• 제목/요약/키워드: Turbo fan

검색결과 66건 처리시간 0.03초

엇회전식 축류홴의 공력 특성에 관한 실험적 연구 (Experimental Study on the Aerodynamic Characteristics of a Counter-Rotating Axial Fan)

  • 최진용;조이상;조진수;원유필
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집B
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    • pp.441-446
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    • 2000
  • The experiments of the Aerodynamic characteristics of a counter-rotating axial fan were carried out. The performance tests of a single and a counter-rotating axial fan were carried out based on the Korean Standard Testing Methods for Turbo-fans and Blowers(KS B 6311). The performances of single and counter-rotating axial fans were obtained and compared with each other. The flow fields of a counter-rotating axial fan at the peak efficiency point were measured using a five-hole probe. As a result, compared with the performance of a single-rotating axial fan, that of a counter-rotating axial fan was superior. And it is confirmed that most of the swirl flow generated by the front rotor was eliminated by the rear rotor.

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대형 디젤엔진 자동변속기 오일쿨러 냉각팬 성능에 관한 연구 (A Study on Performance of Cooling Fan for Auto Transmission Oil Cooler in the Large-Size Diesel Engine)

  • 이중섭;서정세;송철기;윤지훈
    • 한국유체기계학회 논문집
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    • 제13권6호
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    • pp.71-76
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    • 2010
  • This study has investigated numerically and experimentally the flow characteristic of air-cooling fan for transmission oil cooler in the large-size diesel engine. Impellers of cooler were composed of eight normal-scale and eight small-scale blades in the zig-zag pattern. In order to increase the discharge pressure of cooling fan, turbo type of fan blade is proposed in the impeller for transmission oil cooler. The fluidic performance of cooling fan has been estimated numerically by using the commercial code and experimentally carried out with reference on AMCA Standard 210-99. As a result, it is confirmed that the numerical result for performance curve is in good agreement with experimental data.

바이패스 덕트 손실 해석을 이용한 복축 혼합형 터보팬 엔진의 윈드밀 특성 연구 (A Study of Windmilling Characteristics of Twin-Spool Axi-Centrifugal Turbo-Fan Engine Using an Analysis of Bypass-duct Loss)

  • 김민정;최성욱;노태성;임진식
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제21회 추계학술대회 논문집
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    • pp.211-214
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    • 2003
  • 바이패스 덕트 손실을 고려한 비행 중의 복축 혼합형 터보팬 엔진의 윈드밀 성능을 예측하기 위해, 본 연구에서는 원심 및 축류 압축기, 축류 터빈의 윈드밀 작동 과정과 물리적 현상을 규명하고 바이패스 덕트를 통과한 공기와의 혼합 현상을 해석하였다. 윈드밀 성능 예측의 결과는 유차원 해석을 통해 비교 분석하였다.

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엇회전식 축류 펜의 공력 특성에 관한 실험적 연구 (Experimental Study on the Aerodynamic Characteristics of a Counter-Rotating Axial Flow Fan)

  • 최진용;조이상;조진수;원유필
    • 대한기계학회논문집B
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    • 제26권2호
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    • pp.201-210
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    • 2002
  • Experiments were done for performance and flow characteristics of a counter-rotating axial flow fan. Performance curves of a counter-rotating axial flow fan were obtained and compared by varying the blade pitch angles. The fan characteristic curves were obtained following the Korean Standard Testing Methods for Turbo Fans and Blowers (KS B 6311). The fan flow characteristics were measured using a five-hole probe and a slanted hot-wire. The velocity profiles between the hub and tip of the fans were measured and analyzed at the peak efficiency point. The peak efficiency of the counter-rotating axial flow fan was improved about 15% respectively, compared with the single rotating axial fan. The single rotating axial flow fan showed relatively law efficiency due to the swirl velocities behind rotor exit which produced pressure losses. The counter-rotating axial flow fan showed that the swirl velocity generated by the front rotor was eliminated by the rear rotor and the associated dynamic pressure is recovered in the from of the static pressure rise.

