• 제목/요약/키워드: Inclined Centrifugal Impeller

검색결과 6건 처리시간 0.023초

원심 임펠러가 장착된 발효조에서 G. hansenii에 의한 미생물셀룰로오스 생산 (Production of Bacterial Cellulose by Gluconacetobacter hansenii Using a New Bioreactor Equipped with Centrifugal Impellers)

  • 칸살만;쉐자드오머;칸타우스;하정환;박중곤
    • Korean Chemical Engineering Research
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    • 제47권4호
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    • pp.506-511
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    • 2009
  • 미생물셀룰로오스의 생산성을 높이기 위하여 원심(centrifugal) 임펠러와 경사원심(inclined centrifugal) 임펠러가 사용되었다. 발효조 내의 유체흐름 형태와 부피산소전달 계수가 고찰되었으며 원심 임펠러 및 경사원심 임펠러가 장착된 발효조 내에서 G. hansenii PJK 균주에 의하여 미생물 셀룰로오스가 생산되었다. 유체는 발효조 하부에서 원심 임펠러의 실린더 내부를 통과하여 발효조 벽면을 향해 순환되었다. 임펠러의 회전속도 100 rpm에서 부피산소전달계수는 터바인 임펠러 계에 비하여 경사원심 임펠러의 경우는 23%, 원심 임펠러의 경우는 15%에 불과하였다. 하지만 미생물셀룰로오스 생산 불능 돌연변이주로의 전환이 방지되어 20 rpm의 경사원심 임펠러의 회전속도에서 미생물셀룰로오스의 생산량이 터바인임펠러의 최적회전속도 300 rpm에서의 미생물셀룰로오스 생산량과 같았다.

Aeroacoustic Characteristics and Noise Reduction of a Centrifugal Fan for a Vacuum Cleaner

  • Jeon, Wan-Ho;Rew, Ho-Seon;Kim, Chang-Joon
    • Journal of Mechanical Science and Technology
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    • 제18권2호
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    • pp.185-192
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    • 2004
  • The aeroacoustic characteristics of a centrifugal fan for a vacuum cleaner and its noise reduction method are studied in this paper. The major noise source of a vacuum cleaner is the centrifugal fan. The impeller of the fan rotates at over 30000 rpm, and generates very high-level noise. It was revealed that the dominant noise source is the aerodynamic interaction between the rotating impeller and stationary diffuser. The directivity of acoustic pressure showed that most of the noise propagates backward direction of the fan-motor assembly. In order to reduce the high tonal sound generated from the aerodynamic interaction, unevenly pitched impeller and diffuser, and tapered impeller designs were proposed and experiments were performed. Uneven pitch design of the impeller changes the sound quality while the overall sound power level (SPL) and the performance remains similar. The effect of the tapered design of impeller was evaluated. The trailing edge of the tapered fan is inclined. This reduces the flow interaction between the rotating impeller and the stationary diffuser because of some phase shifts. The static efficiency of the new impeller design is slightly lower than the previous design. However, the overall SPL is reduced by about 4 dB(A). The SPL of the fundamental blade passing frequency (BPF) is reduced by about 6 dB (A) and the 2$\^$nd/ BPF is reduced about 20 dB (A). The vacuum cleaner with the tapered impeller design produces lower noise level than the previous one, and the strong tonal sound was dramatically reduced.

청소기의 공력소음 특성 파악 및 저소음화에 관한 연구 (A Study on the Identification of Aeroacoustic Noise and Noise Reduction for a Vacuum Cleaner)

  • 전완호;백승조;김창준
    • 한국소음진동공학회논문집
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    • 제13권6호
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    • pp.460-466
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    • 2003
  • The aeroacoustic characteristics and noise reduction method of a centrifugal fan for a bagless vacuum cleaner were studied. The major noise source of vacuum cleaner is the centrifugal fan. The impeller of the fan rotates over 30000 rpm and generates very high-level piercing noise. It was found that the dominant noise source of the fan is generated from the aerodynamic interaction between the highly rotating impeller and stationary diffuser. In order to reduce the high tonal sound generated from the aerodynamic interaction between the impeller and diffuser, tapered impeller was carefully designed and tested. The trailing edge of the tapered impeller was inclined and this reduces the flow interactions between the rotating impeller and the stationary diffuser because of some phase shift. The static efficiency of the new impeller is slightly lower than the conventional one. The overall SPL is reduced about 3.6 dBA. The SPL of blade passing frequency(BPF) is reduced about 6 dBA and the $2^{nd}$ BPF is reduced about 20 dBA. The vacuum cleaner with the tapered impeller has lower noise level than that of the previous impeller and the strong tonal sound was dramatically reduced.

