• 제목/요약/키워드: Aerodynamic noises

검색결과 21건 처리시간 0.022초

창호일체형 환기장치의 소음분석 및 저감방안 (Noise Analysis and Reduction Methods of the All-in One Window Ventilation System)

  • 박찬재;한찬훈
    • 한국음향학회지
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    • 제32권1호
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    • pp.43-55
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    • 2013
  • 최근 창호의 창틀에 폐열회수장치를 삽입한 일체형 환기장치인 일명 "창호일체형 폐열회수 환기장치"를 개발됨으로써 창문을 열지 않고도 에너지 손실을 최소화하면서 실내외 공기를 교환할 수 있게 되었다. 그러나 이 장치의 작동시 기계소음과 공력소음이 발생하여 실제 주거시설에 적합하지 않은 면이 있다. 따라서 본 연구에서는 창호일체형 환기장치의 소음을 설치상태와 무향실에서 측정하고 소음의 발생 원인과 소음전달 취약부분을 분석하였다. 또한, 창호일체형 환기장치내의 차음재와 흡음재를 설치하여 소음을 제어하기 위한 대안을 제시하였다. 연구결과, 환기장치의 소음원은 블로워로 나타났으며 소음의 주된 누출 원인은 환기장치 구조체의 낮은 차음성능 때문이었음을 알 수 있었다. 또한 이를 제어하기 위하여 장치 내부에 고무시트 등의 차음재를 설치한 결과 폐열회수환기장치의 소음기준인 40 dBA 이하를 만족함을 알 수 있었다.

슬롯관형 초음속 배기노즐의 공력소음에 관한 연구 (A Study on the Aerodynamic Noise of a Supersonic Exhaust Nozzle of Slotted Tube)

  • 이동훈;뢰호방총
    • 대한기계학회논문집B
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    • 제24권1호
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    • pp.132-142
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    • 2000
  • The objective of this study is to experimentally investigate the noise propagating characteristics, the noise reduction mechanism and the performance of a slotted tube attached at the exit plane of a circular convergent nozzle. The experiment is performed through the systematic change of the jet pressure ratio and the slot length under the condition of two kinds of open area ratios, 25% and 51%. The open area ratio calculated by the tube length equivalent for the slot length is defined as the ratio of the total slot area to the surface area of a slotted tube. The experimental results for the near and far field sound, the visualization of jet structures and the static pressure distributions in the jet passing through a slotted tube are presented and explained in comparison with those for a simple tube. The propagating characteristics of supersonic jet noises from the slotted tube is closely connected with the slot length rather than the open area ratio, and its propagating pattern is similar to the simple tube. It is shown that the slotted tube has a good performance to suppress the shock-associated noise as well as the turbulent mixing noise in the range of a limited jet pressure and slot dimension. The considerable suppression of the shock‘associated noise is mainly due to the pressure relief caused by the high-speed jets passing through the slots on the tube. Both the strength of shock waves and the interval between them in a jet plume are decreased by the pressure relief. Moreover, the pressure relief is divided into the gradual and the sudden relief depending upon the open area ratio of the slotted tube. Consequently, the shock waves in a jet plume are also changed by the type of pressure relief. The gradual pressure relief caused by the slotted tube with the open area ratio 25% generates the weak oblique shock waves. On the contrary, the weak normal shock waves appear due to the sudden pressure relief caused by the slotted tube with the open area ratio 51%.

피치각 변화에 따른 헬리콥터 로터에서의 두께 및 하중소음 방사 (Thickness and Loading Noise from Helicopter Rotor at various Pitch Angles)

  • 유기완
    • 한국항공우주학회지
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    • 제35권10호
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    • pp.868-874
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    • 2007
  • 정지비행시의 헬리콥터 로터 모형의 블레이드의 피치각 변화가 소음방사에 미치는 영향을 수치해석을 통해 파악하였다. 공력 자료는 비정상 패널법과 경험후류 방법을 이용하여 구하였으며, $0^{\circ}$에서 $9^{\circ}$까지 등간격으로 $1.5^{\circ}$ 씩 피치각을 증가시키면서 블레이드 표면상의 공력 하중 분포를 얻어내었다. 수치해석을 통해 얻어낸 두께 소음은 피치각에 무관한 결과를 보였으나, 하중소음은 피치각이 $1.5^{\circ}$ 씩 증가할 때 마다 대략 3~4dBA정도로 소음의 세기가 증가하는 경향을 보였으며, 이정도의 증가분은 소음이 더 커졌음을 감지할 수 있는 충분한 크기라 할 수 있다. 또한 하중소음의 방향성 결과로부터 블레이드의 윗면 보다는 아랫면에서의 소음의 세기가 더 크게 나옴을 알 수 있었다.

