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RESEARCH PAPERS

A Consideration Concerning Stall and Surge Limitations Within Centrifugal Compressors

[+] Author and Article Information
Hideaki Kosuge, Takane Ito, Keiichi Nakanishi

Engine Research Laboratory, Central Engineering Laboratories, Nissan Motor Co., Ltd., 1 Natsushima-cho, Yokosuka 237, Japan

J. Eng. Power 104(4), 782-787 (Oct 01, 1982) (6 pages) doi:10.1115/1.3227344 History: Received November 23, 1981; Online September 28, 2009

Abstract

In order to understand the characteristics of an impeller independently, it is necessary that the impeller is tested without a diffuser. Using this method, the surge may be caused either by the inducer stall or impeller stall. Two types of impellers, with different inducer blade-to-blade shape, were employed to investigate the critical condition of stall and surge. Employing a one-dimensional-flow analysis within the impeller, various parameters for stall and surge were investigated. In this study, the relative velocity reduction between the inlet and throat of the inducer, and between the inlet and exit of the impeller were examined in comparison with the inducer throat Mach number.

Copyright © 1982 by ASME
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