Kirchhoff-BEM 을 이용한 Plenum Fan 소음해석 (Acoustic Analysis of Plenum Fan using Kirchhoff-BEM)

  • 송우석;장근정;이승배
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
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    • pp.89-93
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    • 2004
  • To numerically construct the sound fields by a plenum fan mostly found in Air-Handling Unit (AHU), the Kirchhoff-BEM approach was applied to the near-field data of a turbo fan. The scattering effects were found to be significant by the plenum box structure for high-frequency components of source. The directivity petterns and sound pressure levels were also dependent upon the helmholts number which must be considered of the design stage for sound reduction program.

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자동제어계측을 이용한 송풍기 성능시험 (Fan Performance Test with Automatic Control and Measurement)

  • 최영석;김진권
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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    • pp.373-378
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    • 2003
  • In this paper, build up of fan performance tester in KITECH was introduced. The fan tester was set up based on AMCA standards 210-99, ANSI/ASHRAE 51-1999 with maximum flowrate within $1000\;m^{3}/min$. Both of inlet and outlet chamber setup with multiple nozzles described in AMCA 210 were established. The development of fully automatic control and measurement system are described. With this system, the accuracy of fan performance test can be maintained through the various flowrate and the uncertainty can be reduced.

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2단 축류팬과 엇회전식 축류팬의 공력 특성에 관한 실험적 연구 (Experimental Study on the Aerodynamic Characteristics of a Two Stage and a Counter-Rotating Axial Flow Fan)

  • 조이상;조진수
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집B
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    • pp.541-547
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    • 2000
  • Experiments were done for the comparison of performance and flow characteristics between a two stage axial flow fan and a counter-rotating axial flow fm. The fan performance curves were obtained by the Korean Standard Testing Methods for Turbo Fans and Blowers (KS B 6311). The fan flow characteristics were measured using a five-hole probe by the non-nulling method. Each stage of the two stage axial flow fan used for the present study has an eight bladed rotor and thirteen stator blades. The front and the rear rotor of the counter-rotating axial flow fan have eight blades each and are driven by coaxial counter rotating shafts through a gear box located between the rear rotor and the electric motor. Both of the two axial fan configurations use identical rotor blades and the same operating conditions for the one-to-one comparison of the two. Performance characteristics of the two configurations were obtained and compared by varying the blade setting angles and axial gaps between the blade rows. The passage flow fields between the hub and tip of the fans were measured and analyzed for the particular operating conditions of peak efficiency, minimum and maximum pressure coefficients.

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진공청소기용 팬 모터의 비정상 유동 해석 및 공력소음 해석 (The Analysis of the Unsteady Flow Field and Aerodynamic Sound of Fan Motor in a Vacuum Cleaner)

  • 김재열;심재기;송경석;오성민;양동조;김우진
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2004년도 춘계학술대회 논문집
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    • pp.281-286
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    • 2004
  • The vacuum cleaner motor runs on very high speed for the suction power. Specially, the motive power is provided by the impeller being rotate on very high speed. And centrifugal fan consists of the impeller, the diffuser, and the circular casing. Due to the high rotating speed or the impeller and small gap distance between the impeller and diffuser, the centrifugal fan makes very high noise level at BPF and harmonic frequencies. In order to calculate the sound pressure of centrifugal fan, the unsteady flow data is needed. And Noise cause is dividing to fluid noise by exhaust flow of fan and vibration noise by rotational vibration of vacuum cleaner fan motor. Until now, measuring method has been used to measure vibration by the accelerometer; this method has been not measured for the vibration in some parts of brush and commutator because of motor construction and 3-D vibrating mode. This paper was purposed on the accurate analysis, using laser vibration analyzer,. By using this measured data of noise cause against the difficult part in old times, we would like to use for the design of silent fan motor.

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