• Title/Summary/Keyword: Rotor Vibration Analysis

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FEA-based Torque Ripple and Noise Reduction of DC Motor for Automotive Air-Conditioning (유한요소 해석 기반 자동차 공조용 DC모터 토크 리플과 소음 저감에 관한 연구)

  • Hwang, Myeonghwan;Kim, Donghyeon;Yang, Seungjin;Cha, Hyunrok;Han, Jongho
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.66 no.12
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    • pp.1895-1898
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    • 2017
  • This paper discusses methods for the torque ripple and noise reduction of DC motors for automotive air-conditioning based on electromagnetic field analysis. The target of the motor is a blower motor, and to reduce cogging torque and the torque ripple, the optimum model was selected by deforming the brush or commutator shape. In addition, to reduce the cogging torque, the model design was carried out by applying the skew method and the magnetization method of a magnet to the rotor. For optimization, the shape, material, and drive system of the motor were selected using an electromagnetic field as the analysis tool, and the method of reducing the cogging torque was applied to 4-pole, 12- and 13-slot motors considering the mechanical part. Lastly, this paper confirmed thatthemethod, which proposed how much noise, cogging torque, and vibration are reduced, improves through practical analysis.

Design and Application of Database System for Dynamic Balancing Test of Helicopter Main Rotor Blade (헬리콥터 주로터 블레이드의 동적밸런싱 시험에 대한 데이터베이스 설계 및 적용)

  • Yoon, Byung-Il;Paek, Seung-Kil;Song, Keun-Woong;Kim, Deog-Kwan
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.8
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    • pp.582-589
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    • 2019
  • The dynamic balancing test of helicopter main rotor blades is a blade rotation test conducted on the ground to make the track of each blade and the load on each pitch rod to a similar level before the flight tests. The purpose of the test is to reduce the vibration occurring on main rotor system as a result of dissimilarity of each blade. The RTB test has been performed for a long period at Whirl Tower Test Facility located in Goheung Flight Centre, accumulating its data. As the amount of the results has become increasingly enormous the needs for the development of database system has been raised to manage the data with effective method. This research aimed to describe the development of Dynamic-Balancing Database System for the RTB test results. For the design of the database system the informations of RTB test results have been categorized into properties, connecting each others according to its logical meaning, and comprised into a database system with relational elements. It has been shown in this paper that the Dynamic Balancing database system enables to effectively accumulate the RTB test data and to be utilized for the data analysis.

Investigation of Unbalanced Mass of a Work Roll in a Cold Rolling Mill (냉간 압연기에서 작업롤의 질량 불평형에 관한 연구)

  • Kim, Young-Deuk;Kim, Chang-Wan;Park, Hyun-Chul
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.36 no.4
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    • pp.429-435
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    • 2012
  • An abrasion due to continuous friction between a work roll and strip causes the mass of the work roll to be unbalanced in the rolling process. We developed a mathematical model for the rolling mill considering the unbalanced mass and verified the model experimentally. The work roll was approximated as a rigid rotor with eccentricity, and the effect of the unbalanced mass on chatter vibration was investigated. The joint forces computed by quasistatic analysis were applied to the work roll in the rolling mill. Transient responses were obtained, and frequency analysis was performed by solving equations of motion using a direct integration method. Horizontal vibrations were more strongly affected by eccentricity than vertical vibrations. In the horizontal direction, a small eccentricity of 1% of the work roll radius considerably increased the amplitude of the chatter frequency.

Impact Behavior Analysis on Composite Laminate with Damages (손상이 있는 복합적층판의 충격거동 해석)

  • Kim, Sung-Joon;Hong, Chang-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.1
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    • pp.22-28
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    • 2010
  • To detect the damage in composite structure, nondestructive evaluation techniques are widely used. Tapping test is perhaps the most common technique used for the detection of damage in composite laminates. The method is accomplished by tapping the inspection area with light hammer-like device. The tapping test has the ability that indicates damages in a structure due to a localized change of stiffness. The change in vibration signature may be detected by measurement of the dynamic contact force during impact. In this study, it has been shown that the characteristics of impact force histories from a structure during tapping are changed by the presence of damage such as surface crack and delamination. And impact response analysis has been performed on composite rotor blade with crack to investigate the effect of damage.

Vibrations of wind-turbines considering soil-structure interaction

  • Adhikari, S.;Bhattacharya, S.
    • Wind and Structures
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    • v.14 no.2
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    • pp.85-112
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    • 2011
  • Wind turbine structures are long slender columns with a rotor and blade assembly placed on the top. These slender structures vibrate due to dynamic environmental forces and its own dynamics. Analysis of the dynamic behavior of wind turbines is fundamental to the stability, performance, operation and safety of these systems. In this paper a simplied approach is outlined for free vibration analysis of these long, slender structures taking the soil-structure interaction into account. The analytical method is based on an Euler-Bernoulli beam-column with elastic end supports. The elastic end-supports are considered to model the flexible nature of the interaction of these systems with soil. A closed-form approximate expression has been derived for the first natural frequency of the system. This new expression is a function of geometric and elastic properties of wind turbine tower and properties of the foundation including soil. The proposed simple expression has been independently validated using an exact numerical method, laboratory based experimental measurement and field measurement of a real wind turbine structure. The results obtained in the paper shows that the proposed expression can be used for a quick assessment of the fundamental frequency of a wind turbine taking the soil-structure interaction into account.