4톤급 지게차 냉각홴 소음 저감에 관한 실험적 연구 (An Experimental Study on the Noise Reduction of Cooling Fans for Four-ton Forklift Machines)

  • 최대식;김석우;염태영;이승배
    • 드라이브 ㆍ 컨트롤
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    • 제18권1호
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    • pp.1-8
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    • 2021
  • This paper presents research on methods for the reduction of forklifts' noise level for the increased comfort and safety of its operator. A cooling fan with a high air volume flow rate installed in the forklift acts as an important design parameter which efficiently cools the heat exchanger system, helping to transfer internal heat from the engine room to the outdoors with both transmitted and diffracted opening noises. The cooling fan contributes significantly to both the forklift's emitted sound power and the operator room's noise level, thereby necessitating research on the forklift's reduction of acoustic power level and transmission. A noise analysis for various fan models with a biomimetic design based on eagle-wing geometry was conducted. In addition to the acoustic power generation, the aerodynamic performance of the cooling blade is also strongly influenced by the design of airfoil distribution, thereby requiring optimization. The cooling fans were fabricated and installed in the forklift in order to check the efficacy of the forklift engine's cooling, and the final version of the fan was measured for its ability to lower acoustic power level and cool the engine room. This study explains the aerodynamic and acoustic features of the designed fans with the use of BEM analysis and forklift test results.

차량용 전자식 웨이스트 게이트 터보차져의 밸브 떨림음에 대한 실험적 고찰 (Experimental investigation on valve rattle noise of automotive electronic-wastegate turbochargers)

  • 박호일;엄상봉;김영강;황준영
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2013년도 추계학술대회 논문집
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    • pp.686-686
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    • 2013
  • 차량용 터보차져는 디젤엔진뿐만이 아니라 가솔린 엔진에서도 장착이 보편화 되었다. 터보차져는 엔진의 효율과 출력을 효과적으로 증가시키는데 매우 훌륭한 장치이기는 하나, 여러 가지의 소음 문제를 유발시키기도 한다. 이들 소음은 회전축의 거동에 의하여 유발되는 구조 전달 소음과 공기 유동에 의하여 유도되는 공력 소음으로 구분된다. 이와 더불어 웨이스트게이트 밸브를 전자적으로 제어하는 액츄에이터계 거동으로부터 발생되는 기계적 소음이 있는데, 이것이 밸브 떨림음이다. 이 소음은 밸브가 열려 있을 때에만 발생하는데, 이는 연결 구조물 사이의 간극이 외력에 의하여 강제 접촉을 유지하지 않고 밸브부터 액츄에이터 사이에 연결되어 있는 각 연결 구조물이 서로 자유단으로 접촉하고 있기 때문이다. 각 자유단 접촉점에서는 배기가스 맥동파에 의하여 충격 진동이 발생하고 이것이 터빈하우징으로 전달되어 밸브 떨림음이 발생하는 것이다. 그러나, 액츄에이터의 기계적 구동력에 의하여 액츄에이터의 모든 연결 구조물이 강제접촉을 유지하고 있는 기계식 액츄에이터에서는 발생하지 않는다. 본 논문에서는 불평형 회전축을 갖는 소형 진동 모터를 이용하여 전자식 액츄에이터에서 발생하는 밸브 떨림음 평가를 위한 장치를 고안하였으며, 이 장치를 이용하여 밸브 떨림음의 저감효과를 평가하였다. 소음 저감 방법으로는 구조물간 접촉 간극 축소 또는 웨이브 와셔 삽입, 밸브레버와 터빈하우징 사이에 조립되는 부싱의 헐거움 끼움이 효과적임을 확인하였다.

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고속철도 축소모형의 환경소음 예측을 위한 소음원 연구 (A Study of Sound Source to predict Environment Noise in High Speed Train : Scaled model)

  • 김태민;한재현;김정태
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2011년도 춘계학술대회 논문집
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    • pp.1342-1351
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    • 2011
  • Nowadays rolling stock has become a fast and convenient transportation and increased in its demands. But the improvement of speed has result in increase of aerodynamic noise and therefore residential districts near by the railroad are now constantly suffering from the racket. Thus the study regarding rolling stock's environmental noise measurement and appraisal has become important. The case of environmental noise, there are no changes of tone so prediction can be made by reducing areas around the railway. This is part of the study which estimates the noise around the railway using scaled model, and the source of the noise has been researched on. The scaled model of rolling stock will have to be able to make high frequency and it needs to be spread out in a short amount of time. When popping a balloon or firing a gun fits its condition and this study analyzed the characteristics of these two different noises. Measurement was held on a wide vacant lot and the reflection effect of the ground is additionally examined. It is judged to be used in the future when predicting the environmental noise of railway vehicles.

