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654 Chapter 12 ■ Turbomachines<br />

F I G U R E 12.7<br />

(a) Open impeller, (b) enclosed<br />

or shrouded impeller.<br />

(Courtesy of Ingersoll-Dresser<br />

Pump Company.)<br />

Centrifugal pumps<br />

involve radially<br />

outward flows.<br />

<strong>fluid</strong> discharges directly into a volute-shaped casing. The casing shape is designed to reduce the<br />

velocity as the <strong>fluid</strong> leaves the impeller, and this decrease in kinetic energy is converted into an<br />

increase in pressure. The volute-shaped casing, with its increasing area in the direction of flow,<br />

is used to produce an essentially uniform velocity distribution as the <strong>fluid</strong> moves around the casing<br />

into the discharge opening. For large centrifugal pumps, a different design is often used in<br />

which diffuser guide vanes surround the impeller. The diffuser vanes decelerate the flow as the<br />

<strong>fluid</strong> is directed into the pump casing. This type of centrifugal pump is referred to as a diffuser<br />

pump.<br />

Impellers are generally of two types. For one configuration the blades are arranged on a hub<br />

or backing plate and are open on the other 1casing or shroud2 side. A typical open impeller is shown<br />

in Fig. 12.7a. For the second type of impeller, called an enclosed or shrouded impeller, the blades<br />

are covered on both hub and shroud ends as shown in Fig. 12.7b.<br />

Pump impellers can also be single or double suction. For the single-suction impeller the <strong>fluid</strong><br />

enters through the eye on only one side of the impeller, whereas for the double-suction impeller<br />

the <strong>fluid</strong> enters the impeller along its axis from both sides. The double-suction arrangement reduces<br />

end thrust on the shaft, and also, since the net inlet flow area is larger, inlet velocities are<br />

reduced.<br />

Pumps can be single or multistage. For a single-stage pump, only one impeller is mounted on<br />

the shaft, whereas for multistage pumps, several impellers are mounted on the same shaft. The stages<br />

operate in series, that is, the discharge from the first stage flows into the eye of the second stage, the<br />

discharge from the second stage flows into the eye of the third stage, and so on. The flowrate is the<br />

same through all stages, but each stage develops an additional pressure rise. Thus, a very large discharge<br />

pressure, or head, can be developed by a multistage pump.<br />

Centrifugal pumps come in a variety of arrangements 1open or shrouded impellers, volute<br />

or diffuser casings, single- or double-suction, single- or multistage2, but the basic operating principle<br />

remains the same. Work is done on the <strong>fluid</strong> by the rotating blades 1centrifugal action and<br />

tangential blade force acting on the <strong>fluid</strong> over a distance2, creating a large increase in kinetic energy<br />

of the <strong>fluid</strong> flowing through the impeller. This kinetic energy is converted into an increase<br />

in pressure as the <strong>fluid</strong> flows from the impeller into the casing enclosing the impeller. A simplified<br />

theory describing the behavior of the centrifugal pump was introduced in the previous section<br />

and is expanded in the following section.<br />

12.4.1 Theoretical Considerations<br />

Although flow through a pump is very complex 1unsteady and three-dimensional2, the basic theory of<br />

operation of a centrifugal pump can be developed by considering the average one-dimensional flow of<br />

the <strong>fluid</strong> as it passes between the inlet and the outlet sections of the impeller as the blades rotate. As<br />

shown in Fig. 12.8, for a typical blade passage, the absolute velocity, V 1 , of the <strong>fluid</strong> entering the passage<br />

is the vector sum of the velocity of the blade, U 1 , rotating in a circular path with angular velocity<br />

v, and the relative velocity, W 1 , within the blade passage so that V 1 W 1 U 1 . Similarly, at the<br />

exit V 2 W 2 U 2 . Note that U 1 r 1 v and U 2 r 2 v. Fluid velocities are taken to be average<br />

velocities over the inlet and exit sections of the blade passage. The relationship between the various<br />

velocities is shown graphically in Fig. 12.8.

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