• 한국정밀공학회지
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• 제34권4호
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• pp.287-292
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• 2017

A gas turbine is the main equipment used in a combined heat and power plant. It generates a high sound pressure noise level. To reduce the noise level, an enclosure is installed around the turbine. The sound insulation performance of the enclosure affects the amount of external noise reduction. In this study, a sound transmission loss analysis is performed using the boundary element method to predict sound insulation performance according to the numbers and shapes of the supporter. Radiated noise analysis is also performed for the main external points of the enclosure using ray-acoustics. The results of these analyses are presented and a design plan is proposed that reduces the sound pressure noise level of the enclosure.

• 한국전자파학회논문지
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• 제27권12호
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• pp.1097-1104
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• 2016

적외선 카메라는 Mil-Std-461 항목 중 복사성 방사 잡음 시험, RE-102의 규격 만족에 어려움을 겪는다. 특히 무인항공기용 전자장비의 경우 차폐 케이블을 사용하지 않아 전자기적합성 규격 만족이 어려워 적절한 대응 설계가 필요하다. 무인정찰기용 적외선 카메라의 RE-102 시험 중 50~200 MHz 대역에서 30 dBuV/m 이상 규격을 초과하는 방사 잡음을 확인하였다. Pcb em scan 결과, 디지털 제어 신호 클록의 체배 주파수에 의한 첨두 잡음 발생을 확인하였고, 카메라의 제어 클록에 3 % 다운 스프레딩 방식의 확산 스펙트럼 클록 생성기를 적용하여 방사 잡음이 최대 22.9 dBuV/m 감소함을 확인하였다.

• 한국소음진동공학회논문집
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• 제19권5호
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• pp.462-467
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• 2009

Reduction of the structure-borne noise of the naval vessel is very important in order to reduce the underwater radiated noise of it. One of the important factors to reduce the structure-borne noise of the installed machine in a ship is the design of the foundation having sufficiently high mechanical impedance. In this paper, the mechanical impedance of the foundation for the fan-coil unit in a naval vessel is evaluated numerically according to variation of the thickness of the foundation. And also, the forced vibration analysis is conducted considering the dynamic property of the anti-vibration mount. Through the analysis results, it can be known that the dynamic property of the anti-vibration mount should be considered when the minimum level of the mechanical impedance of the foundation is set.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2002년도 추계학술대회논문초록집
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• pp.332.1-332
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• 2002

The study was performed as reduction method using finite and boundary element analysis on structure-borne noise radiated by dash panel of a real car. The radiation efficiency is used to estimate sound noise of dash panel. Curvature and edges of dash panel have effect on radiation efficiency. The simulation results of dash panel was ensured by comparison between experimental results and simulation results of a simple rectangular plate. (omitted)

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.1716-1720
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• 2000

To develop the code of predicting flow-field and aeroacoustic noise by a electrical cable, a combined CFD-acoustic analogy approach is selected. The two-dimensional, unsteady, incompressible Reynolds-Averaged Navier-Stokes solver with a ${\kappa}{\omega}$, ${\kappa}{\omega}$ SST turbulence modeling is used to calculate the near-field around electrical cable. Near-field results are then coupled with two-dimensional Curle's integral formulation based upon Lighthill's acoustic analogy with an assumption of acoustic compactness. To validate this code, numerical results are compared with experimental data for a circular cylinder. The simulation shows an overprediction on acoustic amplitudes, but overally speaking, the spectrum pattern of sound pressure agrees well with experiment in an acceptable amount of error. In addition, various cross sections of a cable were selected and compared with each other in terms of drag and radiated noise.

• 소음진동
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• 제6권5호
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• pp.661-669
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• 1996

Proposed is an aero-acoustic performance prediction method of axial fan. The fan aerodynamic performance is predicted by combining pitch-averaged quasi 3-D flow analysis with pressure loss models for blade boundary layer and wake, secondary flow, endwall boundary layer and tip leakage flows. Fan noise is assumed to be radiated as dipole distribution type, and its generation is assumed to be mainly due to the vortex street shed from blade trailing edge. The fluctuating pressure and lift on the blade surface are analyzed by incorporating the wake vortex stree shed from blade trailing edge. The fluctuating pressure and lift on the blade surface are analyzed by incorporating the wake vortex street model with thin airfoil theory. The aero-acoustic performance prediction results by the present method are in good agreement with the measured results of several axial fans. With the present prediction method, parametric studies are carried out to investigate the effects of blade chord length and spacing on the efficiency and the noise level of fan. In the case of lightly loaded fan, both efficiency improvement and noise reduction can be achieved by decreasing chord length or by increasing blade specing. However, when fan is designed at highly loaded condition, the noise reduction by increasing blade spacing penalizes the attaninable efficiency of fan.

