• Tribology and Lubricants
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• 제38권2호
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• pp.63-69
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• 2022

In this research, the rotordynamic characteristics of the labyrinth seal with and without swirl brake were predicted using the computational fluid dynamic (CFD) model. Based on previous studies, a simple swirl brake consisting of square vanes without stagger angle is designed and placed in front of the seal inlet. The rotating frame of reference is utilized to consider the whirling motion of the rotor in the steady-state analysis since the whirling motion is transient behavior in nature. CFD analysis was performed in the range of -1 to 1 pre-swirl ratio for a given seal and swirl brake design and operating conditions. The CFD analysis result shows that the swirl brake effectively reduces the pre-swirl since the circumferential fluid velocity of labyrinth seal with swirl brake was lower than that without swirl brake. The cross-coupled stiffness coefficient, which is greatly affected by the circumferential fluid velocity, increased with an increasing pre-swirl ratio in a seal without a swirl brake but showed a low value in a seal with a swirl brake. The change in the damping coefficient was relatively small. The effective damping coefficient of the labyrinth seal with swirl brake was generally constant and showed a higher value than the labyrinth seal without swirl brake.

• Tribology and Lubricants
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• 제24권3호
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• pp.147-153
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• 2008

The effect of oil supply pressure on the performance of vapor cavitated short squeeze film dampers is examined. Vapor cavitation is characterized by film rupture occurring as a result of evaporating oils. The pressure of vapor cavity in the film is almost zero in absolute pressure and nearly constant. Pan's model about the shape of vapor cavity is utilized for studying the effect of vapor cavitation on the damping capability of a short squeeze film damper. As the level of oil supply pressure is increasing, vapor cavitation is suppressed so that the direct damping coefficient increases and the cross coupled damping coefficient decreases. Futhermore, the analysis of the unbalance responses of a rigid rotor supported on cavitated squeeze film dampers shows that a significant reduction in rotor amplitude and force transmissibility is possible by controlling the oil supply pressure into short squeeze film dampers.

• 대한조선학회논문집
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• 제40권1호
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• pp.1-7
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• 2003

The effect of the passive anti-rolling tanks(ART) decreases when the roll period of the vessel does not match the designed oscillating period of the fluid in the tank. In order to improve the effect of the passive ART, the damping plates are installed in the lower duct of the ART to adjust the oscillating period of the fluid. The effects of the damping plates on the oscillating period of the fluid and the changes of the stabilizing moments are examined through the series of bench tests. Acryl model tank larger than 1m breadth is made to minimize the viscous effect of the tank and the stabilizing moments of the tank are measured for various roll angles. Using the obtained tank damping coefficient, RAO(Response Amplitude Operator) value in the resonance range is computed and the stabilizing effect of a ART has been estimated.

• 동력기계공학회지
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• 제3권3호
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• pp.91-96
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• 1999

This study is about the design and analysis ot a suspension damper for truck driver's seat to improve the ride comfort. Trucks are usually subjected to hostile driving environments. Therefore, many truck driver's seat have suspension seats to isolate the vibration from the cab floor panel. Because the vehicle suspension system can reduce the primary vibration from the ground, only low frequency vibration can be transmitted to the driver's seat. But, this low frequency vibration can be harmful to the driver. The seat damper is very critical element to improve the ride comfort for the driver. In this study, a four-stage damper is designed and analyzed for the vibration capability. The damping coefficient of this damper can lie manually controlled in response to the road and driving environment.

• 한국소음진동공학회논문집
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• 제12권8호
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• pp.639-647
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• 2002

The nonlinear vibration of the thin perforated plate is analyzed in consideration of the V-shaped tension distribution and the effect of wire impact damping. The reduced order FEM model of the tension plate is obtained from dynamic condensation for the mass and stiffness matrices. Tension wire is modeled using the lumped parameter method to effectively describe its contact interactions with the plate. The nonlinear contact-impact model is composed of spring and damper elements, of which parameters are determined from the Hertzian contact theory and the restitution coefficient, respectively. From the evaluation of the computational accuracy and computation time for the deduced impact stiffness and damping coefficient, we determined proper values for the simulation works, accounting for the computational accuracy as well as the computational efficiency. Finally we discussed the results of nonlinear nitration analysis for variations of their design parameters.

