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

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454 <strong>Centrifugal</strong> <strong>Pumps</strong>: <strong>Design</strong> <strong>and</strong> <strong>Application</strong><br />

ance, coupling unbalance, <strong>and</strong> moment unbalance. An unbalance equal to<br />

a force of 5 % of the rotor weight is usually appli<strong>ed</strong> at the coupling to<br />

excite the rotor. For moment unbalance, an unbalance equal to 5 % of the<br />

rotor weight is us<strong>ed</strong> at the coupling <strong>and</strong> another equal unbalance is us<strong>ed</strong><br />

out-of-phase on the impeller furthest from the coupling.<br />

The unbalance response of a pump should be analyz<strong>ed</strong> for several cases<br />

to bracket the expect<strong>ed</strong> range of critical spe<strong>ed</strong>s. The first analysis should<br />

include minimum seal <strong>and</strong> bearing clearances that represent the maximum<br />

expect<strong>ed</strong> support stiffness <strong>and</strong> therefore, the highest critical spe<strong>ed</strong>.<br />

The second analysis should consider the maximum bearing clearances<br />

<strong>and</strong> seal clearances of twice the design clearance to simulate the pump<br />

condition after long periods of service. The third analysis should simulate<br />

the worn condition with no seal effects <strong>and</strong> maximum bearing clearances<br />

that represent the overall minimum expect<strong>ed</strong> support stiffness for<br />

the rotor (lowest critical spe<strong>ed</strong>).<br />

The unbalanc<strong>ed</strong> response of the eight -stage pump with maximum bearing<br />

clearances <strong>and</strong> no seals is shown in Figure 18*18. The peak response<br />

at 1700 rpm was the minimum calculat<strong>ed</strong> critical spe<strong>ed</strong>. The unbalance<br />

was appli<strong>ed</strong> at the rotor midspan to excite the first mode. The response<br />

for the interm<strong>ed</strong>iate analysis (worn seals) is plott<strong>ed</strong> in Figure 18-19. The<br />

worn seals increas<strong>ed</strong> the pr<strong>ed</strong>ict<strong>ed</strong> response peak to approximately 1800<br />

cpni. With minimum clearances at the bearings <strong>and</strong> seals, the response<br />

was lower <strong>and</strong> the frequency increas<strong>ed</strong> to 2200 cpm, as shown in Figure<br />

18-20 (note scale changes).<br />

Shop acceptance test data was available for the eight-stage pump which<br />

was analyz<strong>ed</strong>. The calculat<strong>ed</strong> unbalanc<strong>ed</strong> response is compar<strong>ed</strong> with the<br />

measur<strong>ed</strong> vibration data from the test st<strong>and</strong> in Figure 18-21. For these<br />

calculations, maximum bearing clearance <strong>and</strong> the design values of seal<br />

clearance were us<strong>ed</strong>. Bas<strong>ed</strong> on these results, Quids' finite length method<br />

[28] provides favorable results compar<strong>ed</strong> with measur<strong>ed</strong> data. The<br />

"shape" of the response curve using Childs' seal values compares<br />

closely with the measur<strong>ed</strong> results, indicating that the damping contribution<br />

of the seals is of the right magnitude.<br />

The anticipat<strong>ed</strong> range of rotor response should be calculat<strong>ed</strong> with the<br />

range of bearing values <strong>and</strong> various combinations of unbalance. This is<br />

important because it is not possible in the design stage to know the exact<br />

install<strong>ed</strong> configuration with regard to bearings (clearance, preload) <strong>and</strong><br />

balance (location of unbalance). Usually a mechanical test will be limit<strong>ed</strong><br />

to one configuration (clearance, preload, unbalance) that may not show<br />

any problem. Changes introduc<strong>ed</strong> later by spare parts during maintenance<br />

turnarounds may change sensitive dimensions that may result in a<br />

higher response. For this reason, the vibration characteristics of some<br />

satisfactorily operating machines may change after an overhaul.

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