International Journal of Fluid Mechanics & Thermal Sciences

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The Development of an Integrally Geared Centrifugal Compressor

Received: 26 September 2018    Accepted: 08 April 2019    Published: 23 May 2019
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Abstract

Integrally geared centrifugal compressors have been widely used in industry especially. Reliable design, good performance, low noise, no resonant frequencies in the operating range and cost effective machining and casting parts are the goals of the design. Computational Fluid Dynamics (CFD) tools have been widely used to optimize the impeller, diffuser and volute designs. Many design considerations are useful for compressor preliminary parameter selections and compressor package designs. In this paper, the detailed development and design of a integrally geared centrifugal compressor are discussed. Some initial design considerations for compressor configureuration, power distribution for each stage, and possible field application issues are discussed in details. The aerodynamic and structural optimization using CFD and Finite Element Analysis (FEA) are performed to obtain a high efficiency and wide operating range compressor with robust operation. The new compressor development process addressed in this paper provides the basic design guidance for future new integrally geared compressor development.

DOI 10.11648/j.ijfmts.20190501.11
Published in International Journal of Fluid Mechanics & Thermal Sciences (Volume 5, Issue 1, March 2019)
Page(s) 1-9
Creative Commons

This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.

Copyright

Copyright © The Author(s), 2024. Published by Science Publishing Group

Keywords

Centrifugal Compressor, Compressor Design Consideration, CFD

References
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[2] C. Xu, M. Muller, The design and development of a centrifugal compressor volute, International journal of rotating machinery 2006.
[3] C. Xu, R. S. Amano, Empirical Design Considerations for Industrial Centrifugal Compressors, International Journal of Rotating Machinery, 2012 (2012) 1-16.
[4] C. Xu, R. S., Development of a Low Flow Coefficient Single Stage Centrifugal Compressor, International Journal for Computational Methods in Engineering Science and Mechanics, 10 (2009) 282 – 289.
[5] C. Xu, R. S. Amano, 2009, The Development of a Centrifugal Compressor Impeller, International Journal for Computational Methods in Engineering Science and Mechanics, 10 (2009) 290 – 301.
[6] C. Xu, R. S. Amano, On the Development of Turbomachine Blade Aerodynamic Design System, International Journal for Computational Methods in Engineering Science and Mechanics, 10 (2009) 186-196.
[7] C. Xu, R. S. Amano, Computational Analysis of Scroll Tongue Shape to Compressor Performance by Using Different Turbulence Models, International Journal for Computational Methods in Engineering Science and Mech, 11 (2010) 85-99.
[8] C. Xu, R. S. Amano, Study of the flow in centrifugal compressor, int. J. of Fluid Machinery and System, 3 (2010) 260-270.
[9] Xu, C., Impeller for a centrifugal compressor, US Patent. US 7563074 B2 (2005). https://www.google.com/patents/US7563074.
[10] W. F. Castle, Air separation and liquefaction: Recent developments and prospects for the beginning of the new millennium," International Journal of Refrigeration. 25(2002) 158–172.
[11] C. Xu, R. S. Amano, Effects of Asymmetric Radial Clearance on Performance of a Centrifugal Compressor, ASME Journal Energy Resource Technology, 140 (2017) 052003-0520016, doi:10.1115/1.4038387.
[12] C. Xu, R. S. Amano, Centrifugal Compressor Performance Improvements Through Impeller Splitter Location, ASME Journal Energy Resource Technology 140(2017), 051201-0512016, doi: 10.1115/1.4037813.
[13] C. Xu, R. S. Amano, computational Analysis of Scroll Tongue Shape to Compressor Performance by Using Different Turbulence Models, International Journal for Computational Methods in Engineering Science and Mechanics, 11(2010), 85-99.
[14] C. Xu, R. S. Amano, Computational Analysis of Swept Compressor Rotor Blades, International Journal for Computational Methods in Engineering Science and Mechanics, 9 (2008) 374–382.
[15] Fradin, C., Investigation of the Three Dimensional Flow near the Exit of Two Backswept Transonic Centrifugal Impellers, Proc. of the Eighth International Symposium in Air Breathing Engines, (1987) 149 -155.
[16] C. Xu, R. S. Amano, Centrifugal compressor design impacts: lean and meridional shape, GT2013-9411, (2013).
[17] C. Xu, R. S. Amano, On the Development of Turbine Blade Aerodynamic Design System, 2001-GT-0443 (2001).
[18] C. Xu, R. S. Amano, Meridional considerations of the centrifugal compressor development, International Journal of Rotating Machinery, (2012), 1-11, doi:10.1155/2012/518381.
[19] C. Xu, R. S. Amano, Performance impacts of centrifugal compressor splitter location, GT2016-56017, (2014).
[20] C. Xu, R. S. Amano, Aerodynamic and structure considerations in centrifugal compressor design-blade lean effects, GT2012-68027 (2012).
[21] F. J. Wiesner, A review of slip factors for centrifugal impellers, ASME J. of Eng for Power, 89 (1969), 558-572.
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Author Information
  • Department of Mechanical and Electrical Engineering, Central South University of Forestry and Technology, Changsha, China; Department of Mechanical Engineering, University of Wisconsin, Milwaukee, USA

