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Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

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Therefore<br />

Hence,<br />

The diffuser system<br />

Centrifugal Pumps, Fans <strong>and</strong> Compressors 237<br />

Centrifugal compressors <strong>and</strong> pumps are, in general, fitted with either a vaneless or<br />

a vaned diffuser to transform the kinetic energy at impeller outlet into static pressure.<br />

Vaneless diffusers<br />

The simplest concept <strong>of</strong> diffusion in a radial flow machine is one where the swirl<br />

velocity is reduced by an increase in radius (conservation <strong>of</strong> angular momentum) <strong>and</strong><br />

the radial velocity component is controlled by the radial flow area. From continuity,<br />

since m . = rAcr = 2prbrc r, where b is the width <strong>of</strong> passage, then<br />

(7.30)<br />

Assuming the flow is frictionless in the diffuser, the angular momentum is constant <strong>and</strong><br />

cq = cq2r2/r. Now the tangential velocity component cq is usually very much larger than<br />

the radial velocity component cr; therefore, the ratio <strong>of</strong> inlet to outlet diffuser velocities<br />

c2/c 3 is approximately r 3/r 2. Clearly, to obtain useful reductions in velocity, vaneless<br />

diffusers must be large. This may not be a disadvantage in industrial applications<br />

where weight <strong>and</strong> size may be <strong>of</strong> secondary importance compared with the cost <strong>of</strong> a<br />

vaned diffuser. A factor in favour <strong>of</strong> vaneless diffusers is the wide operating range<br />

obtainable, vaned diffusers being more sensitive to flow variation because <strong>of</strong> incidence<br />

effects.<br />

For a parallel-walled radial diffuser in incompressible flow, the continuity <strong>of</strong> mass<br />

flow equation requires that rcr is constant. Assuming that rc q remains constant, then the<br />

absolute flow angle a2 = tan -1 (c q/c r) is also constant as the fluid is diffused outwards.<br />

Under these conditions the flow path is a logarithmic spiral. The relationship between<br />

the change in the circumferential angle Dq <strong>and</strong> the radius ratio <strong>of</strong> the flow in the diffuser<br />

can be found from consideration <strong>of</strong> an element <strong>of</strong> the flow geometry shown in<br />

Figure 7.15. For an increment in radius dr we have, r dq = drtan a2 which, upon integration,<br />

gives<br />

(7.31)<br />

Values <strong>of</strong> Dq are shown in Figure 7.16 plotted against r 3/r 2 for several values <strong>of</strong> a 2. It<br />

can be readily seen that when a2 > 70°, rather long flow paths are implied, friction<br />

losses will be significant <strong>and</strong> the diffuser efficiency will be low.

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