Turbine type flowmetering devices are applied worldwide
to the measurement and control of liquid products in
the industrial, chemical and petroleum marketplaces.
Significant advantages associated with the use of turbine
flowmeters, in lieu of other metering principles, make
increased future use inevitable. Newcomers to the field
of flow measurement should become familiar with fundamental
characteristics and conditions surrounding the turbine
flowmeter in order to better understand its usage. Consequently,
this article is provided as a brief guide to the operation
and application of turbine flowmeters for liquid product
measurement.
Barry Ellison
The basic construction of the turbine flowmeter incorporates
a bladed turbine rotor installed in a flow tube. The
rotor is suspended axially in the direction of flow
through the tube. The turbine flowmeter is a transducer,
which senses the momentum of the flowing stream. The
bladed rotor rotates on its axis in proportion to the
rate of the liquid flow through the tube.
TURBINE ROTATION
As the liquid product strikes the front edge of the
rotor blades, a low-pressure area is produced between
the upstream cone and the rotor hub.
The blades of the turbine rotor will tend to travel
toward this low-pressure area as a result of this pressure
differential across the blades. The pressure differential
(or pressure drop) constitutes the energy expended to
produce movement of the rotor. The initial tendency
of the rotor is to travel downstream in the form of
axial thrust. But since the rotor is restrained from
excessive downstream movement, the only resulting movement
is rotation.
Fluid flowing through the meter impacts an angular velocity
to the turbine rotor blades, which is directly proportional
to the linear velocity of the liquid. The degree of
the angular velocity or number of revolutions per minute
of the turbine rotor is determined by the angle of the
rotor blades to the flowing stream of the approach velocity.
ROTOR BALANCE
With axial thrust forcing the turbine rotor downstream,
the friction resulting from contact between the turbine
rotor and the downstream cone would cause excessive
wear if there were not some means of balancing the turbine
rotor on its axis between the upstream and the downstream
cone.
Bernoulli's Principle states that when flow velocity
decreases, the static pressure increases. Therefore,
a high-pressure area exists at the downstream side of
the turbine rotor exerting an upstream force on the
rotor. As a result, the turbine rotor is hydraulically
balanced on its axis.
SIGNAL OUTPUT
Electrical output is generated using the principle of
reluctance. A pickup coil, wrapped around a permanent
magnet, is installed on the exterior of the flow tube
or the meter body immediately adjacent to the perimeter
of the rotor (Figure 1). The magnet is the source of
the magnetic flux field that cuts through the coil.
Each blade of the turbine rotor passing in close proximity
to the pickup coil causes a deflection in the existing
magnetic field. This change in the reluctance of the
magnetic circuit generates a voltage pulse within the
pickup coil.
Each pulse generated represents a discrete amount of
volumetric throughput. Dividing the total number of
pulses generated by the specific amount of liquid product
that passed through the turbine flowmeter determines
the K-Factor. The K-Factor, expressed in pulses per
unit volume, may be used with a factoring totalizer
to provide an indication of volumetric throughput directly
in engineering units. The totalizer continuously divides
the incoming pulses by the K-Factor (or multiplies them
with the inverse of the K-Factor) to provide factored
totalization. The frequency of the pulse output, or
number of pulses per unit time, is directly proportional
to the rotational rate of the turbine rotor. Therefore,
this frequency of the pulse output is proportional to
the rate of the flow.
By dividing the pulse rate by the K-Factor, the volumetric
throughput per unit time of the rate of flow can be
determined. Frequency counters or converters are commonly
used to provide instantaneous flow rate indication.
Plotting the electrical signal output versus flow rate
provides the characteristics profile or calibration
curves for the turbine flowmeter.
Electrical output is also generated using the principle
of inductance. A pickup coil is installed on the exterior
of the flow tube immediately adjacent to the perimeter
of the turbine rotor. The magnetic source of the flux
field in this type of output is either the rotor itself
or small magnets installed in the rotor. In the case
of the rotor, the material of construction would be
nickel or some other easily magnetized flux field. The
results are identical to that of the reluctance principal.

