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Handbook of Turbomachinery Second Edition Revised - Ventech!

Handbook of Turbomachinery Second Edition Revised - Ventech!

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Figure 21 Generalized Laval–Jeffcott rotor.<br />

This system is a 4-degree-<strong>of</strong>-freedom model with two translations ðu, vÞ and<br />

two rotations ðb, gÞ at the disk center. The translations at both boundary<br />

points are constrained to zero. The excitation force for this model includes<br />

both rotating unbalance and rotating disk-skew terms.<br />

The four precessional modes are circular with two <strong>of</strong> the natural<br />

modes whirling in the same direction as the rotor spin (forward modes) and<br />

two whirling in the opposite direction (backward modes). Typical first<br />

forward and second forward mode shapes are illustrated in Fig. 22 for a<br />

rotational speed <strong>of</strong> 3,000 rpm. The backward modes are similar in shape to<br />

the forward modes.<br />

The natural frequencies <strong>of</strong> whirl, and associated modes are a function <strong>of</strong><br />

the rotor spin-speed, and the system parameters. A typical whirl speed map<br />

for this system is illustrated in Fig. 23 for the following selection <strong>of</strong><br />

parameters: m ¼ 10 lbm (4.5359 kg), Id ¼ 90 lbm-in. 2 (0.0263 kg-m 2 ), Ip ¼ 0.5 Id,<br />

E ¼ 30 ? 10 6 lbf/in. 2<br />

(206.84 GPa), r ¼ 0.5 in. (1.27 cm), and L ¼ 12 in.<br />

(30.48 cm). The shaft mass is neglected in this example system. The<br />

translational and rotational coordinates are statically coupled for this system.<br />

As a result, all natural modes <strong>of</strong> motion are affected by the gyroscopic<br />

moments associated with the spinning <strong>of</strong> the disk.<br />

Copyright © 2003 Marcel Dekker, Inc.

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