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Handbook of Turbomachinery Second Edition Revised - Ventech!

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Figure 34 Cross-section view <strong>of</strong> three turbine stages.<br />

together, or cylindrical ‘‘wires’’ or rods inserted through a hole (usually in a<br />

forged boss) in each blade foil [32, 33].<br />

In order to add mechanical damping, some wire or rod-type lashing<br />

wires are left loose in their holes, and there are also some shroud-type<br />

connections that merely abut each other and are not permanently attached.<br />

Continuous connections must make some provision to accommodate<br />

thermal expansion <strong>of</strong> the connection. Shrouds and lacing wires sometimes<br />

are introduced to decrease vibratory stresses, but can act as ‘‘crud traps.’’<br />

Blades are connected at the root to the rotor or disk by several<br />

configurationsasshowninFig.32.Thebladerootsmaybe<strong>of</strong>the‘‘serrated’’<br />

or ‘‘fir-tree’’ configuration, inserted into individual axial slots in the disk or<br />

a similar serrated or T-shape, inserted into a continuous circumferential slot<br />

in the disk (this requires a special insertion gap), or may comprise one or<br />

several flat ‘‘fingers’’ fitting into circumferential slots in the disk and secured<br />

Copyright © 2003 Marcel Dekker, Inc.

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