Centrifugal Pumps Design and Application 2nd ed - Val S. Lobanoff, Robert R. Ross (Butterworth-Heinemann, 1992)
High Speed Pumps 179 some portion of the exit flow path; for example, plugging some of the diffiiser passages in a vaned diffuser. This, of course, results in impeller passages that are oversized for the lower flow rates according to conventional design practice, but in fact can produce efficiencies superior to those attainable with the very narrow passages that would result in EE, design procedures. The term partial emission (P.E.) arose to describe such pump geometry, apparently coined by Balje. The Barske pump is correctly classified as a partial emission type, since the emission throat area is much smaller than the impeller emission area. More to the point, net through-flow in the Barske pump can occur only in a path extending generally from the inlet eye to the vicinity of the emission throat. This is true for the simple reason that the remainder of the case cavity is concentric with the impeller and is filled with incompressible fluid, precluding any possibility of a radial flow component. High circumferential fluid velocities exist in the forced vortex created by the impeller, which are superimposed on the through-flow stream extending from eye to throat. Through-flow is then in essence a fluid migration, where a given element of fluid makes a number of circuits within the forced vortex and moves to successively higher orbits in the eye-tothroat flow region. Alternatively, the Barske pump can be referred to generically and geometrically as a concentric bowl P.E. pump or simply a concentric bowl pump. This is convenient for easier differentiation of the original pump type from its evolutionary offshoots to be described later. Partial Emission Formulae Use of tall, radial-bladed impellers in P.E. pumps results in flow conditions that must be described as disorderly. No attempt is made to match inlet geometry to the flow streamlines. Very low mean radial flow velocities combined with high tip speeds reduce the discharge vector diagram to essentially the tangential tip speed vector, U2. Calculation procedures for P.E. pumps then are based on simple algebraic expressions involving impeller tip speed rather than on the vector diagrams used in EE. design. Barske starts with the assumption that the fluid within the case rotates as a solid body or forced vortex, and neglects the negligibly low radial component, resulting in a theoretical head of: The first term represents the vortex or static head and the second term represents the velocity head or dynamic head. Even within the Barske
180 Centrifugal Pumps: Design and Application paper, question arose as to whether inclusion of the Ui 2 /2g term in the static head expression recognizing the blade inlet diameter is appropriate. Low through flow and a strong forced vortex might well combine to extend rotation to the impeller center!ine, i.e., might introduce prerotation of inlet flow. Measurements indicating that static pressure at the tip is close to u 2 2 /2g reinforce this view. Also, inlet prerotation is indicated by quite respectable suction performance despite radial blade inlet geometry. Thus, the theoretical head normally used in practice simplifies to When the subscript is dropped, u is taken to indicate the impeller tip speed. Actual head for P.E. pumps is then stated as: To further understand the workings of the RE. pump, a somewhat simplistic exercise involving a mixture of theory and experience is put forth to establish how actual head is generated. As has been indicated, tall blade geometry produces a strong forced vortex resulting in a static head coefficient near unity, so the actual static head produced by the impeller is simply u 2 /2g. Tests have shown that diffusion efficiency is nearly flat through much of the flow range, so we state that *? d = .8. Diffusion recovery potential is in accordance with the diffuser area ratio And finally, the P.E. flow coefficient is in the vicinity of 0 = .8. So actual head generation may be written Say, then, that the diffuser terminates in two throat diameters, i.e., has an area ratio of 4, so the actual head should be
- Page 144 and 145: Vertical Pumps 129 Condensate and H
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- Page 218 and 219: High Speed Pumps 203 nal bearings a
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180 <strong>Centrifugal</strong> <strong>Pumps</strong>: <strong>Design</strong> <strong>and</strong> <strong>Application</strong><br />
paper, question arose as to whether inclusion of the Ui 2 /2g term in the<br />
static head expression recognizing the blade inlet diameter is appropriate.<br />
Low through flow <strong>and</strong> a strong forc<strong>ed</strong> vortex might well combine to extend<br />
rotation to the impeller center!ine, i.e., might introduce prerotation<br />
of inlet flow. Measurements indicating that static pressure at the tip is<br />
close to u 2 2 /2g reinforce this view. Also, inlet prerotation is indicat<strong>ed</strong> by<br />
quite respectable suction performance despite radial blade inlet geometry.<br />
Thus, the theoretical head normally us<strong>ed</strong> in practice simplifies to<br />
When the subscript is dropp<strong>ed</strong>, u is taken to indicate the impeller tip<br />
spe<strong>ed</strong>. Actual head for P.E. pumps is then stat<strong>ed</strong> as:<br />
To further underst<strong>and</strong> the workings of the RE. pump, a somewhat simplistic<br />
exercise involving a mixture of theory <strong>and</strong> experience is put forth<br />
to establish how actual head is generat<strong>ed</strong>. As has been indicat<strong>ed</strong>, tall<br />
blade geometry produces a strong forc<strong>ed</strong> vortex resulting in a static head<br />
coefficient near unity, so the actual static head produc<strong>ed</strong> by the impeller<br />
is simply u 2 /2g. Tests have shown that diffusion efficiency is nearly flat<br />
through much of the flow range, so we state that *? d = .8. Diffusion recovery<br />
potential is in accordance with the diffuser area ratio<br />
And finally, the P.E. flow coefficient is in the vicinity of 0 = .8. So actual<br />
head generation may be written<br />
Say, then, that the diffuser terminates in two throat diameters, i.e., has an<br />
area ratio of 4, so the actual head should be