The Influence of Diffuser Channel Geometry on the Flow Range and Efficiency of a Centrifugal Compressor

Author:

Clements W W1,Artt D W1

Affiliation:

1. Department of Mechanical Engineering, The Queen's University of Belfast, Northern Ireland

Abstract

A small centrifugal compressor was tested with a series of straight wedge diffusers which had included channel divergence angles 2θ ranging from 4° to 14°. Diffusers employing sidewall divergence were also tested. Detailed pressure measurements were made with all of the diffusers. A channel divergence angle of 12° was found to be optimum since increasing the divergence angle beyond 12° produced no efficiency improvements but reduced the flow range of the compressor. Channels employing sidewall divergence produced almost identical efficiency and flow range to channels of the same area ratio without sidewall divergence

Publisher

SAGE Publications

Subject

General Engineering

Reference10 articles.

1. Fisher F. B. Development of vaned diffuser compressors for heavy duty diesel engine turbochargers. IMechE conference on Turbocharging and turbochargers, 1986, pp 21–30 (Mechanical Engineering Publications, London).

2. Straight Channel Diffuser Performance at High Inlet Mach Numbers

3. Performance and Design of Straight, Two-Dimensional Diffusers

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