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Prediction of Specific Noise Based on Internal Flow of Forward Curved Fan

  • Sasaki, Soichi;Hayashi, Hidechito;Hatakeyama, Makoto
    • International Journal of Fluid Machinery and Systems
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    • 제2권1호
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    • pp.80-91
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    • 2009
  • In this study, a prediction theory for specific noise that is the overall characteristic of the fan has been proposed. This theory is based on total pressure prediction and broadband noise prediction. The specific noises of two forward curved fans with different number of blades were predicted. The flow around the impeller having 120 blades (MF120) was more biased at a certain positions than the impeller with 40 blades (MF40). An effective domain of the energy conversion of MF40 has extended overall than MF120. The total pressure was affected by the slip factor and pressure loss caused by the vortex flow. The suppression of a major pressure drop by the vortex flow and expansion of the effective domain for energy conversion contributed to an increase in the total pressure of MF40 at the design point. The position of maximum relative velocity was different for each fan. The relative velocity of MF120 was less than that of MF40 due to the deviation angle. The specific noise of MF120 was 2.7 dB less than that of MF40 due to the difference in internal flow. It has been quantitatively estimated that the deceleration in the relative velocity contributed to the improvement in the overall performance.

Noise Prediction of Ducted Fan Unmanned Aerial Vehicles considering Strut Effect in Hover

  • Park, Minjun;Jang, Jisung;Lee, Duckjoo
    • International Journal of Aeronautical and Space Sciences
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    • 제18권1호
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    • pp.144-153
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    • 2017
  • In recent years, unmanned aerial vehicles (UAVs) have been developed and studied for various applications, including drone deliveries, broadcasting, scouting, crop dusting, and firefighting. To enable the wide use of UAVs, their exact aeroacoustic characteristics must be assessed. In this study, a noise prediction method for a ducted fan UAV with complicated geometry was developed. In general, calculation efficiency is increased by simulating a ducted fan UAV without the struts that fix the fuselage to the ducts. However, numerical predictions of noise and aerodynamics differ according to whether struts are present. In terms of aerodynamic performance, the total thrust with and without struts is similar owing to the tendency of the thrust of a blade to offset the drag of the struts. However, in aeroacoustic simulations, the strut effect should be considered in order to predict the UAV's noise because noise from the blades can be changed by the strut effect. Modelling of the strut effect revealed that the dominant tonal noises were closely correlated with the blade passage frequency of the experimental results. Based on the successful detection of noise sources from a ducted fan UAV system, using the proposed noise contribution contour, methods for noise reduction can be suggested by comparing numerical results with measured noise profiles.

Design, Implementation, and Flight Tests of a Feedback Linearization Controller for Multirotor UAVs

  • Lee, Dasol;Lee, Hanseob;Lee, Jaehyun;Shim, David Hyunchul
    • International Journal of Aeronautical and Space Sciences
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    • 제18권4호
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    • pp.740-756
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    • 2017
  • This paper proposes a feedback-linearization-based control algorithm for multirotor unmanned aerial vehicles (UAVs). The feedback linearization scheme is highly efficient for considering nonlinearity between the rotational and translational motion of multirotor UAVs. We also propose a dynamic equation that reflects the aerodynamic effects of the vehicles; the equation's parameters can be determined through curve fitting using actual flight data. We derive the feedback linearization controller from the proposed dynamic equation, and propose a Luenberger observer to attenuate measurement noises. The proposed algorithm is implemented using our in-house flight control computer, and we describe its implementation in detail. To investigate the performance of the proposed algorithm, we carry out two flight scenarios: the first scenario, an autonomous landing on a moving platform, is a test of maneuverability; the second, picking up and replacing an object, test the algorithm's accuracy. In these scenarios, the proposed algorithm precisely controls multirotor UAVs, and we confirm that it can be successfully applied to real flight environments.

고속철도 터널에서 발생하는 파동현상에 관한 충격파관의 연구(1) - 압축파의 특성에 대하여 - (Study of Shock Tube for Wave Phenomenon in High Speed Railway Tunnel(1) - On the characteristics of Compression Wave -)

  • 김희동
    • 대한기계학회논문집
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    • 제18권10호
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    • pp.2686-2697
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    • 1994
  • When a railway train enters a tunnel at high speed, a compression wave is formed in front of the train and propagates along the tunnel. The compression wave subsequently emerges from the exit of the tunnel, which causes an impulsive noise. In order to estimate the magnitudes of the noises and to effectively minimize them, the characteristics of the compression wave propagating in a tunnel must be understood. In the present paper, the experimental and analytical investigations on the attenuation and distortion of the propagating compression waves were carried out using a model tunnel. This facility is a kind of open-ended shock tube with a fast-opening gate valve instead of a general diaphragm. One-dimensional flow model employed in the present study could appropriately predict the strength of the compression wave, Mach number and flow velocity induced by the compression wave. The experimental results show that the strength of a compression wave decreases with the distance from the tunnel entrance. The decreasing rate of the wave strength and pressure gradient in the wave is strongly dependent on the strength of the initial compression wave at the tunnel entrance.