• Proceedings of the Korean Institute of Industrial Safety Conference
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• 1998.11a
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• pp.9-14
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• 1998

고강도 알루미늄 합금은 기술의 진보에 따라서 이용도가 높은 매우 중요한 재료로서, 잘 알려진 적용분야로서는 항공우주산업, 고속회전체, 항공기용재 등으로 많이 사용되고 있다. 고강도 알루미늄 합금은 Al-Cu-Mg(2000 series)를 기초로 둔것과 Al-Zn-Mg-Cu(7000 series)를 기초로 둔 것등이 있다. (중략)

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2000.06a
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• pp.1078-1083
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• 2000

A high speed rotor balancing machine was developed, which is capable of balancing a flexible rotor in high speed. The machine is largely consisted of vacuum chamber, oil supply system and vacuum pump system. And, in order to investigate performances of the machine, various tests were carried. After high speed rotor balancing of gas turbine engine rotor using influence coefficient method, the flexible engine rotor passed smoothly through its critical speed.

• Proceedings of the Korean Society of Machine Tool Engineers Conference
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• 2000.04a
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• pp.714-719
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• 2000

This paper describes a transfer matrix approach to analyze the dynamics of a high sped flexible rotor system supported at 2 positions by five ceramic bearings. The rotor system is modelled as lumped parameters in which many factors are considered not only lumped inertia or mass, bending moment, shear force but also gyroscopic effect and unbalance. The equation of motion is derived in the transfer matrix form, from which the eigenvalues equation is also derived. The transfer natural frequencies and modes. The eigenvalues, eigenmodes, campbell diagram, whirling critical speed, whirling modes, and the response of unbalance are calculated and discussed.

• Journal of the korean Society of Automotive Engineers
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• v.2 no.2
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• pp.25-30
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• 1980

자동차용 추진축의 위험회전속도를 원심력에 의한 탄성변형의 관계로부터 유도하여 보았다. 회전체의 unbalance량은 보통 회전속도에 관계없이 거의 일정하나 자동차용 추진축과 같이 외 경에 비하여 전장이 길고 고속회전하는 경우에는 축의 탄성변형에 의하여 unbalance량이 커진다. 회전속도에 따른 unbalance 변화량을 역시 원심력-탄성변형관계로부터 구하고 balancing을 위한 최적회전속도, tube의 편심도 기타 balancing 작업을 어렵게 하는 요소들에 대하여 정리하여 보았다.

• Journal of the KSME
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• v.35 no.1
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• pp.63-70
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• 1995

연사기는 섬유공정 중에서도 기본적인 제직 준비공정으로서 연사기 시장은 개발도상국의 섬유 산업 진흥과 더불어 날로 확대되고 있다. 최근 섬유산업이 요구하는 연사기의 성능은 범용성\ulcorner 효율성 및 다양한 보조기능(실잇기, 패키지교체, 왁스나 요일의 첨가 등의 기능을 자동화하는 것 등)의 구비 등이다. 연사기의 생산성은 스핀들의 회전수가 높을수록 증대되므로 고속회전체 기 술의 개발이 시급하며, 다양한 기능의 자동화에 대한 연구\ulcorner개발이 뒷받침되어야 한다. 현재 우 리나라 연사기 기술수준은 다른 섬유기계에 비해 선진국 수준에 가깝게 접근해 있다. 따라서 연사기는 우리 섬유기계 산업계와 기계공학인 여러분의 적극적인 관심과 노력이 모아진다면 비 교적 단시간 안에 선진국과 견줄 수 있는 분야라고 생각된다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.17 no.7
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• pp.175-181
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• 2016

This occurs when the unbalanced rotating body is inconsistent with the mass center line axis geometric center line. Wheelsets are assembled by a single axle with two wheels and a rotating body of a running railway vehicle. Owing to non-uniformity of the wheel material, the wear, and error of the wheel and axle assembly may cause an imbalance. Wheelsets will suffer the effects of vibrations due to the unbalanced mass, which becomes more pronounced due to the thin and high-speed rotation compared to the shaft diameter This can affect the driving safety and the running behavior of a rail car during high-speed running. Therefore, this study examined this unbalanced wheel using a railway vehicle multibody dynamics analysis tool to assess the impact of the dynamic VI-Rail movement of high-speed railway vehicles. Increasing the extent of wheel imbalance on the analysis confirmed that the critical speed of a railway vehicle bogie is reduced and the high-speed traveling dropped below the vehicle dynamic behaviour. Therefore, the adverse effects of the amount of a wheel imbalance on travel highlight the need for management of wheel imbalances. In addition, the static and dynamic management needs of a wheel imbalance need to be presented to the national rail vehicles operating agency.

• Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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• 1987.11a
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• pp.75-78
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• 1987

저어널베어링으로 지지되고 있는 축 및 베어링 시스템에서 축이 고속으로 회전할 때, 어느 회전수 이상에서 시스템의 안정성이 깨어져 축의 진동진폭이 갑자기 커지는 Self-excited whirl이라 불리우는 불안정 현상이 존재한다. 따라서 고속회전체에 적용되는 공기윤활 저어널베어링에 있어서 안정성 문제는 설계 및 운전에 고려되어야 하는 지배적 요인 중의 하나가 된다. Lund, Fleming과 Cunningham, Mori 들은 외부가압형 공기윤활 저어널베어링의 안정성을 이론적으로 해석하였으며 Pincus는 Self-acting형 공기베어링에서 편심율이 작은 경우 2-Lobe 베어링이나 3-Lobe 베어링이 원형베어링보다 강성도와 감쇠력이 더 크므로 안정성이 더 좋을 것이라고 정성적으로 예측했다. 그러나 외부가압 공기윤활 저어널베어링의 안정성에 비원형 베어링의 유효성은 김 두환, 김 금모, 박 종포 등에 의하여 실험적으로 제시되었다. 따라서 본 연구는 외부가압형 공기윤활 저어널베어링에서 Multi-lobe 형상의 베어링이 축 및 베어링 스스템의 안정성에 미치는 효과를 원형의 경우와 비교하여 이론적으로 해석하여 Multi-lobe베어링의 유효성을 보이고 이에 적용 가능한 Programing을 하여 몇가지 경우에 대하여 계산을 하고자 한다.

• Journal of the Korean Society for Precision Engineering
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• v.15 no.11
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• pp.233-243
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• 1998

The demand of high speed machining is increasing due to the high speed cutting and grinding provides high efficiency of process, short process time, improved metal removal capacity and better surface finish. Active magnetic bearings allow much high surface speed than conventional ball bearings and therefore greatly suitable for high speed cutting or grinding. This paper describes a design process of an active magnetic bearing system for a high speed grinding spindle with power 5.5kW and maximum speed 60,000rpm. Magnetic actuators are designed by the magnetic circuit theory considering static load condition, and examined with FEM analysis. Dynamic characteristics are also considered, such as bandwidth, stiffness, natural frequency and static deflection. System characteristics are simulated with a rigid rotor model.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2007.05a
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• pp.859-865
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• 2007

This paper presents a method to analyze the unbalance response of a high speed polygon mirror scanner motor supported by sintered bearing and flexible supporting structures by using the finite element method and the mode superposition method. The appropriate finite element equations for polygon mirror are described by rotating annular sector element using Kirchhoff plate theory and von Karman non-linear strain, and its rigid body motion is also considered. The rotating components except for the polygon mirror are modeled by Timoshenko beam element including the gyroscopic effect. The flexible supporting structures are modeled by using a 4-node tetrahedron element and 4-node shell element with rotational degrees of freedom. Finite element equations of each component of the polygon mirror scanner motor and the flexible supporting structures are consistently derived by satisfying the geometric compatibility in the internal boundary between each component. The rigid link constraints are also imposed at the interface area between sleeve and sintered bearing to describe the physical motion at this interface. A global matrix equation obtained by assembling the finite element equations of each substructure is transformed to a state-space matrix-vector equation, and both damped natural frequencies and modal damping ratios are calculated by solving the associated eigenvalue problem by using the restarted Arnoldi iteration method. Unbalance responses in time and frequency domain are performed by superposing the eigenvalues and eigenvectors from the free vibration analysis. The validity of the proposed method is verified by comparing the simulated unbalance response with the experimental results. This research also shows that the flexibility of supporting structures plays an important role in determining the unbalance response of the polygon mirror scanner motor.

• Tribology and Lubricants
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• v.38 no.5
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• pp.205-212
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• 2022

This paper presents experimental measurements of the structural characteristics of a two-pad beam-type gas foil journal bearing and its rotordynamic performance for a high-speed motor-driven turbocompressor. The test bearing had two top foils and two beam foils, each with an arc length of ~180°. Each beam foil was etched to obtain 40 beams with six geometries of different lengths and widths. The insertion of beam foils into the bearing housing produces equivalent beam heights. The structural tests of the bearing with a non-rotating journal revealed a smaller bearing clearance and larger structural stiffness for the load-on-pad configuration than for the load-between-pads configuration. Rotordynamic performance measurements during driving tests up to 100 krpm demonstrated synchronous vibrations and subsynchronous vibrations with large amplitudes. The test was repeated after inserting the shim between the top foil and beam foil to reduce the bearing radial clearance. The reduced bearing clearance resulted in a reduction in the peak amplitude of the synchronous vibrations and an increase in the speed at which the peak amplitude occurred. In addition, the onset speed and amplitude of the subsynchronous vibrations were dramatically increased and diminished, respectively. The rotor coast-down tests at 100 krpm show that the reduction in the bearing clearance extends the time to rotor stop, thus implying an improvement in hydrodynamic pressure generation and a reduction in bearing frictional torque.