• Title/Summary/Keyword: 기내소음

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Measurement of Acoustic transfer function by one microphone (한개의 마이크로폰에 의한 음향 전달함수 측정)

  • 정갑철;임정빈;권영필
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1994.04a
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    • pp.201-205
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    • 1994
  • 본 실험에서는 한개의 마이크로폰만을 이용하여 소음기내에 삽입된 재료의 흡음율을 임피던스관에서 전달함수기법으로 측정하고 측정값의 정확성을 확인하기 위하여 정재파법으로 측정한 결과와 비교하여 보았다. 또한 이 측정법을 단순팽창형 소음기에 적용하여 소음기의 투과손실을 측정한 후, 이론과 비교하여 측정의 정확성을 검토하였고 소음기내에서의 흡음재의 위치에 따른 투과손실의 변화에 대해서도 이론과 비교 검토하였다.

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

  • Elliott Stephan J.;Jeong, W.B.;Hong, Chin-Suk
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2006.11a
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    • pp.464-473
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    • 2006
  • This paper summarises theoretical and experimental work on the feedback control of sound radiation from honeycomb panels using piezoceramic actuators. It is motivated by the problem of sound transmission in aircraft, specifically the active control of trim panels. 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. Local coupling of the closely-spaced sensor and actuator was observed experimentally and modelled using a single degree of freedom system. The effect of the local coupling was to roll-off the response between the actuator and sensor at high frequencies, so that a feedback control system can have high gain margins. Unfortunately, only relatively poor global performance is then achieved because of localisation of reduction around the actuator. This localisation prompts the investigation of a multichannel active control system. Globalised reduction was predicted using a model of 12 channel direct velocity feedback control. The multichannel system, however, does not appear to yield a significant improvement in the performance because of decreased gain margin.

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

  • Hong, Chin-Suk
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.16 no.12 s.117
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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.

실험적 방법과 이론적 방법의 비교를 통한 진공청소기용 Fan Motor의 진동소음 해석

  • 김재열;곽이구;양동조;김우진
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2004.05a
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    • pp.187-187
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    • 2004
  • 진공청소기는 가전 제품 중에서 인간의 일상생활에서 꼭 필요한 가전제품의 하나이다. 그러나, 성능 향상을 위한 과도한 회전 속도 때문에 큰 소음을 유발하며 그로 인해서 사용자에게 소음으로 인한 스트레스나 피로누적 등의 큰 불편을 초래하고 있다. 이것은 진공청소기내에 있는 팬 모터가 30000∼35000 rpm으로 고속회전을 통해서 측에 연결되어 있는 임펠러를 회전시켜 공기를 흡입, 배출시키는 일련의 작동을 하면서 여러 가지 진동 및 유체소음을 일으키기 때문이다. 이러한 진공청소기용 팬모터의 소음 저감 연구는 국내외 관련회사 및 연구소에서 활발히 진행되고 있다.(중략)

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The Noise Reduction of Industrial Blower Using Buff Shapes in Silencer (소음기내의 버프 형상을 이용한 산업용 송풍기의 소음저감)

  • Kim, Chang-Ho;Son, In-Soo;Ahn, Tae-Soo;No, Tae-Woo
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.9 no.1
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    • pp.19-24
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    • 2010
  • The noise of an running industrial fan or blower depends on the type of a fan, the machining accuracy and assembled conditions of each element, and buffs. Many studies have been carried out to reduce the noise through silencer in blower. In this study, 3 types of buffs which have different hole are employed in pipe of blower to study the influence the number and arrangement of buffs on the noise reduction at inlet and outlet in pipe. Commercial engineering software ANSYS was employed to analyze the characteristics and reduction ratio of pressure. Experimental results shows that optimal one can reduce the reduction ratio of noise as much as 16 percents in the laboratory. Good agreement was found between the analysed ratio of noise reduction and those obtained from the experiments.

Study of the Weak Shock Wave Propagating through an Exhaust Pipe Silencer System (배기 소음기내를 전파하는 비정상 충격파의 수치해석)

  • Kweon, Y.H.;Kim, H.D.
    • Proceedings of the KSME Conference
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    • 2001.11b
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    • pp.462-467
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    • 2001
  • The present study addresses a computational work of the weak shock wave propagatings inside a silencer system of automobile exhaust pipe. Four different types of the silencer systems and the initial shock wave Mach number $M_s$ of $1.01\sim1.30$ are applied to investigate their effects on the noise reduction and the flow field in a silencer system. The results obtained from the present computational work are compared with the experimental results. The second order total variation diminishing (TVD) scheme is employed to solve the two dimensional, compressible, unsteady, Euler equations. The present computational results predict the experimental results with a quite good accuracy. Of the four silencer systems applied, the most desirable silencer system to reduce the peak pressure at the exit of the exhaust pipe is discussed.

