• 제목/요약/키워드: Tip-out Noise

검색결과 33건 처리시간 0.026초

깃 끝단 개선을 통한 냉장고용 축류홴 저소음화에 대한 연구 (Study on Noise Reduction of an Axial Fan for Refrigerator through Modification of the Blade Tip)

  • 김창준;전완호;정용규
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 춘계학술대회논문집
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    • pp.639-644
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    • 2002
  • In this paper, a successful noise reduction of an axial flow fan for a refrigerator is presented. The vortex sheet generated at the blade tip of fan was suppressed by changing the shape of the tip. The structure of vortex sheet and detailed flow pattern around the fan were studied by two-dimensional LDV(Laser-Doppler Velocimetry). Effective ways to work out the result as mentioned above are to make the tip of the blade varied in thickness and to have elliptical shapes. To seek the optimal value fur the shape of new fan, several cases were examined. Through the application of the methods, the refrigerator became less noisy by 3.8 dB(A) in terms of air-borne noise produced only by the axial flow fan compared to the current one.

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물 분사를 이용한 프로펠러 날개 끝 보오텍스 캐비테이션 제어 (Propeller Tip Vortex Cavitation Control Using Water Injection)

  • 이창섭;한재문;김진학;안병권
    • 대한조선학회논문집
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    • 제47권6호
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    • pp.770-775
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    • 2010
  • As considerable interests in noise emission from the ships have been increased, control of the propeller cavitation generating vibration and radiating noise is looming large. In general, the tip vortex cavitation is first produced in case of full scale propellers, and noise levels rise dramatically from that moment. In order to reduce induced noise from the tip vortex cavitation and hence increase the cavity inception speed, we propose the mass injection method. Water injected from the propeller tip decreases rotating speed of the tip flow, and it restrains growing the tip vortex cavity. Experimental investigations of the model tests carried out in a large cavitation tunnel show that the tip vortex cavitation is effectively controled by water injection from the propeller tip.

구동계 비틀림진동저감을 위한 이중질량플라이휠의 파라미터해석 (Parametric Study of DMFW to Reduce Torsional Vibration of Power Train System)

  • 이강우;정재훈;송영래;지태한
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 춘계학술대회논문집
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    • pp.405-410
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    • 2002
  • In this paper, numerical method of evaluating the influence of Dual Mass Flywheel(DMFW) to the torsional vibration of the automotive power train system is developed. And we applied the procedure to the currently being developed HMC's DMFW attached to an FF car to find out the best performance characteristics during the Tip-in/Tip-out operating condition. In doing this we compared the numerical results with the experimental results and Performed Parametric studies. We find out that the torsional vibrational characteristics of power train system can be significantly improved when we optimally choose DMFW, and the developed numerical procedure could be used as valuable tools in developing new DMFW.

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3차원 날개의 캐비테이션 소음 계측시험 (Experimental Study on the Cavitation Noise of a Hydrofoil)

  • 이승재;서종수;한재문
    • 대한조선학회논문집
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    • 제44권2호
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    • pp.111-118
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    • 2007
  • In order to investigate the noise characteristics of the different caviation, noise measurements were carried out in a large cavitation tunnel of the Samsuug Ship Model Basin(SSMB). The noise measurements for a 3-dimensional hydrofoil were carried out at the angle of attack of $12^{\circ}$ and $16^{\circ}$ according to the decrease in cavitation number. It is exhibited that sound pressure level(SPL) increased sharply with cavitation inception. The frequency of the noise induced by sheet cavitation was higher than that of tip vortex cavitation in the phase of cavitation inception. Within the range of the high frequency, in the case of fully developed cavitation, sheet cavitation noise was significantly increased in sound pressure level compared with tip vortex cavitation noise. In this study, the noise characteristics of the different cavitation types were considered experimentally and would be utilized as a basis for the analysis of propeller cavitation noise.

풍력터빈 블레이드 주위 흐름의 유동특성에 대한 실험적 분석 (Experimental Analysis of Flow Characteristics around Wind-Turbine Blades)

  • 이정엽;이상준
    • 한국가시화정보학회지
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    • 제7권2호
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    • pp.64-71
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    • 2010
  • The flow and noise characteristics of wake behind wind-turbine blades have been investigated experimentally using a two-frame particle image velocimetry (PIV) technique. Experiments were carried out in a POSTECH subsonic large wind-tunnel ($1.8^W{\times}1.5^H{\times}4.3^L\;m^3$) with KBP-750D (3-blade type) wind-turbine model at a freestream velocity of $U_o\;=\;15\;m/s$ and a tip speed ratio $\lambda\;=\;6.14$ (2933 rpm). The wind-turbine blades are connected to an AC servo motor, brake, encoder and torque meter to control the rotational speed and to extract a synchronization signal for PIV measurements. The wake flow was measured at four azimuth angles ($\phi\;=\;0^{\circ}$, $30^{\circ}$, $60^{\circ}$ and $90^{\circ}$) of the wind-turbine blade. The dominant flow structure of the wake is large-scale tip vortices. The turbulent statistics such as turbulent intensity are weakened as the flow goes downstream due to turbulent dissipation. The dominant peak frequency of the noise signal is identical to the rotation frequency of blades. The noise seems to be mainly induced by the tip vortices.

