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Centrifugal Pumps Design and Application 2nd ed - Val S. Lobanoff, Robert R. Ross (Butterworth-Heinemann, 1992)

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Vibration <strong>and</strong> Noise in <strong>Pumps</strong> 453<br />

Response To Unbalance<br />

The location of a pump critical spe<strong>ed</strong> is defin<strong>ed</strong> by its response to unbalance.<br />

It is important to recognize the difference between critical<br />

spe<strong>ed</strong>s excit<strong>ed</strong> by unbalance <strong>and</strong> damp<strong>ed</strong> eigenvalues that are frequently<br />

also call<strong>ed</strong> critical spe<strong>ed</strong>s [32]. Generally, the effect of damping is to<br />

raise the frequency of the critical spe<strong>ed</strong> response due to unbalance; however,<br />

the effect of damping on the damp<strong>ed</strong> eigen values is to lower the<br />

frequency. The damp<strong>ed</strong> eigenvalues are primarily us<strong>ed</strong> for evaluating the<br />

stability of the rotor system. For compressors <strong>and</strong> turbines with tilting<br />

pad bearings, the damp<strong>ed</strong> eigenvalues are usually comparable to the unbalanc<strong>ed</strong><br />

response criticals. However, in a pump with a large number of<br />

seals, the add<strong>ed</strong> damping to the system can be considerable, resulting in<br />

large differences in the unbalanc<strong>ed</strong> response critical spe<strong>ed</strong>s <strong>and</strong> the<br />

damp<strong>ed</strong> eigenvalues.<br />

Rotor unbalance response calculations are the key analysis in the design<br />

stage for determining if a pump rotor will be acceptable from a dynamics<br />

st<strong>and</strong>point. An accurate pr<strong>ed</strong>iction of rotor unbalanc<strong>ed</strong> response<br />

is difficult for centrifugal pumps because of the sensitivity to bearing <strong>and</strong><br />

seal clearances that may be at the tight or loose end of the tolerance<br />

range.<br />

Computer programs are available that can calculate the elliptical shaft<br />

orbit at any location along the length of a rotor for various types of bearings,<br />

p<strong>ed</strong>estal stiffnesses, p<strong>ed</strong>estal masses, seals, labyrinths, unbalance<br />

combinations, etc. These programs can be us<strong>ed</strong> to determine the response<br />

of the install<strong>ed</strong> rotor to unbalance <strong>and</strong> accurately pr<strong>ed</strong>ict the critical<br />

spe<strong>ed</strong>s over the entire range of variables. The actual critical spe<strong>ed</strong> locations<br />

as determin<strong>ed</strong> from response peaks caus<strong>ed</strong> by unbalance are<br />

strongly influenc<strong>ed</strong> by the following factors [33]:<br />

• bearing direct stiffness <strong>and</strong> damping values<br />

• bearing cross-coupl<strong>ed</strong> stiffness <strong>and</strong> damping values<br />

» location of the unbalance<br />

• location of measurement point<br />

• bearing support flexibility<br />

The normal unbalance us<strong>ed</strong> in the analysis would produce a force equal<br />

to 10% of the rotor weight at operating spe<strong>ed</strong>. Usually the rotor response<br />

to unbalance calculations are independently made for midspan unbal-

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