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Effect of splitter leading edge location on performance of an automotive turbocharger compressor

Author

Listed:
  • Moussavi, S. Abolfazl
  • Hajilouy Benisi, Ali
  • Durali, Mohammad

Abstract

Design of centrifugal compressors can be accomplished using methods provided in text books and open literature. In this general approach, after determination of dimensions in meridional plane, blade profiles are designed using aerodynamic methods. Then, some blades are trimmed at the beginning to avoid inlet blockage. But there is no clear guidance on how this trimming must be performed. With this widely implemented method, splitter blades have the same profile as main ones.

Suggested Citation

  • Moussavi, S. Abolfazl & Hajilouy Benisi, Ali & Durali, Mohammad, 2017. "Effect of splitter leading edge location on performance of an automotive turbocharger compressor," Energy, Elsevier, vol. 123(C), pages 511-520.
    • Handle: RePEc:eee:energy:v:123:y:2017:i:c:p:511-520
    DOI: 10.1016/j.energy.2017.02.011
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    Citations

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    Cited by:

    1. Nima Khoshkalam & Mohammad Mojaddam & Keith R. Pullen, 2019. "Characterization of the Performance of a Turbocharger Centrifugal Compressor by Component Loss Contributions," Energies, MDPI, vol. 12(14), pages 1-21, July.
    2. Omer Faruk Atac & Jeong-Eui Yun & Taehyun Noh, 2018. "Aerodynamic Design Optimization of a Micro Radial Compressor of a Turbocharger," Energies, MDPI, vol. 11(7), pages 1-18, July.
    3. Rong Huang & Jimin Ni & Houchuan Fan & Xiuyong Shi & Qiwei Wang, 2023. "Investigating a New Method-Based Internal Joint Operation Law for Optimizing the Performance of a Turbocharger Compressor," Sustainability, MDPI, vol. 15(2), pages 1-23, January.
    4. Ekradi, Khalil & Madadi, Ali, 2020. "Performance improvement of a transonic centrifugal compressor impeller with splitter blade by three-dimensional optimization," Energy, Elsevier, vol. 201(C).
    5. Tang, Xinzi & Wang, Zhe & Xiao, Peng & Peng, Ruitao & Liu, Xiongwei, 2020. "Uncertainty quantification based optimization of centrifugal compressor impeller for aerodynamic robustness under stochastic operational conditions," Energy, Elsevier, vol. 195(C).
    6. Nakhchi, M.E. & Naung, S. Win & Rahmati, M., 2022. "Influence of blade vibrations on aerodynamic performance of axial compressor in gas turbine: Direct numerical simulation," Energy, Elsevier, vol. 242(C).

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