• 한국해안·해양공학회논문집
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• 제21권2호
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• pp.127-135
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• 2009

Reid and Kajiura(1957)은 해저면에 무한한 깊이의 투수층이 존재할 경우에의 파의 감쇠율을 유도하였다. 본 연구에서는 유한한 깊이의 투수층이 존재할 경우에의 파의 감쇠율을 선형파이론을 이용하여 유도하였다. 그리고 이를 확장하여 해저면에 재질이 다른 2 층 또는 3 층의 투수층이 존재할 경우에 파의 감쇠율을 제시하였다. 다음으로 이를 완경사 방정식에 적용하여, 해저면에 투수층이 존재할 경우에의 파의 투과율을 계산하였으며, 1층 투수층이 존재할 경우의 수치계산결과를 Flaten and Rygg(1991)의 적분식 방법과 비교하여 검증하였다.

• 한국항해항만학회지
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• 제26권1호
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• pp.101-105
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• 2002

컨테이너 크레인 스프레더는 체결시 발생하는 충격으로 인해 많은 고장이 발생한다. 이러한 충격력을 줄이기 위해 2자유도계 유압충격흡수장치를 설계하여 실린더 벽면의 치수변화가 감쇠계수에 미치는 영향에 대해 연구하였다. 내부압력이 작용할 때 벽면 치수를 2～3Omm로 변화시켜 이때 발생하는 실린더 벽면과 피스톤 사이의 틈새는 측정한 결과 Sun이하의 치수에는 벽면형상 굴곡 되며 l0mm이상의 치수에서 감쇠계수에 영향을 미치지 않는 것을 알 수 있다.

• Computers and Concrete
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• 제26권1호
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• pp.31-52
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• 2020

This paper investigates the size dependent effect on the vibration analysis of a porous nanocomposite viscoelastic plate reinforced by functionally graded-single walled carbon nanotubes (FG-SWCNTs) by considering nonlocal strain gradient theory. Therefore, using energy method and Hamilton's principle, the equations of motion are derived. In this article, the effects of nonlocal parameter, aspect ratio, strain gradient parameter, volume fraction of carbon nanotubes (CNTs), damping coefficient, porosity coefficient, and temperature change on the natural frequency are perused. The innovation of this paper is to compare the effectiveness of each mentioned parameters individually on the free vibrations of this plate and to represent the appropriate value for each parameter to achieve an ideal nanocomposite plate that minimizes vibration. The results are verified with those referenced in the paper. The results illustrate that the effect of damping coefficient on the increase of natural frequency is significantly higher than the other parameters effect, and the effects of the strain gradient parameter and nonlocal parameter on the natural frequency increase are less than damping coefficient effect, respectively. Furthermore, the results indicate that the natural frequency decreases with a rise in the nonlocal parameter, aspect ratio and temperature change. Also, the natural frequency increases with a rise in the strain gradient parameter and CNTs volume fraction. This study can be used for optimizing the industrial and medical designs, such as automotive industry, aerospace engineering and water purification system, by considering ideal properties for the nanocomposite plate.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2008년도 춘계학술대회논문집
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• pp.250-254
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• 2008

Eddy currents are induced when a nonmagnetic conductive material is moving subjected to the magnetic field due to a permanent magnet. These currents circulates in the conductive material and are dissipated, causing a repulsive force between the magnet and the conductor. Using this concept, the eddy current damping can be used as a viscous damping. The present study investigates the characteristics of a magnetic damping analytically and experimentally. The theoretical model of a eddy current damping is developed from electromagnetics and is verified from experiments. The drop test of a magnet in the cooper tube shows that the present model can accurately predict the damping force. Additionally, the dynamic test of a eddy current damping is carried to verify the present model.

• 한국항공우주학회지
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• 제36권5호
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• pp.420-427
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• 2008

접힌 공력면이 전개하는 운동을 모사하기 위하여 전개 운동 방정식을 수립하고 공력면에 작용하는 모멘트 등을 모델링하였다. 공력에 의한 롤 모멘트는 정적 롤 모멘트와 감쇠 모멘트로 이루어져 있으며 정적 롤 모멘트는 전개 하중 측정을 위한 풍동 시험을 통하여 획득한 정적 롤 모멘트 계수로부터 계산된다. 롤 감쇠 계수는 패널법을 이용한 수치 해석을 통하여 산출되었는데 전개 각속도로부터 유발된 받음각에 상응하는 변위각을 공력면에 적용하여 수치해석을 하였다. 공력면 형상에 적용한 변위각은 회전 중심으로부터 공력면 끝단까지 선형적으로 증가하며 회전 중심에서는 변위가 없다. 롤 감쇠 계수는 전개 각속도에 따른 롤 모멘트 계수의 변화율로 계산되며 공력조건과 전개각의 함수이고 전개 각속도에 대해서는 일정하다고 가정하였다. 롤 감쇠를 포함하여 모사된 공력면의 전개 모사는 시험과 비교하여 유사한 결과를 보여주었다.