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Study of the Weak Shock Wave Propagating inside an Engine Exhaust Muffler (엔진 배기 소음기내를 전파하는 약한 충격파에 관한 연구)

  • 이동훈;권용훈;김희동
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.12 no.7
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    • pp.510-519
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    • 2002
  • The present study addresses a computational work of the weak shock wave propagating inside an automobile exhaust muffler. Several different types of the silencer systems are employed to investigate the magnitude of the shock wave during propagating through them. The Initial shock wave Mach number $M_s$ is varied between 1.01 and 1.30, and a normal shock wave is given at the inlet of the silencer systems. The second order total variation diminishing scheme Is employed to solve the two dimensional, compressible, unsteady Euler equations. The present computational results are compared with the previous experimental ones available. The present computations predict the experimental results with a quite good accuracy. Of the four silencer systems applied. the most desirable silencer system to reduce the peak pressure at the exalt of the exhaust pipe is discussed from the Point of view of the engineering design of the silencer systems.

A Study on the Flow Characteristics and Pressure Loss of a Muffler for the Variation of Volumetric Rate and Offset (체적비와 오프셋 변화에 의한 소음기내의 유동특성과 압력손실에 관한 연구)

  • 김민호;정우인;천인범
    • Transactions of the Korean Society of Automotive Engineers
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    • v.8 no.4
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    • pp.93-99
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    • 2000
  • It is well known that an automotive muffle strongly influences engine efficiency and noise reduction. The performance of a muffler system is determined by the geometrical parameters such as the relative location of an inlet and outlet pipe size and cross sectional geometry of a chamber. In this study numerical analysis was performed to examine the flow characteristics in the simple automotive muffler for the variation of volumetric rate and offset. The computational grid generation was carried out. The RNG k-$\varepsilon$ turbulence model was applied. To provide the boundary condition for numerical analysis the experimental measurement wes carried out. As a result of this study we could understand that there was a recirculation flow inside muffler and pressure loss depends on the variation of volumetric rate and offset.

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Effects of APU Noise on Employees on the Ramp (APU 소음이 램프 근로자들에게 미치는 영향)

  • Park, Sung-Jae
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.17 no.7
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    • pp.720-725
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    • 2016
  • This study examined how the APU noise of an aircraft influences the work efficiency and stress of airport ramp workers. A survey of airport ramp workers was conducted and the results analyzed. In the demographic analysis, men outnumbered women - accounting for 86% of the survey target - and 80% of the respondents were found to be employees with less than 15 years of work experience. The occupational cluster of the total of 160 respondents included 41 aircraft maintenance workers, 70 ground staff (Cargo, Water and Waste services), 19 ramp coordinators, 18 ramp controllers and 12 catering Service workers. The ground staff were the most prevalent, constituting 44% of the occupational cluster. Regarding the APU noise, 74% of the respondents answered that the environment was "always noisy", while 26% answered that it was "sometimes noisy". 85% answered that they are sensitive to and put under stress by the APU noise, while the majority of the respondents answered that the APU noise degrades their work efficiency. In conclusion, this study examined the effect of APU noise on the work efficiency and stress of airport ramp workers by analyzing the survey data by Regression and Chi-square analysis.

A study on Cogging Torque attenuation structure of traction motor (트랙션용 전동기의 코깅토크 감쇄 구조에 관한 연구)

  • Ko, Hyung-Keun;Kim, Byung-Kook;Lee, Sang-Kyu;Cho, Jae-Hee;Park, Tae-Hong
    • Proceedings of the KSR Conference
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    • 2011.10a
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    • pp.2365-2372
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    • 2011
  • The Cogging Torgue is non-uniform torgue in motor which causes noise and vibration to synchronous motors such as BLDC motor, and regardless of load current, is generated by the interaction between permanent magnet rotor and stator slot which is the force of tangential direction that tends to move into the position where the magnetic energy of motor system is minimal. such Cogging Torgue shall be considered in design stage since it is the main factor of motor's noise and vibration. Understanding that Cogging Torgue is generated by the interaction between relatively low stage harmonic flux density gab of permanent magnet rotor and steel slot of stator. This study proposes the method if reducing Cogging Torgue using response surface method which is a kind of design if experiment.

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