• Title/Summary/Keyword: Small Two-Stage Turbo Blower

Search Result 2, Processing Time 0.016 seconds

Aerodynamic Characteristics Analysis of Small Two-Stage Turbo Blower Using CFD (CFD를 이용한 소형 2단 터보블로워의 공력해석)

  • Seo, Seungjae;Ryu, Minhyoung;Cho, Leesang;Cho, Jinsoo
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.42 no.4
    • /
    • pp.326-335
    • /
    • 2014
  • Aerodynamic characteristics of the small two-stage turbo blower were investigated using commercial CFD tool(ANSYS CFX Ver. 14.5) in this paper. Turbo blower, which is a centrifugal type of turbomachinery, is used in various industries. It is used for application that required high static pressure rising at relatively small volumetric flow rate. In order to understand the mechanism of static pressure rising, the aerodynamic characteristics of the small two-stage turbo blower are analyzed at high rotating speed in this study. The k-${\omega}$ SST turbulence model, which is good at prediction of adverse pressure gradient flows, was applied. The CFD results of the turbo blower are validated by performance test. The static pressure rising of the turbo blower is nonlinearly increased over the first stage and the second stage. The secondary flow occurred at guide vanes, between the casing and the first impeller shroud, and the bottom of the impeller disk. As a result, It is required that whole fluid area is analyzed to predict aerodynamic characteristics of small two-stage turbo blower. and the result should be selected with considering for error from experiment and CFD.

Performance Analysis for Turbo Blower According to Inlet-Vane Angles (입구베인 각도에 따른 터보블로어 성능특성 연구)

  • Jang, Choon-Man;Lim, Soo-Jung;Yang, Sang-Ho
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.35 no.3
    • /
    • pp.301-307
    • /
    • 2011
  • Turbo blowers are mainly used in refuse collection systems. We discuss blower performance in relation to the angle of the inlet vane installed at the upstream of the blower. The flow characteristics of the components are analyzed by three-dimensional Navier-Stokes analysis and compared to experimental results. A two-stage serially connected turbo blower is introduced to analyze the performance experimentally. Throughout the experimental measurements and the numerical simulation, the distorted inlet velocity generated in the small vane angle reduces the performance of the blower, because of the local leading-edge separation and the resulting non-uniform blade loading. We also perform a detailed flow analysis using the results obtained in the numerical simulation.