• Title/Summary/Keyword: 제어형 소음기

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Control of the Multi-Mode Muffler for Low Noise and Low Backpressure (저소음 저배압을 위한 다중모드 배기계의 소음제어)

  • Son, Dong-Gu;Kim, Heung-Seop;O, Jae-Eung
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.24 no.6 s.177
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    • pp.1371-1378
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    • 2000
  • To reduce backpressure for improving engine power in exhaust system, a large difference of pressure is required, but this is in conflict with the requirement for reducing exhaust noise that needs a small pressure difference. In this paper, the controllable muffler designed by simplifying the structure of the exhaust system has a low backpressure and a proper sound specification to the rotation of engine. The exhaust system in conventional studies has been designed to have maximum noise reduction over the whole driving domain, but due to its complex structure this led to increased backpressure. If the muffler is designed according to the driving frequency, which is a dominant noise component in stationary driving speed, the backpressure is reduced due to the simplified structure of the muffler. Furthermore, a multi-mode muffler able to change structure with varied driving speed was designed.

Modal Characteristics and Vibration Control of Cylindrical Shell Structure : Experimental Results Comparison in the Air and Water (실린더형 셸 구조물의 모드 특성 및 진동제어 : 공기중 및 수중 실험결과 비교)

  • Sohn, Jung-Woo;Kwon, Oh-Cheol;Choi, Seung-Bok
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.19 no.9
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    • pp.899-906
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    • 2009
  • In the present paper, dynamic characteristics and vibration control performance of a cylindrical shell structure are experimentally investigated and results are presented in the air and underwater conditions. End-capped cylindrical shell structure is manufactured and macro-fiber composite(MFC) actuators are attached on the inside-surface of the structure. Modal characteristics are studied in the air and under the water conditions and then equation of motion of the structure is derived from the test results. Structural vibration control performances of the proposed structure are evaluated via experiments with optimal control algorithm. Vibration control performances are presented both in the frequency and time domains.

Active Control of Harmonic Signal Based on On-line Fundamental Frequency Tracking Method (실시간 기본주파수 추종방법에 근간한 조화 신호의 능동제어)

  • 김선민;박영진
    • Journal of KSNVE
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    • v.10 no.6
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    • pp.1059-1066
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    • 2000
  • In this paper. a new indirect feedback active noise control (ANC) scheme barred on the fundamental frequency estimation is proposed for systems with a harmonic noise. When reference signals necessary for feedforward ANC configuration are difficult to obtain, the conventional ANC algorithms for multi-tonal noise do not measure the reference signals but generate them with the estimated frequencies.$^{(4)}$ However, the beating phenomena, in which certain frequency components of the noise vanish intermittently, may make the adaptive frequency estimation difficult. The confusion in the estimated frequencies due to the beating phenomena makes the generated reference signals worthless. The proposed algorithm consists of two parts. The first part is a reference generator using the fundamental frequency estimation and the second one is the conventional feedforward control. We propose the fundamental frequency estimation algorithm using decision rules. which is insensitive to the beating phenomena. In addition, the proposed fundamental frequency estimation algorithm has good tracking capability and lower variance of frequency estimation error than that of the conventional cascade ANF method.$^{(4)}$ We are also able to control all interested modes of the noise, even which cannot be estimated by the conventional frequency estimation method because of the poor S/N ratio. We verify the performance of the proposed ANC method through simulations for the measured cabin noise of a passenger ship and the measured time-varying engine booming noise of a passenger vehicle.

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Dynamic Analysis of Tip-actuators for Controlling Tip-media Gap in Cantilever Type Optical Data Storage (캔틸레버형 광 정보저장에서의 빠른 팁/매체 간극제어를 위한 팁/구동기의 동역학적 분석)

  • 이성규;송기봉;김준호;김은경;박강호;남효진;이선영;김영식
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2003.05a
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    • pp.1004-1008
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    • 2003
  • Near-filed optical storage using cantilever aperture tip is a promising way fer next generation optical data storage. To enhance the speed of reading and writing data, gap between tip and media should be controlled fast and precisely within near field region. In this paper, several PZT actuators are analyzed far constructing dual servo control algorithm: coarse actuators(stact. PZT, bimorph PZI) for media surface inclination and One actuator(film PZT) for media surface roughness. Dynamic analysis of stack PZT, bimorph PZT, and film PZT are performed through the frequency response. Based on the frequency response and mathematical model, fast analog controller is designed.

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Study on Hybrid type Optical Pickup Actuator for Tilt Control (틸트제어를 위한 하이브리드형 광픽업 구동기에 대한 연구)

  • Kim, Chul-Jin;Lee, Kyung-Taek;Shin, Chang-Hun;Park, No-Cheol;Park, Young-Pil
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2002.11b
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    • pp.782-787
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    • 2002
  • In optical disk drives (ODD), the demands of high data density and high speed have been increasing rapidly to achieve high data capacity and data transfer rate. The short wavelength laser, High NA objective lens, and high track following performance are needed to raise data density and data rate. For high-performance actuator, the improvement of linearity and acceleration become more important. Also, 3-axis actuator for active tilt compensation is introduced to overcome the decrease in disk tilt tolerance which is induced by short wavelength laser. In this paper, a hybrid type 3-axis actuator is presented and a new yoke structure, which can reduce the interaction between yoke and moving magnet, is designed to keep the efficiency of magnetic circuit. Experimental results show the validity of the yoke in the hybrid type actuator.