Figure 1
ACCURACY
The accuracy of a turbine flowmeter is derived from
its output (electrical or mechanical) and is the measure
of the deviation of an indicated measurement from the
referenced standard. Turbine meter accuracy is dependent
upon several items.
The accuracy must include the error associated with
the calibration standard. In the USA, the National Institute
of Standards and Technology represents the flow standard.
Linearity is the variation of the flowmeter K-factor
from a nominal value of a point on a curve. Normally
during calibration, a value is chosen which makes linearity
fall in line with accuracy. Linearity may remain constant
during meter life although the absolute accuracy level
has changed.
Repeatability is the ability of a turbine flowmeter
to reproduce its output indefinitely under constant
operating conditions at any point over its specified
operating range.

Figure 2 (click on the image to enlarge picture)
SPECIFIC GRAVITY
The specific gravity of a liquid is the ratio of its
density to that of water at 4BC (39.2BF) and is dimensionless.
While changes in specific gravity do not affect the
average turbine meter K-factor value, the overall linear
range of the flowmeter is changed (Figure 2). The linear
range represents the minimum to the maximum flow rate
within which the linearity of the flowmeter is specified.
As stated previously, the rotor rotates due to pressure
differential across the rotor blades. Specific gravity
is one of the factors affecting this pressure differential.
As the specific gravity decreases, the pressure differential
decreases. On a fluid with a low specific gravity and
a low flow rate, the pressure differential across the
blades is very low. This leaves almost no energy for
turning the rotor. Consequently, the rotor cannot turn
in proportion to the liquid throughput and the K-factor
drops off.
Therefore, the angle of the rotor blades is changed
to help compensate for the change to a lower specific
gravity. This allows products with lower specific gravity's
to be measured accurately by the turbine flowmeter.
VISCOSITY
Viscosity if the measure of the liquid products resistance
to flow. Kinematics viscosity is the ratio of the absolute
viscosity to the specific gravity, usually expressed
in centistokes (cs), where the resistance to flow is
measured in square millimeters per second (mm2/s).
VISCOSITY EFFECTS ON RANGEABILITY
Viscosity has two different effects on the turbine flowmeter
rotor. First of all, the profile causes boundary layer
thickness to increase as viscosity increases for a fixed
volume. This means that rotor-blade shape and length
will be important in determining the K-factor since
the flow around the blade tip region changes with respect
to viscosity. This boundary layer thickness causes the
turbine flowmeter to be non-linear. Supplying a shroud
around the turbine rotor, with the shroud outer diameter
slightly smaller than the inside diameter of the flow
tube, increases the viscosity and creates a drag (resistance
to rotation). This drag offsets the non-linear effect
of the boundary layer.
The second effect of viscosity is one of viscous shear-force
change on the rotor and increased viscous drag within
the bearing. These effects act to slow the rotor while
the profile effect acts to speed the rotor. The relative
magnitude of all these forces changes the Reynolds number.
As previously indicated, some turbine flowmeter designs
introduce a device or shroud that introduces viscous
drag, which eliminates the hump that normally, occurs
in the transition region.
While linearity is affected by viscosity, repeatability
is not.
FLOW RANGE
The minimum flow rate of a turbine flowmeter becomes
a factor of viscosity versus the degree of accuracy.
As product viscosity increases, the minimum flow rate
required to maintain a specific degree of accuracy increases.
The maximum rate of flow allowable becomes a factor
of viscosity versus the pressure drop across the flowmeter.
As the product viscosity increases, the maximum flow
rate decreases in accordance with the maximum allowable
pressure drop across the flowmeter. In order to arrive
at the minimum and maximum rate of flow limits for a
particular turbine flowmeter size and application these
factors must first be determined:
· The viscosity of the product to be metered
(or maximum value of viscosity for products with varying
viscosity's at 37.8B (100BF).
· The degree of accuracy required.
· The maximum amount of pressure drop allowed
across the flowmeter.
Using an area-of-operation diagram for a particular
turbine flowmeter size and charting the factors for
viscosity accuracy and pressure drop will determine
the minimum and maximum flow rates.
