Elementary Theory of Centrifugal Pump
2nd Lecture
Elementary Theory of Centrifugal Pump
At any point with in the blade passages, the
fluid velocity will in general have three
components:
Radial
Tangential
Axial
The velocity may then be written as a function
of the three components:
V = (r, , z)
Elementary Theory of Centrifugal Pump
contd
Elementary Theory of Centrifugal Pump
contd
Elementary Theory of Centrifugal Pump
contd
From assumptions 1 & 2, the velocity
becomes a function of radius only i.e.
V = (r)
Energy transferred will be determined by
velocity triangle drawn at the inlet and
outlet.
Elementary Theory of Centrifugal Pump
contd
Refer to velocity triangle figure, the blades
are curved between the inlet radius r1 and
outlet radius r2. A particle of fluid moving
along the broken curve is shown. Let:
1 and 2 be the angle subtended by the
blade at inlet and outlet, measured from
the tangent to the inlet and outlet radius.
Elementary Theory of Centrifugal Pump
contd
C1 and C2 is the absolute velocity of fluid
entering at the eye of the impeller and at
exit respectively.
U1 and U2 are tangential velocity of the
blade tip, can be denoted by r1 and r2,
where is the angular velocity of the
impeller
Elementary Theory of Centrifugal Pump
contd
1 and 2 are the angles between the
absolute velocity C1 and C2, and tangential
velocity U1 and U2.
It is seen that the blade angles at inlet and
outlet (1 and 2) are not equal to their
respective relative flow angles (1 and 2).
This affects the pump performance and will
be discussed in a subsequent section. For
this case we assume that 1 and 2 are equal
to 1 and 2.
Elementary Theory of Centrifugal Pump
contd
All of the turbomachines involve the rotation of an
impeller or a rotor about a central axis, it is appropriate
to discuss their performance in terms of torque and
angular momentum.
If the shaft torque (the torque that the shaft applies to
the rotor) and the rotation of the rotor are in the same
direction, energy is transferred from the shaft to the
rotor and from the rotor to the fluidthe machine is a
pump.
Elementary Theory of Centrifugal Pump
contd
Conversely, if the torque exerted by the shaft on the
rotor is opposite to the direction of rotation, the energy
transfer is from the fluid to the rotora turbine.
The amount of shaft torque (and, hence, shaft work)
can be obtained from the moment-of-momentum
equation i.e.
Elementary Theory of Centrifugal Pump
contd
For steady flow, the term
Therefore, the moment of momentum equation
becomes
Elementary Theory of Centrifugal Pump
contd
From velocity triangle figure, the sum of all torque
acting on the system is equal to the rate of change of
angular momentum, therefore,
= (r2Cx2 r1Cx1 )
This equation is often called the Euler turbomachine
equation.
Shaft torque is directly proportional to the mass flow
rate and it also depends on the tangential component
of the absolute velocity, Cx.
Elementary Theory of Centrifugal Pump
contd
For a rotating shaft, the power transferred
is given by
For a machine revolving at an angular velocity of
=U/r
after simplifying, the power transferred becomes
=
Elementary Theory of Centrifugal Pump
contd
= QE
hence,
QE =
E=
/ Q
Where
= g &
= Q , then
This is known as Euler head, or theoretical head some times
ideal head developed by the impeller only.
Questions?
Questions?