  • Department of Mechanical and Electrical Engineering, Central South University of Forestry and Technology, Changsha, China

  • Department of Mechanical and Electrical Engineering, Central South University of Forestry and Technology, Changsha, China

  • Department of Mechanical and Electrical Engineering, Central South University of Forestry and Technology, Changsha, China

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  • APA Style

    Cheng Xu, Hanqian Yang, Yandan Jiang, Zhongwei Yi. (2019). The Development of an Integrally Geared Centrifugal Compressor. International Journal of Fluid Mechanics & Thermal Sciences, 5(1), 1-9. https://doi.org/10.11648/j.ijfmts.20190501.11

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    ACS Style

    Cheng Xu; Hanqian Yang; Yandan Jiang; Zhongwei Yi. The Development of an Integrally Geared Centrifugal Compressor. Int. J. Fluid Mech. Therm. Sci. 2019, 5(1), 1-9. doi: 10.11648/j.ijfmts.20190501.11

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    AMA Style

    Cheng Xu, Hanqian Yang, Yandan Jiang, Zhongwei Yi. The Development of an Integrally Geared Centrifugal Compressor. Int J Fluid Mech Therm Sci. 2019;5(1):1-9. doi: 10.11648/j.ijfmts.20190501.11

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  • @article{10.11648/j.ijfmts.20190501.11,
      author = {Cheng Xu and Hanqian Yang and Yandan Jiang and Zhongwei Yi},
      title = {The Development of an Integrally Geared Centrifugal Compressor},
      journal = {International Journal of Fluid Mechanics & Thermal Sciences},
      volume = {5},
      number = {1},
      pages = {1-9},
      doi = {10.11648/j.ijfmts.20190501.11},
      url = {https://doi.org/10.11648/j.ijfmts.20190501.11},
      eprint = {https://download.sciencepg.com/pdf/10.11648.j.ijfmts.20190501.11},
      abstract = {Integrally geared centrifugal compressors have been widely used in industry especially. Reliable design, good performance, low noise, no resonant frequencies in the operating range and cost effective machining and casting parts are the goals of the design. Computational Fluid Dynamics (CFD) tools have been widely used to optimize the impeller, diffuser and volute designs. Many design considerations are useful for compressor preliminary parameter selections and compressor package designs. In this paper, the detailed development and design of a integrally geared centrifugal compressor are discussed. Some initial design considerations for compressor configureuration, power distribution for each stage, and possible field application issues are discussed in details. The aerodynamic and structural optimization using CFD and Finite Element Analysis (FEA) are performed to obtain a high efficiency and wide operating range compressor with robust operation. The new compressor development process addressed in this paper provides the basic design guidance for future new integrally geared compressor development.},
     year = {2019}
    }
    

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    T1  - The Development of an Integrally Geared Centrifugal Compressor
    AU  - Cheng Xu
    AU  - Hanqian Yang
    AU  - Yandan Jiang
    AU  - Zhongwei Yi
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    DO  - 10.11648/j.ijfmts.20190501.11
    T2  - International Journal of Fluid Mechanics & Thermal Sciences
    JF  - International Journal of Fluid Mechanics & Thermal Sciences
    JO  - International Journal of Fluid Mechanics & Thermal Sciences
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    EP  - 9
    PB  - Science Publishing Group
    SN  - 2469-8113
    UR  - https://doi.org/10.11648/j.ijfmts.20190501.11
    AB  - Integrally geared centrifugal compressors have been widely used in industry especially. Reliable design, good performance, low noise, no resonant frequencies in the operating range and cost effective machining and casting parts are the goals of the design. Computational Fluid Dynamics (CFD) tools have been widely used to optimize the impeller, diffuser and volute designs. Many design considerations are useful for compressor preliminary parameter selections and compressor package designs. In this paper, the detailed development and design of a integrally geared centrifugal compressor are discussed. Some initial design considerations for compressor configureuration, power distribution for each stage, and possible field application issues are discussed in details. The aerodynamic and structural optimization using CFD and Finite Element Analysis (FEA) are performed to obtain a high efficiency and wide operating range compressor with robust operation. The new compressor development process addressed in this paper provides the basic design guidance for future new integrally geared compressor development.
    VL  - 5
    IS  - 1
    ER  - 

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