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Handbook of Turbomachinery Second Edition Revised - Ventech!

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tests. One should take pains to provide compressors with uniform flow rates<br />

and properties at the inlet during these tests.<br />

If compressor specifications require it to operate with gradients in the<br />

flow at the inlet, this ability can be verified by separate tests. Usually,<br />

specified deviations from uniform flow can be established with the use <strong>of</strong><br />

overlapping screens upstream <strong>of</strong> the inlet. Under some conditions, however,<br />

ingenuity is required to effect suitable tests.<br />

Instrumentation<br />

The object <strong>of</strong> overall tests is to determine how the rotating speed and flow<br />

rate affect the pressure ratio, the temperature rise, and the position <strong>of</strong> the<br />

surge line. A number <strong>of</strong> instruments are available for sensing and measuring<br />

rotating speed, flow rate, pressures, temperatures, and velocities, as well as<br />

variations <strong>of</strong> the last four items with time. Torque measurements are useful<br />

for confirming the amount <strong>of</strong> energy added by the rotors: the effect <strong>of</strong> any<br />

backflow over rotor blade tips is then properly identified as an increase in<br />

entropy instead <strong>of</strong> a transfer <strong>of</strong> mechanical energy.<br />

The location <strong>of</strong> the sensing elements deserves careful study. Figure 18<br />

illustrates a typical problem. This figure shows how the total pressure, as<br />

measured behind the last blade row <strong>of</strong> a compressor, can vary throughout<br />

the annulus. This result was observed even though uniform flow was<br />

presented to the compressor inlet. Measurements <strong>of</strong> total temperature <strong>of</strong>ten<br />

exhibit similar trends. Experience shows that this type <strong>of</strong> distribution can<br />

change with flow rate and speed. The section on energy degradation noted<br />

how this flow is subsequently mixed as it moves downstream. The mass flow<br />

rate, the power, and the momentum <strong>of</strong> the gas are preserved during mixing,<br />

while the available total pressure is reduced. Many data points can be<br />

required to obtain the information necessary to accurately evaluate the<br />

available total pressure or the true total temperature.<br />

Whenever possible, the data should be taken far enough downstream<br />

so that the flow is sufficiently uniform that the effects <strong>of</strong> subsequent mixing<br />

can be ignored. In this case the data at the measuring points can be weighted<br />

either by the local mass flow rate or by volume flow rate. The result is<br />

practically the same.<br />

When gradients in flow are inevitable at the measuring station, some<br />

method must be used to get meaningful averages. Some measure <strong>of</strong> the<br />

statistical variance is also required. Previous discussions have demonstrated<br />

that both radial and circumferential gradients in pressure may have been the<br />

result <strong>of</strong> the design and inlet conditions. They are not random in a statistical<br />

sense. The method <strong>of</strong> averaging must recognize this situation, and those<br />

Copyright © 2003 Marcel Dekker, Inc.

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