• Title/Summary/Keyword: Pressure recovery coeff.

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Performance Test and Aerodynamic Design on the High Pressure Ratio Centrifugal Compressor of a Turbocharger (과급기의 고압력비 원심압축기 공력설계 및 시험평가)

  • Kim, Hong-Won;Ryu, Seung-Hyup;Lee, Geun-Sik
    • The KSFM Journal of Fluid Machinery
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    • v.17 no.6
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    • pp.13-20
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    • 2014
  • It is necessary to design a compressor with high pressure ratio that satisfies the IMO(international maritime organization) NOx emission regulation for the marine diesel engine. Impeller was designed using the modified slip factor with the flow coefficient. The main purpose of this study is to investigate the sensitivity of the compressor performance by the vaned diffuser geometries. The first vaned diffuser type was based on a NACA airfoil, the second was channel diffuser, and the third was conformally transformated configuration of a NACA65(4A10)06 airfoil. The sensitivity of the performance was calculated using a commercial CFD program for three different diffuser geometries. The channel diffuser showed the wide range of operation and higher pressure characteristics, comparing with the others. This is attributed to the flow stability at diffuser. Combined with this results with impeller design, the optimized compressor was designed and verified by the test results.

The Evaluation of Performance and Flow Characteristics on the Diffuser Geometries Variations of the Centrifugal Compressor in a Marine Engine Turbocharger (박용 터보차져의 원심압축기의 디퓨져 형상변경에 따른 성능비교 및 유동특성 평가 연구)

  • Kim, Hong-Won;Ha, Ji-Soo;Kim, Bong-Hwan
    • The KSFM Journal of Fluid Machinery
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    • v.11 no.2
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    • pp.55-63
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    • 2008
  • An examination of the condition of the flow leaving the impeller exit kinetic energy often accounts for 30-50% of the shaft work input to the compressor stage, and for energy efficiency it is important to recover as much of this as possible. This is the function of the diffuser which follows the impeller. The purpose of this study is to investigate the sensitivity of how compressor performances changes as vaned diffuser geometry is varied. Three kinds of vaned diffusers were studied and its results were compared. First vaned diffuser type is based on NACA airfoil and second is channel diffuser and third is conformal transformation of NACA65(4A10)06 airfoil. Mean-line prediction method was applied to investigate the performance and stability for three kinds of diffusers. And CFD analyses have been done for comparison and detailed interior flow pattern study. NACA65(4A10)06 airfoil showed the widest operating range and higher pressure characteristics than the others.