Blade Number Selection for a Splittered Mixed-Flow Compressor Impeller Using Improved Loss Model

Author:

Xiang Hang1,Chen Jiang1,Cheng Jinxin1,Song Xiancheng2

Affiliation:

1. School of Energy and Power Engineering , Beihang University , Beijing 100191 , China

2. Beijing Research Institute of Precise Mechatronics and Controls , Beijing 100076 , China

Abstract

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.

Publisher

Walter de Gruyter GmbH

Subject

Aerospace Engineering

Reference34 articles.

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