• 제목/요약/키워드: vibration and noise control

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21세기 소음정책 선진화 방안 고찰 (A Study on the Plan for Advanced Noise-Policy in the 21st Century)

  • 양근호;박영민;이내현;장윤영
    • 환경영향평가
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    • 제18권1호
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    • pp.21-30
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    • 2009
  • The study show that things about the noise control are indicated at The Noise & Vibration Control Act and the other Act. Also, the details program and total government ministries' program for the noise control are indicated what are the advance noise control plan. The study consist of the four part which are "Draw up the environmental noise infrastructure plan; the install shall be done the noisemap & the automatic noise measurement devices", "Resetting of environmental noise standard at the application area and Introduce of indoor noise; the guide for region classification of the noise standard & indoor noise", "Setting of aircraft noise standard and Program of measurement point operation; the noise-assessment-standard shall change from WECPN to new index($L_{den}$, $L_{dn}$, $L_{Aeq\;24h}$) & the operation and control of aircraft noise measurement changes from local environmental office to central control center" and "The method of noise regulation at construction site and the plan on making of standard for vibration regulation; It shall be made that the guideline of construction noise should include a target-construction, noise standard etc & the ministries shall unify control about construction vibration of the blasting vibration". The advance noise-policy will improve efficiency to deal with civil appeal & damage on residents about noise.

항공기용 하니콤 트림판넬의 다채널 능동제어 (Multichannel Active Control of Honeycomb Trim Panels for Aircrafts)

  • 홍진숙
    • 한국소음진동공학회논문집
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    • 제16권12호
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    • pp.1252-1261
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    • 2006
  • This paper summarizes theoretical work on the multichannel decentralized feedback control of sound radiation from aircraft trim panels using piezoceramic actuators. The aircraft trim panels are generally honeycomb structures designed to meet the design requirement of low weight and high stiffness. They are resiliently-mounted to the fuselage for the passive reduction of noise transmission. It is motivated by the localization of reduction in vibration of single channel active trim panels. 12-channel decentralized feedback control systems are investigated in terms of the reduction of noise and vibration for three configurations of sensor actuator pairs. Local coupling of the closely-spaced sensor and actuator pairs was modeled using single degree of freedom systems. The multichannel control system is characterized using the state-space model. For the stability point of view, the relative stability or robustness is evaluated by comparing the real part of eigenvalues of the system matrix for the three configurations. The control performance is also evaluated and compared for the three configurations. It is found that the multichannel system can lead to the globalization of the reduction in vibration and radiated noise. It does not appear to yield a significant improvement in the vibration because of decreased gain margin. However, the reduction in the radiated noise is remarkably improved due to the variation of the vibration pattern with the actuation configurations.

대형 구조물 바닥판의 동적 거동 및 제어 (Vibration Control and System Identification of Long Span Slab)

  • 황재승;김장윤
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2003년도 추계학술대회논문집
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    • pp.56-59
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    • 2003
  • As the slab is longer and lighter, it is more sensitive to the external force so that the vibration of slab and noise induced by the slab vibration is bigger than expected in normal slab. The purpose of this study is to investigate how the dynamic characteristic of slab is different from the normal slab through the system identification and tn evaluate the vibration control performance when the damper system is installed. Finally, we was trying to understand by what mechanism the slab noise is induced from the slab vibration. The relationship between the vibration and the noise of slab is shown by the numerical simulation.

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건설장비 캐빈 저소음화를 위한 시험적 연구 (Experimental Study for Construction Equipment's Cabin Noise Control)

  • 이태경;주원호;배종국
    • 한국소음진동공학회논문집
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    • 제19권8호
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    • pp.802-808
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    • 2009
  • In this paper, the experimental study on the identification of noise sources and noise transmission paths was carried out for the cabin noise control of construction equipment. In order to investigate noise and vibration characteristics of cabin structure, sound absorption, transmission, and radiation tests were performed using cabin assembly models. The noise/vibration source levels were obtained from the real cabins of wheel loader and excavator. Using transfer functions of cabins and real cabins' source data, cabin noise was decomposed into airborne and structureborne noise transmissions. Finally noise sources and major transmission paths were successfully identified for wheel loader and excavator's cabins.

