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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> 451<br />

Figure 18-16. Eight-stage pump seat geometries <strong>and</strong> fluid properties.<br />

Table 18-2<br />

Summary of Seal Coefficients<br />

Stiffness<br />

Damping<br />

Principal Cross-Coupl<strong>ed</strong> Principal Cross-Coupl<strong>ed</strong><br />

Seal Type K-lb/in K-lb/in C-lb sec/in C-lb sec/in<br />

Neck-Ring 13,400 4900 23 0<br />

Int-Stg Bush -8 370 3 0<br />

Balance Piston -271,000 627,000 25,000 3000<br />

the first mode without altering the mode shape significantly. For an assum<strong>ed</strong><br />

bearing stiffness of 500,000 lb/in., the first, second, <strong>and</strong> third<br />

critical spe<strong>ed</strong>s from Figure 18-15 are 2570, 7120, <strong>and</strong> 8830 cpm.<br />

Evaluation of Critical Spe<strong>ed</strong> Calculations. To summarize, in the evaluation<br />

of the adequacy of the rotor from the critical spe<strong>ed</strong> map <strong>and</strong> the<br />

mode shapes, the following items should be examin<strong>ed</strong> [18]:<br />

• The proximity of the critical spe<strong>ed</strong> to running spe<strong>ed</strong> or spe<strong>ed</strong> range,<br />

The undamp<strong>ed</strong> lateral critical spe<strong>ed</strong>s should not coincide with the running<br />

spe<strong>ed</strong>. Various codes [7] address the allowable margin between<br />

lateral critical spe<strong>ed</strong>s <strong>and</strong> exciting frequencies. To determine if the actual<br />

critical spe<strong>ed</strong> will cause excessive vibrations, a rotor response to<br />

unbalance analysis should be perform<strong>ed</strong>.

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