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Blade Number Selection for a Splittered Mixed-Flow Compressor Impeller Using Improved Loss Model
- Source :
- International Journal of Turbo & Jet-Engines. 39:549-564
- Publication Year :
- 2020
- Publisher :
- Walter de Gruyter GmbH, 2020.
-
Abstract
- An improved mean streamline loss model for splittered centrifugal/mixed-flow compressor impellers is presented. One-dimensional model predictions, CFD simulations and experimental results for Krain impeller are compared to confirm the model validity. A new description for the interaction between blade number and splitter blade length of a splittered mixed-flow compressor impeller with high hub/tip ratio is discussed and formulized. The optimal principal blade number and optimal splitter blade length corresponding to maximum impeller efficiency are selected by the new formulas studied. The results indicate that the improved model and new formulas have reasonable prediction effects for the impeller efficiency and the selection of blade number and splitter blade length. Blade height/pitch ratio can also be adopted as a selection reference especially for high hub/tip impellers. Effective blade number or equivalent solidity is only suitable for evaluating load capacity rather than efficiency in impeller design processes.
- Subjects :
- 020301 aerospace & aeronautics
Blade (geometry)
Aerospace Engineering
Mechanical engineering
02 engineering and technology
01 natural sciences
Energy engineering
010305 fluids & plasmas
Impeller
Mixed flow
0203 mechanical engineering
0103 physical sciences
Gas compressor
Selection (genetic algorithm)
Subjects
Details
- ISSN :
- 21910332 and 03340082
- Volume :
- 39
- Database :
- OpenAIRE
- Journal :
- International Journal of Turbo & Jet-Engines
- Accession number :
- edsair.doi...........72e92809fc3ab8b92be71aedd69a192e
- Full Text :
- https://doi.org/10.1515/tjj-2020-0008