건설장비 캐빈 저소음화를 위한 시험적 연구 (Experimental Study for Construction Equipment's Cabin Noise Control)

  • 이태경;주원호;배종국
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2009년도 춘계학술대회 논문집
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    • pp.84-89
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    • 2009
  • In this paper, the experimental study on the identification of noise sources and noise transmission paths was carried out for the cabin noise control of construction equipment. In order to investigate noise and vibration characteristics of cabin structure, sound absorption, transmission, and radiation tests were performed using cabin assembly models. The noise/vibration source levels were obtained from the real cabins of wheel loader and excavator. Using transfer functions of cabins and real cabins' source data, cabin noise was decomposed into airborne and structureborne noise transmissions. Finally noise sources and major transmission paths were successfully identified for wheel loader and excavator's cabins.

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유연구조물이 있는 다점지지 시스템의 능동진동제어 (Active vibration control of multi-point mounting systems with flexible structures)

  • 오시환;박영진
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2000년도 춘계학술대회논문집
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    • pp.274-279
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    • 2000
  • Driving of the engine makes unbalance forces which induces vibration to the engine mount system. Active vibration control must be performed to reduce the vibration and the propagation of structure-born sound. In this study, the engine system is modeled as 3-dim. vibration system including flexible structures and an effective active noise control method is proposed. Also, appropriate actuator and sensor locations and types are selected. The miniature of the engine vibration system with multi-input multi-output is built and an active vibration control with multiple filtered-X LMS algorithm is applied to it. The applied control method was effective to reduce the transmitted vibration power through the rubber mount It showed the feasibility of the control of the engine vibration systems with flexible structures.

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질량형 댐퍼를 이용한 바닥판의 진동 및 소음 저감 (Vibration and Noise Control of Slab Using the Mass Type Damper)

  • 황재승;박성철;김홍진
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2007년도 정기 학술대회 논문집
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    • pp.597-602
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    • 2007
  • It is proposed to analyze the vibration of slab with MTMD and vibration-induced noise. Substructure synthesis is introduced to develope the interaction between the slab and MTMD which are defined in different space and acoustic power is obtained from the velocity field of slab. Numerical analysis is performed to show that the vibration and noise of slab can be reduced by MTMD. A living room of wall type apartment including the wall and MTMD is modeled and analyzed by FEM program Numerical analysis shows that the vibration and noise control effect is different depending on the location and mass ratio of MTMD. Futhermore, noise is more effectively reduced when the vibration of higher modes of slab are reduced rather than lower modes.

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헬리콥터 능동 진동/소음 제어 기법 해외 동향 및 사례 (Technology Trend of Vibration/Noise Active Control in Helicopter)

  • 김덕관;윤철용;정기훈;김승호
    • 항공우주산업기술동향
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    • 제9권1호
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    • pp.77-89
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    • 2011
  • 헬리콥터는회전하는구동시스템에의해추력및비행제어력을발생하기때문에회전체에서기체로전달되는 진동 및 소음을 줄이는 것이 아주 중요하다. 과거에는 수동적 방법으로 특정주파수에 해당하는 진동 및 소음을 줄였지만, 기술이 발달함에 따라 주파수를 변동시킬 수 있는 장치를 적용할 수 있는 능동적 진동 및 소음 제어방법이 개발되었다. 본 논문에서는 이러한 헬리콥터 진동 및 소음을 제어하는 능동적 방법에 대한 세계적인 기술동향 및 사례를 기술하였다. 서론에서는 헬리콥터 진동 및 소음을 제어하는 일반적인 방법론을 소개하고, 본론에서는 능동적으로 제어하는 사례 및 동향을 중심으로 기술하였다. 현재 가장 활발하게 진행되고 있는 능동적 플랩구동장치 및 비틀림장치 등을 중심으로 소개하였다.

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PRINCIPLES OF AN ACTIVE NOISE AND VIBRATION CONTROL SYSTEM CONSTRUCTION FOR SHIP

  • Maslov, Viatcheslav L.;Soloveitchik, Leonid I.
    • 한국음향학회:학술대회논문집
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    • 한국음향학회 1994년도 FIFTH WESTERN PACIFIC REGIONAL ACOUSTICS CONFERENCE SEOUL KOREA
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    • pp.860-863
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    • 1994
  • Main sources of increased vibrations and air noise on ship are main and auxiliary engines and ship ducts. The various ways of transfer of vibration energy and air noise in passenger cabin of a vessel require, in general case, of various methods of attenuation. The transfer of vibration energy from engines through a support requires, alongside with shock-absorbers, availability active shock-absorbers. The transfer of vibration energy and hydrodynamic noise on ship ducts requires availability, alongside with flexible muffler, active mufflers. The availability of air noise from working equipment can require, along with absorbent covers, of space systems of active noise control. In the given article it is spoken about the unified approach to formation of the block-diagram of active noise and vibration control. The complex approach permits to receive additional efficiency in reduction of noise in passenger cabin of vessels.

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