Bearing Pad Temperature Change Depending on the Preload of Vertical Journal Guide Bearing (수직형 저널 베어링에서 preload 변화에 따른 베어링 패드 온도 변화)

  • Kim, Jun-Sung;Kim, Du-Young;Kim, Dong-Kwan;Park, Sang-Ho
    • The KSFM Journal of Fluid Machinery
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    • v.12 no.6
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    • pp.33-40
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    • 2009
  • The temperature of vertical pump bearing metal in the pumped storage power plant has been high enough to shutdown the unit. Attempts such as decreasing the oil supply temperature, increasing the bearing oil gap etc. were performed to resolve the problem, but the issue was not resolved. Finally, the high bearing metal temperature was corrected by adjusting the bearing preload. The preload is formed by the oil wedge between the journal surface and bearing pad surface and the degree of preload is determined by the machined radial clearance, assembled radial clearance, rotor journal diameter etc. This paper focuses on the analysis of the preload depending on the bearing parameters and the result of the modification of the bearing following the analysis. The bearing metal temperature dropped as much as $20^{\circ}C$ which was similar as expected by software calculation. But the shaft vibration could increase when the assembled radial clearance is excessive. So, the adjustment of the bearing preload for the tilting pad type journal bearing should be carefully performed.

Design of Experiments for Optimization of Helicopter Flight Tests (헬리콥터 비행시험 최적화를 위한 실험계획법의 적용)

  • Byun, Jai-Hyun;Lee, Gun-Myung;Kim, Se-Hee
    • Transactions of the KSME C: Technology and Education
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    • v.2 no.2
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    • pp.113-124
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    • 2014
  • In developing an aircraft, configuration determination and requirement proofing depend on flight test results. Since the flight tests require much time and high cost, systematic flight test planning and analysis are needed to reduce cost and development time. This paper presents a desirability function approach to present an integrative measure of vibration levels at important positions and suggests a fractional factorial design which is one of the experimental design methods to help perform systematic flight tests. A method to perform flight tests in stages is also suggested to further reduce the number of flight tests.

Operation Analysis of Induction Motor under the Combination of Linear & Non-linear Loads (선형 및 비선형 부하 혼합 운전시 유도전동기의 동작 분석)

  • Kim, Jong-Gyeum;Park, Young-Jeen;Lee, Dong-Ju;Kim, Jun-Ho;Lee, Jong-Han;Jeong, Jong-Ho;Lee, Eun-Woong
    • Proceedings of the KIEE Conference
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    • 2006.04b
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    • pp.65-67
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    • 2006
  • This paper presents a scheme on the characteristics of induction motor under the combination of linear & non-linear loads at the three phase 4-wire power distribution system. Under the combination operation of single & three phase load, voltage unbalance will be generated and current unbalance will be more severe by the dropped voltage quality. All power electronic converters used in different types of electronic systems can increase harmonic disturbances by injecting harmonic currents directly into the feeder grid of three phase 4-wire. Harmonic current may cause torque to decrease. Motors may also overheat or become noisy and torque oscillation in the rotor can lead to mechanical resonance and vibration.

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Optimum Geometric and Electrical Parameter for minimization Torque Ripple of Switched Reluctance Motor (스위치드 릴럭턴스 전동기의 토오크 리플 저감을 위한 기하학적인 파라미터와 전기적인 파라미터의 최적화)

  • Jung, S.I.;Choi, J.H.;Kim, Y.H.;Kim, S.;Lee, J.;Ju, M.S.;Choi, D.H.
    • Proceedings of the KIEE Conference
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    • 2001.07b
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    • pp.608-610
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    • 2001
  • In this paper, 6/4 Switched Reluctance Motor(SRM) which has simple structure and little switching element is selected basic analysis model. In order to reduce torque ripple causing noise and vibration, we execute optimization of geometric parameters (stator and rotor pole arc) and electrical parameters (turn-on angle and turn-of angle) by means of combining Fletcher-Reeves's Conjugate Directions and Finite Element Method (FEM) considering driving circuits. When considering the switching condition according to inductance profile, torque characteristics is influenced by geometric and electrical parameters importantly. The pole arc and switching angle of the optimum can also obtain the low torque ripple without high currents.

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A Study on Fuzzy Trend Monitoring Method for Fault Detection of Gas Turbine Engine (가스터빈 엔진의 손상 진단을 위한 퍼지 경향감시 방법에 관한 연구)

  • Kong, Chang-Duk;Kho, Seong-Hee;Ki, Ja-Young;Oh, Sung-Hwan;Kim, Ji-Hyun;Ko, Han-Young
    • Journal of the Korean Society of Propulsion Engineers
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    • v.12 no.6
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    • pp.1-6
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    • 2008
  • This work proposes a fuzzy trend monitoring method for the fault detection of a gas turbine engine through analyzing measured performance data trend. The proposed trend monitoring technique can diagnose the engine status by monitoring major engine measured parameters such as fuel flow rate, exhaust gas temperature, rotor rotational speed and vibration, and then analyzing their time deppendent changes. In order to perform this, firstly the measured engine performance data variation is formulated using Linear Regression, and then faults are isolated and identified using fuzzy logic.