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Handbook of Turbomachinery Second Edition Revised - Ventech!

Handbook of Turbomachinery Second Edition Revised - Ventech!

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calculate the relevant thermodynamic losses and to predict the likely<br />

magnitude <strong>of</strong> the changes in those losses will be central to such an economic<br />

analysis and will help determine which options are viable.<br />

As befits the central importance <strong>of</strong> thermodynamic losses in turbine<br />

design, maintenance, and operation, numerous references describe these<br />

contributions in great detail [11, 12].<br />

Three groups <strong>of</strong> losses can be considered: pressure drops that occur<br />

with the passage <strong>of</strong> steam through valves, piping, and exhaust between<br />

sections; turbine section losses; and individual turbine stage losses. Figure 12<br />

shows that the relative mix and magnitude <strong>of</strong> efficiency losses varies by type<br />

<strong>of</strong> stage. The figure shows the major losses for a typical 700 MW single<br />

reheat turbine.<br />

Pressure Drop Losses<br />

A rule <strong>of</strong> thumb is that every 1% pressure reduction results in a reduced heat<br />

rate <strong>of</strong> about 0.1% in a fossil unit and 0.15% in a nuclear unit [9].<br />

Figure 12 Stage and section efficiency losses for a 700-Mw single reheat turbine.<br />

Copyright © 2003 Marcel Dekker, Inc.

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