말단질량을 갖는 원형강관 캔틸레버 보의 결함탐지기법 (Fault Detection Method of Pipe-type Cantilever Beam with a Tip Mass)

  • 이종원
    • 한국소음진동공학회논문집
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    • 제25권11호
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    • pp.764-770
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    • 2015
  • A crack identification method using an equivalent bending stiffness and natural frequency for cracked beam is presented. Modal properties of cantilever beam with a tip mass is identified by applying the boundary conditions to a general solution. An equivalent bending stiffness for cracked beam based on an energy method is used to identify natural frequencies of cantilever thin-walled pipe with a tip mass, which has a through-the-thickness crack, subjected to bending. The identified natural frequencies of the cracked beam are used in constructing training patterns of neural networks. Then crack location and size are identified using a committee of the neural networks. Crack detection was carried out for an example beam using the proposed method, and the identified crack locations and sizes agree reasonably well with the exact values.

터보엔진의 저소음 흡기 RCV 시스템 개발 (A Development of an Intake RCV System for the Low Noise Turbo Engine)

  • 이종규;김재헌;강상규;강구태
    • 한국소음진동공학회논문집
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    • 제20권8호
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    • pp.734-741
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    • 2010
  • In this paper, an intake RCV system for low noise turbo engine was developed through optimization process of a geometric path of compressor housing and an open rate of recirculation valve. At first, the critical customer requirement from voice of customer was defined and quality function deployment of an intake RCV system was executed. And then, the renovative concept design using pugh matrix method was selected as final concept for satisfaction of requirement. Simultaneously, system analysis was carried by function diagram and fishbone diagram. Next, control factors and levels for the optimal design were performed. And, the optimal design of an intake RCV system was studied using design of experiment. Conclusively, we achieved not only cancellation tip-out noise at the driving condition but also improvement of NVH commodity through optimization process of an intake RCV system, which is optimal configuration of compressor housing and recirculation valve.

Multi-point detection of hydrogen using the hetero-core structured optical fiber hydrogen tip sensors and Pseudorandom Noise code correlation reflectometry

  • Hosoki, Ai;Nishiyama, Michiko;Igawa, Hirotaka;Seki, Atsushi;Watanabe, Kazuhiro
    • 동력기계공학회지
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    • 제19권3호
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    • pp.11-15
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    • 2015
  • In this paper, the multi-point hydrogen detection system based on the combination of the hetero-core optical fiber SPR hydrogen tip sensor and interrogator by pseudorandom noise (PN) code correlation reflectometry has been developed. In a light intensity-based experiment with an LED operating at 850 nm, it has been presented that a transmitted loss change of 0.32dB was induced with a response time of 25 s for 4% $H_2$ in $N_2$ in the case of the 25-nm Au, 60-nm $Ta_2O_5$, and 5-nm Pd multi-layers film. The proposed sensor characteristic shows excellent reproducibility in terms of loss level and time response for the in- and out- $H_2$ action. In addition, in the experiment for multi-point hydrogen detection, all sensors show the real-time response for 4% hydrogen adding with reproducible working. As a result, the real-time multi-point hydrogen detection could be realized by means of the combination of interrogating system and hetero-core optical fiber SPR hydrogen tip sensors.

소형버스 구동계 Clonk 소음 원인규명 및 대책고찰 (An Investigation into Driveline Clonk Noise of Midi - Bus)

  • 이태훈;안상도;김유겸
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2012년도 춘계학술대회 논문집
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    • pp.658-664
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    • 2012
  • This paper presents an investigation into driveline clonk noise of midi-bus. Test was performed for operational acceleration and pressure, torsional vibration of driveline and FRF to TPA. Wavelet analysis was used to study spectral-time characteristics to all measurement data and specially for torsional vibration, lash analysis was carried out. To investigate the path of the clonk in detail, time domain TPA was introduced. With time domain TPA, the contribution of each path for the clonk was estimated by both subjectively and objectively. As a result, Transmission mount part was came to light as the main contributor of issued clonk. This was verified by reinforcing the bracket of transmission side. And 1D torsional nvh performance simulation model was built with measured torsional vibration. The simulation tool was used for prediction of some clonk behavior in tip in-out transient condition.

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축소형 UH-1H 로터에서의 광역소음과 이산소음의 비교 (Comparison of Discrete Noise with Broadband Noise from Small-scaled UH-1H Rotor)

  • 유기완
    • 한국항공우주학회지
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    • 제33권1호
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    • pp.20-25
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    • 2005
  • 본 연구에서는 UH-1H 헬리콥터의 축소 로터에 대한 두께소음과 하중소음, 그리고 와류흘림에 의한 광역소음을 각각 수치계산을 통해 얻어내고, 그 크기를 비교하였다. 로터의 후류형상은 Kocurek과 Tangler의 지정후류 방법을 사용하였으며, 팁 마하수 $M_{T}$의 범위는 0.2, 0.4, 0.8로 나누어서 유동장 계산과 그에 따른 소음해석을 시도하였다. 팁 마흐 수 $M_{T}$ = 0.8에서 와류 흘림에 의한 광역 소음은 가청주파수 대역 및 A-가중함수를 고려하였을 때에 상대적으로 저주파수 특성을 갖는 두께소음이나 하중소음에 비해 작은 값을 보이는 것으로 나타났다. 특히 광역소음은 가청주파수를 벗어난 초음파 영역에서 대부분의 음압을 방사하는 것으로 나타났다. 반면 $M_{T}$를 0.4 이하로 하였을 때에는 광역소음이 저주파수 영역으로 이동하면서 이산소음에 비해 더 소음레벨을 보이는 것으로 나타났다. 즉, 저속 회전하는 헬리콥터 로터의 경우에는 광역소음의 고려가 필수적임을 알 수 있다.