Operating the flowmeter within this flow range will
meet the operating requirements unique to that application.
Technical bulletins providing area of operation for
turbine flowmeter sizes with varying viscosity fluids
can be obtained from the various meter manufacturers.
CAVITATION
Cavitation in a turbine flowmeter will take place when
the local pressures fall close to or below the vapor
pressure of the liquid product. The formation of bubbles
and their collapse or local vaporization of product
as it passes over the rotor blade surface can cause
erratic behavior in the turbine flowmeter and excessive
wear due to over speeding. Maintaining a system backpressure
of 2 times the flowmeter pressure drop plus 25 times
the product vapor pressure is sufficient to prevent
cavitation as shown by the following formula:
BP= (
P
x 2) + (VP x 1.25)
Where,
BP= Required back pressure
P=
Pressure drop at maximum flow.
VP= Absolute vapor pressure at maximum temperature.
Cavitation usually causes the rotor to speed up at
the high flow rate due to the increased flow volume
and causes the accuracy curve of the turbine flowmeter
to be adversely affected.
INSTALLATION
The term swirl is used to describe the rotational velocity
or tangential velocity component of fluid flow in a
pipe or tube. Depending on its degree and direction,
swirl will change the angle of attack between the fluid
and the turbine rotor blades, causing a different rotor
speed at a constant flow rate to non-swirling conditions
at the same flow rate. Liquid swirl and non-uniform
velocity profiles may be introduced upstream of the
turbine flowmeter by variations in piping configurations
or projections and protrusions within the piping. Swirl
may be effectively reduced or eliminated through the
use of sufficient lengths of straight pipe or a combination
of straight pipe and straightening vanes installed upstream
of the turbine flowmeter.

APPLICATIONS
Turbine flowmeters, when first introduced, were used
mainly by the aircraft industry in small sizes. Turbine
flowmeters are now used on many applications (figure
3). Reasons for this increased used are sizes up to
12", weight and size versus flow rate, extended
flow ranges, operating pressures up to 10,000 pounds
per square inch, temperature range of -450° to 1000°F
and a wide variety of construction materials including
stainless steels.
In recent years, turbine flowmeters have been competing
successfully with positive displacement flowmeters in
many applications due to the economy of installation,
low maintenance costs, weight, size and high flow rates
per comparable connection size. You must exercise caution
when making this comparison, especially on viscous products.
Following the parameters outlined previously will prevent
most misapplications of the turbine flowmeter.
When products are used in which viscosity changes with
seasonal temperature, a proving run should be done at
a time when the product temperature would be changing.
For instance, fuel oil may change 50°F in ambient
temperature between summer and winter. A change of this
magnitude would affect the flowmeter curve and directly
affect the flow range.
Increased expertise with electronics such as linearization
is permitting turbine flowmeters to be used more widely
(figure 4).
PROVING
Proving is a method of checking a measuring device against
an accepted standard to determine the accuracy and repeatability
of that measuring device. Turbine flowmeters should
be proven immediately after installation, after repair,
following removal from service (for any reason) when
changing products, when product viscosity changes, or
to chart the flow patterns of the flowmeter during a
period of time.
In general, provings should be quite frequent in the
early history of an installation. When sufficient results
have been gathered to establish meter factor versus
flow rate curves for each product, frequently proving
can taper off unless one of the aforementioned reasons
for proving occurs.

Figure 4: The turbine flowmeter position
should not adversely affect velocity or the smooth rotation
of the rotor. The rotor should decelerate and stop in
a smooth uninterrupted fashion. An abrupt sticking motion
indicates bearing failure.
METHODS
There are several different methods of proving. Volumetric
proving consists of a measured volume of fluid being
compared to a known standard, such as a seraphin can
or piston prover.
Gravimetric proving entails measuring weight of a fluid
by scale or load cell, then converting it by a known
formula.
Master-meter proving is the comparison of a test flowmeter
to another flowmeter previously calibrated in one of
the above methods.
CONCLUSION
Turbine flowmeters are becoming more prominent in the
field of liquid flow measurement. Turbine flowmeter
manufacturers continue to respond to industry interest
with improvements.