• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.32 no.6
• /
• pp.34-48
• /
• 2004

In this paper an optimization algorithm is suggested to reduce the huge computation time in the optimum design of large structures, especially in spacecraft structures. It combines the coupled load analysis model using a constrained mode of component mode synthesis and the modal transient analysis. The computer simulation code is developed and evaluated in optimizing spacecraft platforms. The developed algorithm can alleviate the computational load with adequate accuracy. From the optimization of a spacecraft structural member, the characteristics of each structural member can be understood.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 2009.10a
• /
• pp.582-583
• /
• 2009

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.36 no.7
• /
• pp.688-694
• /
• 2008

A rotordynamic analysis is performed for a high thrust class liquid rocket engine turbopump considering the dynamic characteristics of ball bearings and pump noncontact seals. Complex eigenvalue problems are solved to predict the rotating natural frequencies and damping ratios as a function of rotating speeds. Synchronous rotor mass unbalance response and time transient response analyses are also performed to figure out the rotor critical speed and the onset speed of instability. From the numerical analysis, it is found that the rear bearing stiffness is most important parameter for the critical speed and instability because the 1st mode is turbine side shaft bending mode. The pump seal effect on the critical speed is enlarged as the rear bearing stiffness decreases and the front bearing stiffness increases.

• Journal of Digital Convergence
• /
• v.13 no.1
• /
• pp.269-274
• /
• 2015

According to the development of IT industry, prevalence of AOI equipment is spreading, and also requiring the high resolution of the camera used in the equipment. The weight of the camera is increased to obtain a high resolution, and thus increases the vibration displacement is a problem occurring in the picturing, camera motion control also becomes difficult. In this study, using a finite element analysis program NX/NASTRAN, the transient response of the camera was analysed which is subjected to an impact force due to inertia. The finite element analysis result is correlated with laser interferometer measurement. When AOI equipment is restructuring, the correlated finite element analysis model can be used to verify the authenticity of the new design.

• Proceedings of the Korean Society of Precision Engineering Conference
• /
• 2010.05a
• /
• pp.1221-1222
• /
• 2010

• Journal of the Korean Society of Safety
• /
• v.8 no.1
• /
• pp.80-87
• /
• 1993

This paper summarizes an experimental and analytical study on the application of viscoelastic dampers as energy dissipation devices in structural applications. Shaking table tests are carried out on the viscoelastically damped structure and the obtained structural responses are compared to those of the inelastic analysis results for the same test structure with no dampers added. It can be concluded the viscoelastic dampers are effective in reducing excessive vibrations of structures under strong earthquake ground motions. It is also observed that the increase in structure's stiffness by the addition of dampers can not contribute to improving the seismic response of a structure. In general. the reduction of the seismic response by adding the dampers to the structure is mostly resulted from the increased damping effect. It is found that the modal strain energy method can be used to reliably predict the equivalent structural damping. and the seismic response of a viscoelastically damped structure can be accurately estimated by conventional modal analysis techniques.

• The KSFM Journal of Fluid Machinery
• /
• v.13 no.3
• /
• pp.18-23
• /
• 2010

This paper predicts the unbalance and transient (start-up) response of a 5MW industrial gas turbine by using commercial rotordynamic tool, DYNAMICS 4.3. The gas turbine is operated at 12,975rpm on squeeze film dampers or tilting pad bearings. The stiffness and damping coefficients of the squeeze film dampers and tilting pad bearings are estimated. It is seen that the vibration amplitude of the gas turbine rotor is sufficiently small around the critical speeds and at the rated speed.

• 전기의세계
• /
• v.15 no.3
• /
• pp.8-14
• /
• 1966

제어이론은 안정성판별을 중심으로 발달하여 왔으며 제어공학자체가 하나의 기술인 이상 안정판별법은 가능한 한 그 표현이 간단명료한 것을 요구하게 되었다. 과거에 연구되어 온 여러가지 안정판별법등은 즉 Routh 및 Hurwitz에 의한 방법, Nyquist 및 Michailov에 의한 방법 등, 정성적방법과 Bode 및 Nichols에 의한 방법, Evans에 의한 Root locus법, Bilharz 및 Frank에 의한 방법, Tsypkin 및 Bromberg에 의한 방법 등, 정량적인 취급방법 등이 연구발표되어 제어계통의 설허 및 해석에 이용되어왔다. 그러나 설계자들은 제어계통의 안정성판별에만 흥미를 갖는것이 아니라 안정도판별 즉 계통응답에 더 주의를 기우리게 된다. 특히 실시간응답에 대하여 명확한 해답을 요구한다. 본 고에서는 두개의 Parameter Plane Method의 기초를 다룬 것으로 특성방정식의 계수중에서 임의의 두개를 Parameter로 하는 것이며 과도해답 및 주파수응답을 요하는데 편리하나 임의의 두개의 계수만을 Paraweter로 하므로서 두개 이상의 Parameter가 존재하는 경우에는 부적당하다. 또한 우리나라에서도 시도된 바가 있다. 이와같은 것을 개선한것이 Siljak의 Parameter Plane Method이며 이것을 여기에 소개하고자 한다.

• Journal of the Korean Society for Precision Engineering
• /
• v.14 no.9
• /
• pp.124-129
• /
• 1997

The purpose of this study is to predict the stability and frequency response of multipurpose vehicle. The vehicle model has seven degrees of freedom. The motion equations are derived by using Lagrangian equation and linearized. The positions of eigenvalues of model which are dominated by lateral velocity, yaw rate, roll rate of sprung mass are used to predict the stability of motion. The resonse of sprung mass to steering wheel is simulated in time domain. It is predicted that the roll response of sprung mass would rather be improved by modifying the position of eigenvalues. The responses of sprung mass to steering wheel are also simulated in frequency domain. The magnitude and phase plots of gains are evaluated in driver's steering input frequency range.

• Journal of the Korea institute for structural maintenance and inspection
• /
• v.13 no.3 s.55
• /
• pp.164-172
• /
• 2009

Anchors and saddles are used to have sufficient geometrical rigidity and make target configuration of main cable of suspension bridge. Neglecting the sliding effect at saddles, points at them have been idealized as fixed nodes in lots of former studies. In general, sliding effects are reported to show significant structural behaviors of main cable and cause to the different responses of bridges. During early erection steps of the suspension bridge, especially, the sliding effect occurs easily because there is large difference of cable tension between main and side span in removing set-back ropes or not applying set-back. This study presents the finite element analysis considering to cable sliding effect and shows the comparison of differences between sliding and non-sliding at election sequence. The analysis of sliding between main cables and saddles needs to obtain more realistic responses because the analysis result can represent unfavorably different responses of bridges. Moreover, the sliding analysis method and results in this study can be used to basic criteria in engineering design and construction steps.