청소기의 공력소음 특성 파악 및 저소음화에 관한 연구 (A Study on the Identification of Aeroacoustic Noise and Noise Reduction for a Vacuum Cleaner)

  • 전완호;백승조;김창준;허남건
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 춘계학술대회논문집
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    • pp.633-638
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    • 2002
  • The vacuum cleaner that has no dust bag generates very high level annoying noise. The dominant noise source is the 2$\^$nd/ BPF tone of the rotating impeller. In order to reduce the noise, we identify the acoustic characteristics and reduce the noise of the vacuum cleaner and centrifugal fan. The resonance phenomenon is observed in blade passages and we found out that the resonance frequency is very close to the 2$\^$nd/ BPF. In order to reduce this high-level peak noise, new impeller is designed in this paper. The trailing edge of new impeller is inclined and this makes the flow interactions between the rotating impeller and the stationary diffuser vane occurs with some phase shift. The performance of new impeller is similar to the old one but the overall SPL is reduced about 3.6dBA. The SPL of BPF is reduced about 6dBA and 2$\^$nd/ BPF is reduced about 20dBA. The vacuum cleaner, which uses newly developed centrifugal fan, generate more comfortable noise than the old model and the strong tonal sound was dramatically reduced.

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터보 압축기 임펠러-디퓨저 운동장에 대한 정상상태 해석 (Steady Simulations of Impeller-Diffuser Flow Fields in Turbocompressor Applications)

  • 남삼식;박일영;이성룡;주병수;황영수;인배석
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2005년도 연구개발 발표회 논문집
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    • pp.405-412
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    • 2005
  • Numerical and experimental investigations were conducted to assess the aerodynamic performance of several centrifugal compressors. In order to impose an appropriate physics at the interface between impeller and vaned diffuser numerically, two different techniques, frozen rotor and stage models, were applied and the simulation results were compared with the corresponding prototype test data. An equivalent sand-grain roughness height was utilized in the present computational study to consider a relative surface roughness effect on the stage performance simulated. From a series of investigations, it was found that the stage model is more suitable than the frozen rotor scheme for the steady interactions between impeller and diffuser in turbocompressor applications. It is supposed that the solution by frozen rotor scheme is inclined to overrate the non-uniformity of the flow fields. The predicted aerodynamic performance accounting for surface roughness effect shows favorable agreement with experimental data. Simulations based on the aerodynamically smooth surface assumption tend to overestimate the stage performance.

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재생 펌프의 날개 각도에 따른 성능 변화에 관한 실험적 연구 (Experimental Investigation on the Hydraulic Performance of the Regenerative Pump According to the Blade Angle)

  • 유일수;최원철;박무룡;이공훈
    • 한국유체기계학회 논문집
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    • 제16권5호
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    • pp.5-10
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    • 2013
  • The regenerative pump is a kind of turbomachine which is capable of developing high pressure rise at relatively lower flow rates compared to the centrifugal and axial pumps. Although the efficiency of regenerative pumps is much lower than other turbomachines, still they have been widely used in many industrial applications for working at low specific speeds. There are some theoretical models to analysis the pump performance, however, the effect of the blade angle on the pump performance has not been covered in any model to date. In the present study, experimental study on the regenerative pump performance according to the impeller blade angle and its shape has been carried out. The straight radial blades with forward, backward and chevron blades which have inclined angles of $15^{\circ}$, $30^{\circ}$ and $45^{\circ}$ were tested. The pump performance characteristics as the pressure head, efficiency were obtained depending on the flow rate for every impeller, and their results, expressed in appropriate non-dimensional coefficients, were compared and analysed in detail. From the experimental results, it was found that the pressure head and the efficiency depend strongly on the blade angles as well as the blade type. These experimental data has made it possible to better understand the effects of the blade angle on the pump performance, and widen the applicability of the current performance analysis and design models with including the effect of blade angles.