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Handbook of Turbomachinery Second Edition Revised - Ventech!

Handbook of Turbomachinery Second Edition Revised - Ventech!

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this graph is quite simple; however, it is presented here to introduce the<br />

concept as a forerunner <strong>of</strong> whirl speed maps for more complicated systems.<br />

For the case <strong>of</strong> a Laval–Jeffcott rotor in translation only, two natural<br />

frequencies <strong>of</strong> whirl exist. The first is a forward whirl (denoted as 1f) with<br />

natural whirl frequency, ot, and the second is a backward whirl (denoted as<br />

1b) at the frequency, ot. These natural frequencies are not a function <strong>of</strong><br />

the rotor spin-speed since the natural motion <strong>of</strong> the rigid disk is pure<br />

translation. Thus, gyroscopic moments are not present for this simple<br />

translational model.<br />

One option is to graph the positive and negative natural whirl<br />

frequencies as a function <strong>of</strong> the spin-speed including the entire range <strong>of</strong><br />

positive and negative spin-speeds (i.e., a four-quadrant map). This graph is<br />

illustrated in Fig. 10(a) for the Laval–Jeffcott rotor. When the rotor is<br />

defined as having a positive spin-speed, a positive whirl frequency<br />

corresponds to a forward mode and a negative whirl frequency corresponds<br />

to a backward mode. When the rotor is defined as having a negative spinspeed,<br />

a positive whirl frequency corresponds to a backward mode and a<br />

negative whirl frequency corresponds to a forward mode. Recall: a forward<br />

mode is simply defined as a whirling motion in the same sense as the spin<br />

while a backward mode is in the opposite sense.<br />

Because <strong>of</strong> the polar symmetry <strong>of</strong> the four-quadrant graph, it is<br />

common practice to present a whirl speed map as a single-quadrant graph<br />

associated with a positive spin-speed and include both the positive and<br />

negative whirl frequencies in the first quadrant. Quite <strong>of</strong>ten, different line<br />

types are used to distinguish the positive (e.g., solid) and negative (e.g.,<br />

dashed) whirl frequencies. A single-quadrant whirl speed map for the Laval–<br />

Jeffcott rotor is illustrated in Fig. 10(b). For this simple system, the positive<br />

and negative whirl frequencies have the same absolute value and are<br />

therefore coincident on the graph.<br />

It is common practice to include an excitation frequency line, e.g.,<br />

oexc ¼ rO, on whirl speed maps. This line indicates an excitation frequency<br />

that is a multiple, r, <strong>of</strong> the rotor spin-speed, O. The line shown in Fig. 10(a)<br />

and (b) corresponds to r ¼ 1 and indicates an excitation frequency that is<br />

synchronous with the rotor spin-speed. This excitation is generally <strong>of</strong><br />

interest because rotating unbalance is always present in a rotor system, and<br />

the associated excitation is synchronous with the rotor spin-speed, i.e.,<br />

r ¼ 1. An intersection <strong>of</strong> the excitation frequency line with a whirl speed line<br />

identifies a ‘‘critical speed’’ or rotor spin-speed, n, associated with a<br />

resonance condition. For the Laval–Jeffcott rotor, only one forward critical<br />

speed exists for synchronous spin-speed excitation, with a value <strong>of</strong> nf ¼ ot.<br />

A second type <strong>of</strong> graph that is <strong>of</strong>ten used by designers to assist in<br />

making design parameter decisions is called a ‘‘critical speed map.’’ This<br />

Copyright © 2003 Marcel Dekker, Inc.

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