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A Study on the Development of a Hybrid Electromagnetic Actuator Against Microvibration (미진동 저감을 위한 복합형 전자기식 작동기의 개발에 대한 연구)

  • Moon, S.J.;Park, S.H.;Jeong, J.A.;Huh, Y.C.;Kim, C.H.;Choi, S.M.
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.21 no.5
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    • pp.475-483
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    • 2011
  • A hybrid electromagnetic actuator with an air mount is designed so as to achieve the desired isolation reduce the vibration efficiency on the floor vibration. The performance specification of the hybrid electromagnetic actuator is determined based on the vibration criterion for vibration-sensitive equipment. In the design stage of the electromagnetic actuator, the simple reluctance method is adapted to analyze magnetic circuits. The result is verified by finite element analysis using ANSYS Emag. Finally, in order to confirm the design performance, a dynamic characteristic test is carried out for the prototype of a hybrid electromagnetic actuator.

Slim Tilt Actuator for High density Recording in Optical Disc (기록용 고밀도 광디스크를 위한 박형 틸트 구동기)

  • 정호섭;이호철;윤용한
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2002.11a
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    • pp.378.1-378
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    • 2002
  • DVD, HD(High Density)-DVD등의 고밀도 광 디스크의 광 기록재생장치는 고 개구율(Numerical Aperature)의 대물렌즈로 집광 빔의 크기를 소형화하여 기록용량을 증대시키고 있다. 이 경우 광축과 광 디스크의 기록면에 대한 경사는 광학적인 수차가 발생되어 신호 레벨의 저하나 기록시의 피트(pit) 형성의 오류, Crosstalk등의 문제가 발생한다. 이를 극복하기 위해 직접 디스크의 경사에 따라 제어할 수 있는 픽업 구동기가 제안되어 왔지만 주로 Half Height(12.7mm)에 사용되는 틸트 구동기였으며 Slim(6.3mm)형 틸트 구동기는 제안되지 못하였다. (중략)

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Development of an Intelligent Active Trailing-edge Flap Rotor to Reduce Vibratory Loads in Helicopter (헬리콥터의 진동하중 저감을 위한 지능형 능동 뒷전 플랩 로터 제어 시스템 개발)

  • Lee, Jae-Hwan;Choe, Jae-Hyeok;Shin, Sang-Joon
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2011.04a
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    • pp.492-497
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    • 2011
  • Helicopter uses a rotor system to generate lift, thrust and forces, and its aerodynamic environment is generally complex. Unsteady aerodynamic environment arises such as blade vortex interaction. This unsteady aerodynamic environment induces vibratory aerodynamic loads and high aeroacoustic noise. Those are at N times the rotor blade revolutions (N/rev). But conventional rotor control system composed of pitch links and swash plate is not capable of adjusting such vibratory loads because its control is restricted to 1/rev. Many active control methodologies have been examined to alleviate the problem. The blade using active control device manipulates the blade pitch angle at arbitrary frequencies. In this paper, Active Trailing-edge Flap blade, which is one of the active control methods, is designed to modify the unsteady aerodynamic loads. Active Trailing-edge Flap blade uses a trailing edge flap manipulated by an actuator to change camber of the airfoil. Piezoelectric actuators are installed inside the blade to manipulate the trailing edge flap.

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Comparison of Harmonic Compensation Based on Wound/Squirrel-Cage Rotor Type (권선형 유도기와 농형 유도기를 이용한 고조파 보상 시스템의 비교)

  • Kim, Yoon-Ho;Lee, Kyoung-Hun;Cho, Young-Hyun;Hong, Young-Keun
    • Proceedings of the KIEE Conference
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    • 2000.07b
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    • pp.1264-1266
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    • 2000
  • 본 논문에서 비교하는 두 시스템은 모두 전력계통에서 발생할 수 있는 고조파 전류를 효과적으로 보상할 수 있는 시스템이다. 전력계통에서 고조파전류는 계통전압에 장해를 주기 때문에, 프릿카나 각종 전력용기기의 발열 진동, 소음 혹은 유도잡음 장해등의 원인이 된다. 따라서, 이에 대한 대책이 중요한 문제가 되고 있다. 본 논문은 이러한 고조파보상 시스템의 새로운 형태로써, 플라이휠에 의해서 만들어지는 에너지 저장시스템에, 전압형 PWM 인버터를 병용하여 순시제어가 가능한 시스템을 설계하는 것이다. 그리고 여기에 사용되는 회전기로 각각 권선형과 농형을 사용하여 시스템을 구성하고 그 특징과 장/단점을 비교 분석하였다.

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Simulation of Active Noise Control on Harmonic Sound (복수조화음에 대한 능동소음제어 시뮬레이션)

  • Kwon, O-Cheol;Lee, Gyeong-Tae;Lee, Hae-Jin;Yang, In-Hyung;Oh, Jae-Eung
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2007.11a
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    • pp.737-742
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    • 2007
  • The method of the reducing duct noise can be classified by passive and active control techniques. However, passive control has a limited effect of noise reduction at low frequencies (below 500Hz) and is limited by the space. On the other hand, active control can overcome these passive control limitations. The active control technique mostly uses the Least-Mean-Square (LMS) algorithm, because the LMS algorithm can easily obtain the complex transfer function in real-time particularly when the Filtered-X LMS (FXLMS) algorithm is applied to an active noise control (ANC) system. However, the convergence performance of the LMS algorithm decreases slightly so it may delay the convergence time when the FXLMS algorithm is applied to the active control of duct noise. Thus the Co-FXLMS algorithm was developed to improve the control performance in order to solve this problem. The Co-FXLMS algorithm is realized by using an estimate of the cross correlation between the adaptation error and the filtered input signal to control the step size. In this paper, the performance of the Co-FXLMS algorithm is presented in comparison with the FXLMS algorithm. Simulation results show that active noise control using Co-FXLMS is effective in reducing duct noise.

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