• Title/Summary/Keyword: Turbo-Machinery

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Application of PIV to Fluid-Machinery Studies (유체기계연구에서의 PIV의 적용)

  • Lee, Y. H.
    • 유체기계공업학회:학술대회논문집
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    • 1997.02a
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    • pp.188-195
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    • 1997
  • The application of PIV to the studies of fluid-machines, especially focused on turbo-machinery is reviewed by scrutinizing the previous investigation. Owing to the inevitable high-speed analysis of turbo-machinery consisting of rotating impellers, the importance of optical setups to cope with illumination problem is frequently mentioned as main ingredient affecting the PIV performance. And the acquisition of the relative velocity and absolute velocity is determined mainly by the optical recording conditions. A few studies cast satisfactory extension of the PIV data to quantitative pressure estimation and related noise assessment.

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Seismic analysis of turbo machinery foundation: Shaking table test and computational modeling

  • Tripathy, Sungyani;Desai, Atul K
    • Earthquakes and Structures
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    • v.12 no.6
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    • pp.629-641
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    • 2017
  • Foundation plays a significant role in safe and efficient turbo machinery operation. Turbo machineries generate harmonic load on the foundation due to their high speed rotating motion which causes vibration in the machinery, foundation and soil beneath the foundation. The problems caused by vibration get multiplied if the soil is poor. An improperly designed machine foundation increases the vibration and reduces machinery health leading to frequent maintenance. Hence it is very important to study the soil structure interaction and effect of machine vibration on the foundation during turbo machinery operation in the design stage itself. The present work studies the effect of harmonic load due to machine operation along with earthquake loading on the frame foundation for poor soil conditions. Various alternative foundations like rafts, barrette, batter pile and combinations of barrettes with batter pile are analyzed to study the improvements in the vibration patterns. Detailed computational analysis was carried out in SAP 2000 software; the numerical model was analyzed and compared with the shaking table experiment results. The numerical results are found to be closely matching with the experimental data which confirms the accuracy of the numerical model predictions. Both shake table and SAP 2000 results reveal that combination of barrette and batter piles with raft are best suitable for poor soil conditions because it reduces the displacement at top deck, bending moment and horizontal displacement of pile and thereby making the foundation more stable under seismic loading.

Optimal design and operation of a turbo blower used for refuse collection system (생활폐기물 관로이송용 터보블로어 운전 및 설계 최적화 연구)

  • Jang, Choon-Man
    • The KSFM Journal of Fluid Machinery
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    • v.13 no.5
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    • pp.58-63
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    • 2010
  • Optimal operation of turbo blowers connected in serial is analyzed by experimental measurements and numerical simulation with three-dimensional Navier-Stokes equations. The turbo blower system considered in the present study is widely used for the refuse collection system. Design optimization of the turbo blower using some design variables is also studied to enhance the performance of the blower. Throughout numerical simulation, it is found that the input energy reduction by optimal operation of the turbo blowers with the proper changes of the rotor's rotating frequency can be reduced a input energy for operating the blower system compared to the conventional on-off operation method theoretically. It is also found that the optimal design method is effective to enhance the performance of the turbo blower.

Performance and Flow Test of a Turbo Pump Inducer (터보 펌프 인듀서의 성능 및 유동실험)

  • Kang, Shin-Hyoung;Yeom, Ki-Tae
    • The KSFM Journal of Fluid Machinery
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    • v.6 no.1 s.18
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    • pp.6-13
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    • 2003
  • Variations of performance and NPSH of a turbo pump inducer were measured. The flows at the inlet and the outlet of the inducer were also experimentally investigated by measuring flow velocity and angle using a 3-hole Pilot tube. Performance and velocity profiles show a similarity for tested speeds, however not for efficiencies. Strong recirculating flows appears at the inlet of inducer even at the design condition. Cavitating flows were also visualized at several NPSH's.

