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Handbook of Turbomachinery Second Edition Revised - Ventech!

Handbook of Turbomachinery Second Edition Revised - Ventech!

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assembly ‘‘straddles’’ the two bearing supports and is <strong>of</strong>ten referred to as a<br />

straddle-mount rotor. The rotor consists <strong>of</strong> a single solid steel shaft<br />

[r ¼ 7,832 kg/m 3 (0.283 lbm/in. 3 ), E ¼ 200 GPa (29 ? 10 6 lbf/in. 2 ), G ¼ 77 GPa<br />

(11.17 ? 10 6 lbf/in. 2 )] <strong>of</strong> length equal to 30 cm (11.81 in.) and diameter equal<br />

to 5 cm (1.97 in.). Three rigid disks <strong>of</strong> equal size [m ¼ 3.3 kg (7.28 lbm),<br />

Id ¼ 0.006 kg-m 2<br />

(20.50 lbm-in. 2 ), Ip ¼ 0.011 kg-m 2<br />

(37.59 lbm-in. 2 )] are<br />

attached to the shaft—one nominally at each end and one at the center <strong>of</strong><br />

the shaft. The isotropic bearings each have a stiffness k ¼ 10 MN/m<br />

(57,100 lbf/in.) and viscous damping coefficient c ¼ 1.0 kN-s/m (5.71 lbf-s/<br />

in.).<br />

A graph <strong>of</strong> the natural frequencies <strong>of</strong> whirl versus the rotor spin-speed<br />

(whirl speed map) is presented in Fig. 26. The first forward and first<br />

backward whirl speeds are nearly identical; thus, their values appear<br />

essentially as a single line on the graph. These modes are nearly cylindrical<br />

(i.e., small rotatory motion <strong>of</strong> the disks) and, as a result, the gyroscopic<br />

effects are negligible, providing essentially constant values for the whirl<br />

speeds as the rotor spin-speed changes. The second and third forward and<br />

Figure 26 Whirl speed map: straddle-mount rotor.<br />

Copyright © 2003 Marcel Dekker, Inc.

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