Page 213 - Centrifugal Pumps Design and Application
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High Speed Pumps      187


          As an aside, pump users should be aware that overly conservative
        statements of NPSHA in an application can work to their disadvantage.
        The pump manufacturer must meet the stated NPSHA, so understated
        suction conditions can force the design toward lower speed or more and
        larger stages, which can result in an efficiency penalty or higher initial
        cost.

        Inducers

          Need to improve suction performance becomes quickly apparent in the
        move toward exploitation of high speed advantage. Inducer development
        began more than 50 years ago to provide this improvement. An inducer is
        basically a high specific speed, axial flow, pumping device roughly in the
        range of N s = 4,000 to 9,000 that is series mounted preceding a radial
        stage to provide overall system suction advantage. Inducers are charac-
        terized by relatively few blades, shallow inlet blade angles, and generally
        sophisticated hydraulic design.
          The inducer must put up enough head to satisfy the needs of the radial
        impeller stage but in itself has a suction level requirement that establishes
        a new lower NPSHR for the system. Inducers are an important element
        in high speed pump design, and so have been and continue to be the sub-
       ject of considerable interest and developmental work. Inducer design
        should be such that maximum suction performance is achieved, and such
        that cavitation erosion in the inducer itself is avoided in long-term opera-
       tion.
         Inducer performance is generally taken as the suction specific speed
       which corresponds to 3% pump head depression as NPSH is decreased.
       Theory exists establishing optimum suction performance in an expres-
       sion known as the Brumfield criterion. A form of the Brumfield criterion
       developed in a comprehensive document on inducer design developed by
       NASA is as follows:






       Where 4> is the inlet flow coefficient or the ratio of meridianal flow ve-
       locity to inducer tip speed:





         A plot of the Brumfield criterion is shown in Figure 11-4. It should be
       emphasized that this expression is theoretical but tempered by practical
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