Effects of Vaned Diffuser Shapes on the Flowfields of a Small-Size Turbo-Compressor (소형 터보압축기의 디퓨저 형상변화에 따른 유동특성 고찰)

  • Kim, H.-S.;Kim, Youn J.;Kim, C.-S.
    • The KSFM Journal of Fluid Machinery
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    • v.4 no.3 s.12
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    • pp.21-28
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    • 2001
  • The effects of diffuser shapes on the flowfields of a small-size turbo-compressor have been investigated numerically and experimentally. The optimal design of elements shapes is important to develop the high efficiency turbo-compressor. Typical range of rotating speed for a small-size turbo-compressor is 40,000-70,000rpm. Numerical analyses were conducted to the rectangular and conical shapes of diffuser Three-dimensional, steady and viscous governing equations were solved by SIMPLE algorithm. To confirm the numerical results, the experimental measurements for the static pressure and temperature at the inlet and outlet boundaries were performed. Comparisons of these results were done, and the reasonable agreements were acquired.

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Pressure Characteristics According to the Duct Shapes of Turbo Blowers Connected in Serial (다단 블로어 덕트형상에 따른 압력특성 연구)

  • Park, Young-Bin;Jang, Choon-Man;Yang, Sang-Ho
    • The KSFM Journal of Fluid Machinery
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    • v.13 no.2
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    • pp.30-35
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    • 2010
  • Pressure characteristics according to the duct shapes of turbo blowers connected in serial have been performed to reduce pressure loss in the piping system. To analyze three-dimensional flow field in the turbo blower system, general analysis code, CFX, is introduced in the present work. SST turbulence model is applied to estimate the eddy viscosity. Throughout the numerical simulation for the turbo blower system having a various shape of a inlet guide, optimal inlet guide can be selected. It is found that the pressure loss in the piping system having the optimal inlet guide can be reduced by minimizing the inflow distortion at the upstream of the impeller. Detailed flow analysis of the blower system serially connected is also performed and analyzed.

AEffects of Impeller Blade Thickness on Performance of a Turbo Blower (임펠러 블레이드 두께가 터보블로워 성능에 미치는 영향)

  • Park, Jun-Young;Park, Moo-Ryong;Hwang, Soon-Chan;Ahn, Kook-Young
    • The KSFM Journal of Fluid Machinery
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    • v.13 no.4
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    • pp.5-10
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    • 2010
  • This study is concerned with effects of impeller blade thickness on performance of a turbo blower. This turbo blower is developed as an air supply system in 250 kW MCFC system. The turbo blower consists of an impeller, two vaneless diffusers, a vaned diffuser and a volute. The three dimensional, steady state numerical analysis is simultaneously conducted for the impeller, diffuser and volute to investigate the performance of total system. To consider the non-uniform condition in volute inlet due to volute tongue, full diffuser passages are included in the calculation. The results of numerical analysis are validated with experimental results of thin blade thickness. Total pressure ratio, efficiency, slip factor and blade loading are compared in two cases. The slip factor is different in two cases and the comparison of two cases shows a good performance in thin blade thickness in all aspects.

Development of Turbo Expanders with Hydrostatic Bearings for Hydrogen Liquefaction Plants (정압 베어링을 적용한 수소 액화 공정용 터보 팽창기 개발)

  • Lee, Donghyun;Kim, Byungock;Park, Mooryong;Lim, Hyungsoo
    • Tribology and Lubricants
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    • v.37 no.3
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    • pp.91-98
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    • 2021
  • This paper presents a hydrostatic bearing design and rotordynamic analysis of a turbo expander for a hydrogen liquefaction plant. Th~e turbo expander includes the turbine and compressor wheel assembled to a shaft supported by two hydrostatic radial and thrust bearings. The rated speed is 75,000 rpm and the rated power is 6 kW. For the bearing operation, we use pressurized air at 8.5 bar as the lubricant that is supplied to the bearing through the orifice restrictor. We calculate the bearing stiffness and flow rate for various gauge pressure ratios and select the orifice diameter providing the maximum bearing stiffness. Additionally, we conduct a rotordynamic analysis based on the calculated bearing stiffness and damping considering design parameters of the turbo expander. The predicted Cambell diagram indicates that there are two critical speeds under the rated speed and there exists a sufficient separation margin for the rated speed. In addition, the predicted rotor vibration is under 1 ㎛ at the rated speed. We conduct the operating test of the turbo expander in the test rig. For the operation, we supply pressurized air to the turbine and monitor the shaft vibration during the test. The test results show that there are two critical speeds under the rated speed, and the shaft vibration is controlled under 2.5 ㎛.