• 소음진동
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• 제10권3호
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• pp.465-473
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• 2000

In this crankshaft of marine diesel engines the exciting torques are produced by gas pressure and reciprocating masses. These torques are periodically changing and are extremely out of balance. To calculate the torsional vibrations of propulsion shafting caused by unbalanced torque the torque harmonics are utilized. Until now to calculate the torsional vibrations of propulsion shafting. the torque harmonics have been supplied by the engine maker. When the torque harmonics of an engine are not available the torque harmonics of a similar engine type had to be used. However such data is not suitable for the reliable calculations of torsional vibrations. In this paper the combustion characteristics of marine diesel engines including $\rho{-}\upsilon$ diagram are investigated and the torque harmonics based on these are theoretically calculated. reliability of the calculations is confirmed by comparing them with those of an engine maker. This study should prove useful for the calculations of torsional vibrations for diesel engine propulsion shafting. particularly for 4-stroke engines whose torque harmonics are difficult to obtain directly from the engine and not ordinarily supplied by the engine maker.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2004년도 추계학술대회 논문집
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• pp.166-169
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• 2004

A fatigue test was used to evaluate the fatigue life of an actual structure. The loaded state and the constraint condition of an actual structure must be same as the specimen in order to apply the test results to an actual structure by the specimen. The loaded state and constraint conditions can't be same as the specimen in the actual structure which is complicated. In order to reduce these differences, an actual structure test with a lot of frequencies is need to get a fatigue life curve. Therefore, ten sets of accelerated test units which attached unbalanced mass were composed in this study. Acceleration history about the vibration of an actual structure was acquired. Rainflow counting was used on acceleration history, and the life curve return formula was assumed. The return formula that damage satisfied `1' was acquired in a feedback process by the Miner's rule, which was the linear cumulative damage theory. A conservative fatigue life curve was determined with a return formula to have been presumed by each set. The fatigue life of regular rpm condition was calculated by these conservative fatigue life curves.

• 조명전기설비학회논문지
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• 제18권3호
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• pp.114-119
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• 2004

차량이라는 특수한 장소에 적용되는 산소 발생 장치는 소형/경량화 및 소음, 충격, 발열에 대한 문제점을 무시할 수 없다. 이러한 문제점을 해결할 방법으로 BLDC를 이용하여 모터의 발열을 줄이고 합성 제올라이트 NaX형을 사용한 베드로 소형에서도 고농도의 산소를 발생시킬 수 있게 하였다. 또한, 합성 제올라이트 NaX형의 특성으로 인한 질소의 강제 탈착을 진공펌프 한 대로 사용하기 위하여 Two Head 진공펌프 Pump Type을 개발하여 소비 전력을 줄이고 소형/경량화 및 저소음, 충격/발열 문제를 해결할 수 있었다.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2001년도 춘계학술대회 논문집 전기기기 및 에너지변환시스템부문
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• pp.33-36
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• 2001

Torque ripple control of brush less DC motor has been the main issue of the servo drive systems in which the speed fluctuation, vibration and acoustic noise should be minimized. Most methods for suppressing the torque ripples require Fourier series analysis and either the iterative or least mean square minimization. In this paper, the novel approach to achieve the ripple-tree torque control with maximum efficiency based on the d-q-0 reference frame is presented. The proposed method optimize the reference phase current waveforms including even the case of 3 phase unbalanced condition, and the motor winding currents are controlled to follow up the optimized current waveforms by delta modulation technique. As a result, the proposed approach provides a simple and clear way to obtain the optimal motor excitation currents. The validity and practical applications of the proposed control scheme are verified through the simulations and experimental results.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2006년도 제37회 하계학술대회 논문집 B
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• pp.765-766
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• 2006

Interior Permanent Magnet Synchronous Motor(IPMSM) have many advantages such as high power density, wide speed range and so on. With the IPMSM, miniaturization and energy efficient design can be achieved in comparison with Surface Permanent Magnet Synchronous Motor(SPMSM). In order to secure miniaturization and manufacturing efficiency of the motor, it has concentrated winding, because concentrated winding can reduce the motor volume and make manufacturing to be simple compared with the distributed winding. However, according to the pole-slot combinations motor parameters can be changed and unexpected normal force can be generated. Especially, unbalanced normal force in airgap can cause serious vibration and acoustic problem. Accordingly, in this paper, normal force and parameters variation of concentrated winding IPMSM are investigated according to the pole-slot combinations.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2013년도 추계학술대회 논문집
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• pp.686-686
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• 2013

