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

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Impeller <strong>Design</strong> 39<br />

The vane development <strong>and</strong> layout for the back shroud is done in the<br />

same manner, taking into account the requir<strong>ed</strong> hub vane angle. This proc<strong>ed</strong>ure<br />

should result in Point 10 reaching the estimat<strong>ed</strong> hub vane diameter.<br />

If this diameter is miss<strong>ed</strong> by more than ! /4-in., the hub vane angle<br />

should be chang<strong>ed</strong> <strong>and</strong> the layout repeat<strong>ed</strong>.<br />

Complete the vane layout by adding vane thickness (Figure 3-11) <strong>and</strong><br />

indicating a slight underfile at the vane OD <strong>and</strong> a thinning at the suction,<br />

This underfile will produce higher head <strong>and</strong> improv<strong>ed</strong> efficiency. The<br />

vane spacing location of the second vane on the end view will be determin<strong>ed</strong><br />

by the number of vanes.<br />

At this point it is necessary to check the ratio of the vane area A v to the<br />

suction eye area A e . Referring to Figure 3-12, this ratio should be 0.4 to<br />

0,6. The area A v is the area which is shad<strong>ed</strong> on the plan view. If the area<br />

ratio falls outside the limits shown, it will be necessary to change the plan<br />

view profile <strong>and</strong>/or vane thickness.<br />

<strong>Pumps</strong> in the higher specific spe<strong>ed</strong> range (N s 1,000-5,000) have suction<br />

velocity triangles that dictate different suction vane angularity at the<br />

impeller hub <strong>and</strong> impeller eye. This difference in angularity restricts<br />

vane removal from the core box, requiring a segment<strong>ed</strong> core <strong>and</strong> more<br />

costly patterns <strong>and</strong> casting. Hydraulically, it is very necessary, <strong>and</strong> we<br />

must learn to live with it. On low specific spe<strong>ed</strong>s however, (N s 500-<br />

1000) a straight vane is acceptable <strong>and</strong> will not jeopardize hydraulic performance,<br />

<strong>Design</strong> Suggestions<br />

The following points should be kept in mind when designing an impeller.<br />

• St<strong>and</strong>ardize the relationship between the number of vanes <strong>and</strong> discharge<br />

vane angle. The relationship shown in Figure 3-13 is suggest<strong>ed</strong>.<br />

Number <strong>and</strong> angularity of vanes greatly affect H-Q pump performance.<br />

St<strong>and</strong>ardization as shown will lead to more accurate perfor<br />

mance pr<strong>ed</strong>iction.<br />

• Figure 3-14 shows the effect of the number of impeller vanes in the<br />

same casing, on H-Q performance. Please note that with less vanes, the<br />

lower is the BEP head <strong>and</strong> efficiency <strong>and</strong> steeper is the shape of H-Q<br />

curve.<br />

» It is possible to maintain same BEP, Q, <strong>and</strong> efficiency by increasing b 2<br />

where number of vanes <strong>and</strong> angularity are r<strong>ed</strong>uc<strong>ed</strong> (Figure 3-15). For<br />

best efficiency, the velocity ratio between volute <strong>and</strong> impeller peripheral<br />

must be maintain<strong>ed</strong>. Similarly for the same impeller diameter,<br />

vane number <strong>and</strong> discharge angle BEP will change with change in b 2<br />

(Figure 3-16).<br />

• Avoid using even number of vanes in double volute pumps.

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