Influence of the Different Design Parameters to the Centrifugal Compressor Tip Clearance Loss

Author:

Turunen-Saaresti Teemu12,Jaatinen Ahti2

Affiliation:

1. e-mail:

2. e-mail:  Laboratory of Fluid Dynamics, Institute of Energy Technology, Lappeenranta University of Technology, Lappeenranta, Finland

Abstract

In this paper the effect of the tip clearance was studied with six different centrifugal compressors and data available in literature. The changes in the overall performance of the compressor stage were examined. The aim was to study the influence of the different design parameters to the tip clearance loss. It was evident by the previous studies that the sensitivity of the centrifugal compressor to the tip clearance loss varies with different designs. However, for the designer it is important to know the effect of the tip clearance loss in order to initially evaluate the quality of different designs. Analysis of the data demonstrated that no clear correlation between the sensitivity of the tip clearance loss and the specific speed, the diffusion ratio, the blade number and the ratio of blade heights exists.

Publisher

ASME International

Subject

Mechanical Engineering

Reference17 articles.

1. Small Turbomachinery Compressor and Fan Aerodynamics;ASME J. Eng. Power,1973

2. Effects of Fluid Leakage on Performance of a Centrifugal Compressor;ASME J. Eng. Power,1979

3. Experimental Performance of a 16.10-Centimeter-Tip-Diameter Sweptback Centrifugal Compressor Designed for a 6:1 Pressure Ratio;NASA, Washington, DC, Tech. Report No. X-3552,1977

4. Experimental Performance of a 13.65-Centimeter-Tip-Diameter Tandem-Bladed Sweptback Centrifugal Compressor Designed for a Pressure Ratio of 6;NASA, Washington, DC, Tech. Report No. 1091,1977

5. Thermal Tip Clearance Control for Centrifugal Compressor of an Apu Engine;ASME J. Turbomach.,1994

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