• Journal of the Korean Society of Safety
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• v.12 no.3
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• pp.17-22
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• 1997

This paper reals with the structure and function of duel mass flywheel. Damping effects of engine rotational fluctuation are compared with those of pre-damper clutch and duel mass flywheel and driven- system behavior is estimated engine idle r.p.m. The reason of gear rattle noise is higher in summer than winter and driving longer period than initial driving is due to affection by drag torque changing. The above-contents can be used on the design of clutch system and transmission matching including engine and duel mass flywheel.

• Proceedings of the KSME Conference
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• 2003.04a
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• pp.723-728
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• 2003

Planetary gearheads are widely used in the transmissions of samll precision mechanism, automation, robotics, heavy machinery and marine vehicle . Planetary gearheads have advantages that same-axle structure, high torque transmission, low noise in comparison with spur gearheads. And, planetary gearheads are typically specified in application where space is limited. In till study included planetary type gearheads design, manufacture, efficiency test. Especially, this time performed gear mesh stiffness simulation and vibration analysis for planetary gearheads.

• Proceedings of the KSR Conference
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• 2008.11b
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• pp.1634-1641
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• 2008

The shock absorbing equipment for railway rolling is one of the most important components. It's effects on the safety of both passengers and vehicle itself and reduce shock, vibration and noise. The shock absorber equipment is mainly consisted of the yoke, plate and rubber draft gear. The objective of the this paper is to evaluation of structure and strength for the yoke in railway vehicles. Structure and strength analysis has been performed by use of finite element method and experimental stress analysis.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.11
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• pp.883-891
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• 2018

In this paper, aerodynamic noise simulation was conducted using DES (Detached Eddy Simulation) and FW-H (Ffowcs Williams and Hawkings) acoustic analogy for the tandem cylinders which have configuration similar to a landing gear of airplanes. Numerical simulation for the tandem cylinders whose centers are 3.7D apart was carried out and results were compared with the measured data such as flow characteristics, pressure coefficients on the cylinder surfaces and far-field noise characteristics. It was confirmed that periodically shedded vortices released at the upstream cylinder and impinged on the downstream cylinder surface are major sources of aerodynamic noise. After verifying the computational method of using DES and FW-H acoustic analogy for predicting aerodynamic noise of tandem cylinders, additional simulation was conducted to examine the effect of attaching a splitter plate at the rear of the upstream cylinder. It was confirmed that the noise level in specific frequency band decreased significantly because the splitter plate changed the vortex shedding features and reduced dipole noise source.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1998.04a
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• pp.108-113
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• 1998

Nonclassically damping comes from drastic variations of energy absorption rates of the materials in different parts of structures, or from the external damping sources inserted into the structures. In this study, an approximate method based on the real valued normal modes to analyze the responses of a nonclassically damped system under stationary random excitations has been suggested. The dynamic responses of an aircraft landing gear under stationary random excitations has been analyzed using the proposed method. It has been found by a series of simulation that this method is superior to other approaches in respect of computational effort and accuracy.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2009.04a
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• pp.78-83
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• 2009

In this study, computer applied engineering (CAE) techniques are fully used to conduct structural and dynamic analyses of a whole huge wind turbine system including composite blades, tower and nacelle. For this study, computational fluid dynamics (CFD) is used to predict aerodynamic loads of the rotating wind-turbine blade model. Multi-body dynamic structural analyses are conducted based on the non-linear finite element method (FEM) by using super-element method for composite laminates blade. Three-dimensional finite element model of a wind turbine system is constructed including power train(main shaft, gear box, coupling, generator), bedplate and tower. The results for multi-body dynamic simulations on the wind turbine's critical operating conditions are presented in detail.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2005.11b
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• pp.41-44
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• 2005

This paper described improvement and operation of a 'Tail-Fan' anti-torque performance test system KARI (Korea Aerospace Research Institute) developed a 'Tail-Fan' anti-torque system of a helicopter and a performance test-rig to test the performance of the Tail-Fan. The test-rig was improved for full rotating test in 4300rpm(100%). Machinery and hydraulic parts ware changed to reduce vibration and to increase safety. To find the operation rotating speed for the performance test, vibration test were carried out rising accelerometers on tail gear box. The performance test conditions of the Tail-Fan to avoid a resonance were found from vibration test results. The Tail-Fan operation tests were performed safely frier to carry out performance test.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2002.11a
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• pp.329.2-329
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• 2002

This paper presents an improved escalator dynamic model so as to reflect the experimental observation on the pseudo-resonance affected by load applied. The experimental evidence reveals that backlash of gearbox as well as sag of driving chain are most critical factors to the pseudo-resonance in escalators. The dynamic model effectively reflects vibration characteristics measured in real escalators with respect to different conditions of driving chain and the number of passengers. (omitted)

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1990.10a
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• pp.187-191
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• 1990

그동안 실험을 통해 측정된 울산화력 BFP 진동 Data의 분석을 통하여 문제 가 되는 과도진동원에 대한 분석이 시도되었다. BFP의 이력과 그간의 측정 자료를 근거로 진동원과 진동에너지의 전달 경로를 가정하였고 각각의 진동 원에 대한 타당성 검토를 위하여 신호처리가 수행되었으며 그 결과로부터 BFP 과도진동 현상에 의해 야기되는 F 베어링 92.5 Hz의 진동에너지는 Voith Coupling의 기어에서 발생되었던 것으로 밝혀졌다. 문제의 해결을 위 해 치차를 대체시켰으며 진동값은 치차가 교환되기 전의 193.$\mu$m이 40.$\mu$m 이하로 줄 수 있었고 따라서 BFP는 안전운행 조건을 만족시키는 동급(Fair Operation)에 들게 됨을 볼 수 있다. BFP로부터 분리된 구동축 Gear는 육안상 크게 균열은 없어 보였으나 특정방향으로 일부 마모가 있어 보였으며 이는 유체와의 회전시 Unbalance에 의한 마모결과로 보여진다. 현 재 6-2 BFP에서 사용되었던 구동측 부품인 기어, Impellar는 치차마모등 비 파괴 정밀조사와 함께 Wet Balancing등의 측정이 진행되고 있다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2008.04a
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• pp.986-989
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• 2008

Recently the agitator are being widely used in the machine plan in order to increase the petrochemical industry. The agitator normally consist of impeller, shaft, hub, reduction gear and the driving motor. It is one of the key design issue to confirm that the vibration caused by the rotation of the shaft should not coincide with the natural frequency of the shaft itself. And petrochemical industry as well as plants have been in operation for long period beyond their original design lives. In this paper the vibration of Ox-Reactor Agitator is measured for check machine condition. The result of diagnosis and solution is discussed in this paper.