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Numerical study of surge predecessors in centrifugal blower — inlet recirculation

Treść / Zawartość
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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Paper presents the numerical investigation of inlet recirculation in a centrifugal blower. This phenomenon is known as a local flow instability that is not too harmful in centrifugal compressors compared to centrifugal pumps. However recent findings have shown that it can be regarded as a surge predecessor, and hence very significant for compressors. Therefore there is strong need to understand its physics. One of ways to understand it to apply computational fluid dynamic (CFD) simulations. Therefore in this study the transient numerical simulations were conducted and results were related to the experimental data presented in other papers. Simulation confirmed that the inlet recirculation structure can be resolved by means of CFD and the results are in agreement with some available models. Inlet recirculation structure built up gradually along the circumference increasing the power loss. Obtained structure also explained pressure variations observed in experiments. This has shown that CFD can bring significant improvement in existing antisurge systems and recirculation bleeds that extend the machine operating range.
Słowa kluczowe
Rocznik
Tom
Strony
29--44
Opis fizyczny
Bibliogr. 28 poz., rys., tab.
Twórcy
  • Institute of Turbomachinery, Lodz University of Technology, 219/223 Wólczańska, 90-924 Łódź, Poland
  • Institute of Turbomachinery, Lodz University of Technology, 219/223 Wólczańska, 90-924 Łódź, Poland
  • Institute of Turbomachinery, Lodz University of Technology, 219/223 Wólczańska, 90-924 Łódź, Poland
Bibliografia
  • [1] Sen M., Breugelmans F., Schiavello B.: Reverse flow, prerotation and unsteady flow in centrifugal pumps. In: Proc. NEL Fluid Mechanics Silver Jubilee Conf. Glasgow 1979.
  • [2] Breugelmans F.A., Sen M.: Prerotation and fluid recirculation in the suction pipe of contrifugal pumps. In: Proc. 11th Turbomachinery Symp., 1982, 165–180.
  • [3] Schiavello B., Sen M.: On the prediction of the reverse flow onset at the centrifugal pump inlet. ASME Symp. on Performance Prediction of Centrifugal Pumps and Compressors, New Orleans 1980.
  • [4] Tanaka T.: An experimental study of backflow phenomena in a high specific speed propeller pump. Proc. ASME, 80-FE–6, 1980.
  • [5] Fraser W.H.: Recirculation in centrifugal pumps. In: Proc. Construction of Fluid Machinery and Their Relationship to Design and Performance, World Pumps, 1981, 65–86.
  • [6] Tamaki H.: Experimental study on surge inception in a centrifugal compressor. Int. J. Fluid Mach. Sys. 2(2009), 4, 409–417.
  • [7] Liskiewicz G., Horodko L.: Time-frequency analysis of the surge onset in the centrifugal blower. Open Eng. 5(2015), 1, 299–306.
  • [8] Kabalyk K., Liśkiewicz G., Horodko L., Stickland M., Kryłłowicz W.: Use of pressure spectral maps for analysis of influence of the plenum volume on the surge in centrifugal blower. Proc. ASME, 2014, GT2014–26931.
  • [9] Horodko L.: Investigation of centrifugal compressor surge with wavelet methods. In: Proc. 6th Eur. Conf. on Turbomachinery, Fluid Dynamics and Thermodynamics Vol. 2, Lille 7–11 March, 2005, 635–644.
  • [10] Harley P., Spence S., Filsinger D., Dietrich M., Early J.: Meanline modelling of inlet recirculation in automotive. ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, Vol. 2D: Turbomachinery, Düsseldorf, June 16–20, 2014, GT2014-25853, V02DT42A020.
  • [11] Qiu X., Japikse D., Anderson M.: A meanline model for impeller flow recirculation. Proc. ASME Turbo Expo, GT2008–513, 2008.
  • [12] Oh H.W., Yoon E.S., Chung M.K.: An optimum set of loss models for performance prediction of centrifugal compressors. P I Mech. Eng. A-J Pow. 211(1997), 4 , 331–338.
  • [13] Aungier R.H.: Centrifugal Compressors: A Strategy for Aerodynamic Design and Analysis. ASME Press, 2000.
  • [14] Gülich J.F.: Centrifugal Pumps. Springer, Berlin Heidelberg 2014.
  • [15] Hunziker R., Dickmann H.-P., Emmrich R.: Numerical and experimental investigation of a centrifugal compressor with an inducer casing bleed system. P I Mech. Eng. A-J Pow. 215(2001), 6, 783–791.
  • [16] Tamaki H., Unno M., Tanaka R., Yamaguchi S., Ishizu Y.: Enhancement of centrifugal compressor operating range by control of inlet recirculation with inlet fins. J. Turbomach. 138(2016), 10, 01010-1–01010-12
  • [17] Yang M., Zheng X., Zhang Y., Bamba T., Tamaki H., Huenteler J., Li Z.: Stability improvement of high-pressure-ratio turbocharger centrifugal compressor by asymmetric flow control — Part I: Non-axisymmetrical flow in centrifugal compressor. J. Turbomach. 135(2013), 3, 1–9.
  • [18] McKee R.J., Edlund C.E.: Method and Apparatus for Detecting the Occurrence of Surge in a Centrifugal Compressor. Google Patents, 2006.
  • [19] McKee R.J., Siebenaler S.J., Deffenbaugh D.M.: Increased flexibility of turbo-compressors in natural gas transmission through direct surge control. U.S. Department of Energy Report, San Antonio 2005.
  • [20] Liśkiewicz G., Horodko L., Stickland M., Kryłłowicz W.: Identification of phenomena preceding blower surge by means of pressure spectral maps. Exp. Therm. Fluid Sci. 54(2014), 267–278.
  • [21] Garcia D., Stickland M., Liskiewicz G.: Dynamical system analysis of unstable flow phenomena in centrifugal blower. Open Eng. 5(2015), 1, 332–342.
  • [22] Sorokes J.M., Borer C.J., Koch J.M.: Investigation of the circumferential static pressure non-uniformity caused by a centrifugal compressor discharge volute. In: Proc. Int. Gas Turbine and Aeroengine Cong., 98-GT-326, 1998, 1–9, doi:10.1115/98-GT-326.
  • [23] Ansys Fluent 14.0 Theory Guide. ANSYS Inc, 2011.
  • [24] Guo Q., Chen H., Zhu X.-C.C., Du Z.-H.H., Zhao Y.: Numerical simulations of stall inside a centrifugal compressor. J. Power Energ. 221(2007), 5, 683–693.
  • [25] HuangW., Geng S., ZhuJ., ZhangH.: Numerical simulation of rotating stall in a centrifugal compressor with vaned diffuser. J. Therm. Sci. 16(2007), 2, 115–120.
  • [26] Turunen-Saaresti T., Larjola J.: Unsteady pressure field in a vaneless diffuser of a centrifugal compressor: An experimental and computational analysis. J. Therm. Sci. 13(2004), 4, 302–309.
  • [27] Liśkiewicz G., Horodko L., Stickland M., Kryłłowicz W.: Identification of phenomena preceding blower surge by means of pressure spectral maps. Exp. Therm. Fluid Sci., 54(2014), 267–278.
  • [28] Horodko L.: Detection of surge precursors in a centrifugal compressor with a wavelet method. In: Proc. 7th Eur. Conf. on Turbomachinery, Fluid Dynamics and Thermodynamics, Athenes 2007, 317–326
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-63f9e0b9-260e-4563-abc4-bef058ec2e0f
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