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Handbook of Turbomachinery Second Edition Revised - Ventech!

Handbook of Turbomachinery Second Edition Revised - Ventech!

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Figure 18 Whirl speed map: Laval–Jeffcott rotor rotatory motion.<br />

The backward synchronous critical speed is<br />

nb ¼<br />

s<br />

ffiffiffiffiffiffiffiffiffiffiffiffiffiffi<br />

kr<br />

Id þ Ip<br />

ð21bÞ<br />

For the choice when Ip ¼ 0:80Id, these two critical speeds are nf ¼<br />

21; 540 rpm and nb ¼ 7; 181 rpm.<br />

Note that Eq. (21a) is singular when Ip ¼ Id and that this equation<br />

yields an extraneous solution when Ip > Id. WhenIp ¼ Id, the disk is said to<br />

be ‘‘inertially spherical.’’ As illustrated in Fig. 18, when Ip is larger than Id,<br />

an intersection <strong>of</strong> the synchronous excitation line and the forward natural<br />

frequency line does not exist. In general, forward natural whirl speeds<br />

increase in value due to a ‘‘gyroscopic stiffening’’ <strong>of</strong> the shaft as the rotor<br />

spin-speed increases, and backward natural whirl speeds decrease due to a<br />

‘‘gyroscopic s<strong>of</strong>tening.’’ For the special case when Ip > Id, the Laval–<br />

Jeffcott rotor system ‘‘stiffens’’ such that the forward natural frequency is<br />

always larger than the rotor spin-speed. Thus, a forward critical speed does<br />

not exist for this situation. For additional information on the effects <strong>of</strong><br />

rotatory inertia and gyroscopic moments, refer to the vibrations book by<br />

Den Hartog [3].<br />

Copyright © 2003 Marcel Dekker, Inc.

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