한다.

• Proceedings of the KSR Conference
• /
• 2003.05a
• /
• pp.343-348
• /
• 2003

As one of countermeasures for vibration and noise source which come from train operation in subway system, the heavy-weighted tunnel structure and the low-vibration track design have been adopted. In recent the low-vibration concrete track have been constructed to enhance the maintenance effectiveness as well as the reduction of vibration. This paper is explaining and evaluating of the characteristics of vibration and its effects comparing to tile ballast track, concrete track, and full surface supported floating slab track installed on Express bus terminal in Seoul subway No. 7 line.

• Journal of the Korean Society for Railway
• /
• v.15 no.5
• /
• pp.485-497
• /
• 2012

Recently, with increasing social interests on noise and vibration induced by railway traffic, the application of floating slab track that can efficiently reduce the railway vibration is increasing. In this study, to more accurately understand the dynamic behavior of the floating slab track, a laboratory mock-up test has been performed, and the static and dynamic behaviors at frequency range near the system resonance frequency were explored. Based on the test results, the design of the floating slab track and the structural analysis model used in the design have been verified. The analytic and test results demonstrate that the dominant frequency of the floating slab track occurs at the frequencies between vertical rigid body mode natural frequency and bending mode natural frequency, and the dominant deformation mode is close to the bending mode. This suggests that in the design of the floating slab track, the bending rigidity of the slab and the boundary conditions at slab joints and slab ends should be taken into consideration. Also, the analytic results by the two-dimensional finite element analysis model using Kelvin-Voigt model, such as static and dynamic deflections and force transmissibility, are found in good agreement with the test results, and thus the model used in this study has shown the reliability suitable to be utilized in the design of the floating slab track.

• The Bulletin of The Korean Astronomical Society
• /
• v.37 no.2
• /
• pp.136.2-136.2
• /
• 2012

저궤도지구관측 위성의 광학탑재체는 위성이 궤도에 진입한 이후 관측과 같은 주요 임무를 전담하는 중요 시스템이다. 광학탑재체가 장착된 위성이 발사체에 탑재되어 발사하는 순간부터 우주의 궤도에 진입하기까지 극심한 진동 환경에 노출된다. 이러한 상황을 예측하여 설계된 해당 시스템은 발사 이전에 진동 환경을 모사하는 시험을 통해 완벽하게 검증되어야 한다. 본 논문에서는 저궤도지구관측위성용 광학탑재체에 대하여 실시한 진동 환경 시험 방법 및 분석 내용을 소개하고자한다.