• 대한기계학회논문집A
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• 제20권5호
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• pp.1573-1581
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• 1996

This paper present as experimental demonstratio of DSP and a sensory actuator that is used to actively control sound transmission/radiation through a vibrating plate. A plane acoustic wave incident on a clamped, thin circular plate was used as a noise source, and a sensory actuator bounded to the plate was used to control and sense vibration of the plate. The sound transmission reduction problem was tranformed as a structural vibration control problem that actively control the structural vibration modes coupled to acoustic modes. The results show that the first structural vibration mode is controlled with a reduction of 78 percent in the displacement and velocity of the plate. This corresponds to a 13dB reduction in the acoustic response. These experimental results indicate that a sensory actuator bounded to the plate can be employed to attenuate the sound transmitted to radiated from the plate.

• 소음진동
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• 제8권6호
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• pp.1030-1036
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• 1998

When the lateral dimensions of a duct is larger than or comparable to the wavelengths of Interest, higher order modes propagate in the duct. These modes will be radiated and produce noise. A number of sensors and actuators for control of radiating noise from the duct have to be incorporated with the number of modes which one wants to control. These considerations motivated the present study that considers a control system which has less microphones and control sources than required. In this work, by theoretical analysis, the control performance of such a kind of system is investigated in terms of sound-field variables and control system variables. The possible maximum and minimum value. mean and variance of residual acoustic potential energy are derived for the set of primary sound fields.

• 한국소음진동공학회논문집
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• 제14권7호
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• pp.577-585
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• 2004

In this paper, reactive shearing structural intensity method is extended to damping patches placement on outer panels of outdoor unit of air-conditioner to reduce its structural borne noise. The structural intensity is calculated from the normal velocities of structures that are measured by using a laser scanning vibrometer, and $textsc{k}$-space (wave-number domain) signal processing is used to obtain the spatial derivatives in formulation of structural intensity. This method is applied to the outdoor unit of air-conditioner on shaker-exciting mode and operating mode. and then damping patches are placed over area of high reactive shearing structural intensity for reducing the radiated noise. Experimental results show the largest reduction of sound pressure level of an outdoor unit by appling small damping patches to optimal position.

• 한국음향학회지
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• 제39권6호
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• pp.524-532
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• 2020

본 논문에서는 무선진공청소기용 팬 모터 단품으로부터 방사되는 공력소음을 저감하기 위하여 팬 모터 단품 내부의 기존 임펠라에 스플리터 날개를 설계하였다. 우선, 팬 모터 단품, 특히 임펠라의 유동장을 분석하기 위하여 전산유체역학 기법을 사용하여 비정상, 비압축성 Reynolds-Averaged Navier-Stokes(RANS) 방정식을 수치적으로 해석하였다. 예측한 유동장 결과를 입력값으로 Ffowcs Williams-Hawkings(FW-H) 적분 방정식을 풀어 임펠라로부터 방사되는 소음을 수치적으로 예측하였다. 예측한 음압스펙트럼과 측정값의 비교를 통하여 수치해석방법의 유효성을 검증하였다. 예측한 유동장 결과에 대한 추가 분석을 통하여 임펠라 날개 사이에서 강한 와류가 형성되는 것을 확인하였다. 와류는 유동에는 손실로 소음에는 소음원으로 작용하기 때문에 기존 임펠라에 스플리터 형상을 추가 설계하여 와류를 억제하고자 하였다. 스플리터의 길이와 위치를 설계 인자로 선정하였으며, 다구찌 기법을 사용하여 각각의 설계 인자가 공력소음에 미치는 영향도를 살펴보았다. 이 결과로부터 최소소음을 나타내는 스플리터의 최적 위치와 길이를 결정하였다. 최종 선정된 설계안에 대한 추가 해석을 통하여 소음성능이 개선됨을 확인 하였다.