An Efficient Procedure for Designing Various Series of Centrifugal Compressor Impellers

Chun Wei Kong, Yueh Heng Li, Wen Lih Chen

研究成果: Article

摘要

In this study, a new integrated procedure was developed to design centrifugal compressor impellers. It can provide robust guidelines for designers in a short period of time. The procedure uses an in-house program - IMPELLER 1D DESIGN and commercial software - BladeGen and ANSYS. By simply selecting a set of input parameters, a series of impellers for different performance requirements can be generated by this integrated procedure. The procedure was used to design two micro centrifugal compressor impellers with pressure ratio of 1.2. The performance of these two impellers was evaluated by experiment and CFD simulation, and the results confirm that both impellers can meet their designed performance requirements, thus validating the correctness of the current design procedure.

原文English
頁(從 - 到)237-248
頁數12
期刊Journal of Aeronautics, Astronautics and Aviation
51
發行號3
DOIs
出版狀態Published - 2019 九月 1

    指紋

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

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