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Handbook of Turbomachinery Second Edition Revised - Ventech!

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6<br />

Fundamentals <strong>of</strong> Compressor Design<br />

INTRODUCTION<br />

Robert O. Bullock*<br />

Allied Signal Company, Phoenix, Arizona, U.S.A.<br />

Compressors raise the pressure <strong>of</strong> a gas by transferring mechanical energy<br />

from a rotating shaft to the gas. Many ingenious methods have been devised<br />

for this purpose, but the compressors discussed herein are limited to those<br />

that are similar to the axial-flow and centrifugal units illustrated in Figures<br />

1–4. Figure 1 is a cutaway photograph <strong>of</strong> a TFE 731 turb<strong>of</strong>an engine<br />

manufactured by the Allied Signal Corporation. Figure 2is adrawing <strong>of</strong> the<br />

projection <strong>of</strong> the engine on a plane through the axis <strong>of</strong> rotation. The fan is a<br />

single-stage axial compressor. A four-stage axial compressor follows, and to<br />

the right is acentrifugal compressor. Figures 3and 4illustrate atwo-stage<br />

centrifugal compressor that is part <strong>of</strong> the Allied Signal TPE 331 turboprop<br />

engine.<br />

All <strong>of</strong> these compressors have rows <strong>of</strong> blades that are mounted on<br />

rotating disks. The blades provide conservative forces that increase the<br />

angular momentum <strong>of</strong> the gases flowing between them; Euler’s turbine<br />

* Deceased<br />

Copyright © 2003 Marcel Dekker, Inc.

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