차량용 터보차져는 디젤엔진뿐만이 아니라 가솔린 엔진에서도 장착이 보편화 되었다. 터보차져는 엔진의 효율과 출력을 효과적으로 증가시키는데 매우 훌륭한 장치이기는 하나, 여러 가지의 소음 문제를 유발시키기도 한다. 이들 소음은 회전축의 거동에 의하여 유발되는 구조 전달 소음과 공기 유동에 의하여 유도되는 공력 소음으로 구분된다. 이와 더불어 웨이스트게이트 밸브를 전자적으로 제어하는 액츄에이터계 거동으로부터 발생되는 기계적 소음이 있는데, 이것이 밸브 떨림음이다. 이 소음은 밸브가 열려 있을 때에만 발생하는데, 이는 연결 구조물 사이의 간극이 외력에 의하여 강제 접촉을 유지하지 않고 밸브부터 액츄에이터 사이에 연결되어 있는 각 연결 구조물이 서로 자유단으로 접촉하고 있기 때문이다. 각 자유단 접촉점에서는 배기가스 맥동파에 의하여 충격 진동이 발생하고 이것이 터빈하우징으로 전달되어 밸브 떨림음이 발생하는 것이다. 그러나, 액츄에이터의 기계적 구동력에 의하여 액츄에이터의 모든 연결 구조물이 강제접촉을 유지하고 있는 기계식 액츄에이터에서는 발생하지 않는다. 본 논문에서는 불평형 회전축을 갖는 소형 진동 모터를 이용하여 전자식 액츄에이터에서 발생하는 밸브 떨림음 평가를 위한 장치를 고안하였으며, 이 장치를 이용하여 밸브 떨림음의 저감효과를 평가하였다. 소음 저감 방법으로는 구조물간 접촉 간극 축소 또는 웨이브 와셔 삽입, 밸브레버와 터빈하우징 사이에 조립되는 부싱의 헐거움 끼움이 효과적임을 확인하였다.

• Tribology and Lubricants
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• 제36권2호
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• pp.105-115
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• 2020

This paper presents a numerical study on the rotordynamic analysis of a dual-spool turbofan engine in the context of blade defect events. The blades of an axial-type aeroengine are typically well aligned during the compressor and turbine stages. However, they are sometimes exposed to damage, partially or entirely, for several operational reasons, such as cracks due to foreign objects, burns from the combustion gas, and corrosion due to oxygen in the air. Herein, we designed a dual-spool rotor using the commercial 3D modeling software CATIA to simulate blade defects in the turbofan engine. We utilized the rotordynamic parameters to create two finite element Euler-Bernoulli beam models connected by means of an inter-rotor bearing. We then applied the unbalanced forces induced by the mass eccentricities of the blades to the following selected scenarios: 1) fully balanced, 2) crack in the low-pressure compressor (LPC) and high pressure compressor (HPC), 3) burn on the high-pressure turbine (HPT) and low pressure compressor, 4) corrosion of the LPC, and 5) corrosion of the HPC. Additionally, we obtained the transient and steady-state responses of the overall rotor nodes using the Runge-Kutta numerical integration method, and employed model reduction techniques such as component mode synthesis to enhance the computational efficiency of the process. The simulation results indicate that the high-vibration status of the rotor commences beyond 10,000 rpm, which is identified as the first critical speed of the lower speed rotor. Moreover, we monitored the unbalanced stages near the inter-rotor bearing, which prominently influences the overall rotordynamic status, and the corrosion of the HPC to prevent further instability. The high-speed range operation (>13,000 rpm) coupled with HPC/HPT blade defects possibly presents a rotor-case contact problem that can lead to catastrophic failure.

• 한국자동차공학회논문집
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• 제23권3호
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• pp.292-298
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• 2015

A wiper is a safety device removing rain and debris from windshield and ensuring visibility of drivers. If contact pressure distribution between rubber of the blade and the windshield is unbalanced, unwanted noise, vibration, and abrasion of the blade can occur and sometimes fatal accidents could occur. To improve the safety of the wiper, there have been many researches on the contact pressure analysis of the wiper, but the analysis results were not converged or require much computational time due to material nonlinearity of the rubber and contact conditions between the blade rubber and the windshield. In this research, a simple model with 1D beam and 2D shell elements was used for the contact pressure analysis instead of the 3D blade model. The simplified model saved computational time of the analysis and resolved convergence problems. The accuracy of the analysis results was verified by comparing them with experimental results for different rail spring curvatures.