Brochure
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4. Pump theory
4. Pump theory
The purpose of this chapter is to describe the theoretical foundation of en-
ergy conversion in a centrifugal pump. Despite advanced calculation meth-
ods which have seen the light of day in the last couple of years, there is still
much to be learned by evaluating the pump’s performance based on funda-
mental and simple models.
When the pump operates, energy is added to the shaft in the form of me-
chanical energy. In the impeller it is converted to internal (static pressure)
and kinetic energy (velocity). The process is described through Euler’s pump
equation which is covered in this chapter. By means of velocity triangles for
the flow in the impeller in- and outlet, the pump equation can be interpreted
and a theoretical loss-free head and power consumption can be calculated.
Velocity triangles can also be used for prediction of the pump’s performance
in connection with changes of e.g. speed, impeller diameter and width.
4.1 Velocity triangles
For fluid flowing through an impeller it is possible to determine the absolute
velocity (C) as the sum of the relative velocity (W) with respect to the im-
peller, i.e. the tangential velocity of the impeller (U). These velocity vectors
are added through vector addition, forming velocity triangles at the in- and
outlet of the impeller. The relative and absolute velocity are the same in the
stationary part of the pump.
The flow in the impeller can be described by means of velocity triangles,
which state the direction and magnitude of the flow. The flow is three-di-
mensional and in order to describe it completely, it is necessary to make two
plane illustrations. The first one is the meridional plane which is an axial
cut through the pump’s centre axis, where the blade edge is mapped into
the plane, as shown in figure 4.1. Here index 1 represents the inlet and index
2 represents the outlet. As the tangential velocity is perpendicular to this
plane, only absolute velocities are present in the figure. The plane shown in
figure 4.1 contains the meridional velocity, C
m
, which runs along the channel
and is the vector sum of the axial velocity, C
a
, and the radial velocity, C
r
.
Figure 4.1: Meridional cut.
C
r
C
m
C
a
1
2