Unbalance
of an impeller can be
a source of
vibrations. These vibrations can lead to a reduced lifetime of the
impeller, as
well as excessive noise, and possible contact to other non-moving parts
of the assembly. The vibrations will add extra stresses to all
components of the impeller and possibly other
components in the system that interact with the impeller.
An impeller or any rotating
component will
never be in perfect balance and residual unbalance will always occur.
The
question is therefore “when is the balance of an impeller
acceptable” or when
will the impeller not create any excessive vibrations due to the
residual
unbalance.
Static or dynamic
balancing
A rotating object can either be
balanced in one
or two planes. When a rotating object is balanced in one plane, it
means that
all the corrective weight is placed in the same plane. Single plane
balancing
is also referred to as static balancing. If a rotating object is
balanced in
two planes, the corrective weight is used in two planes and this type
of
balancing is called dynamic balancing. It is important to emphasise
that static
or dynamic balancing has nothing to do with the physical method being
used in
the balancing process.
According to the ISO 1940/1
standard“Mechanical
vibrations – Balance quality requirements of rigid rotors
– Part1:
Determination of permissible residual unbalance”,
the use of one correction
plan is sufficient for a disc shaped rotor.
Because of the relative narrow
axial depth compared with the overall diameter, single plane balancing
is
considered to be sufficient for an axial impeller. The standard is not
specific
as to when you need to perform a two-plane balance, however as a
guideline, a
single plane balance should be sufficient when the axial depth is less
than 20%
of the impeller diameter.
Caclulating the
permissible unbalance
Based on empirical data, the
ISO 1940/1
standard defines a balancing quality grade system. The roughest grade
applies
for equipment such as crankshafts and drives of rigidly mounted
slow marine diesel
engines with uneven numbers of cylinders. The finest grade
applies for spindles, discs, and armatures of precision grinders and gyroscopes.
Between these two is the
balancing grade G6.3
that applies for fans, i.e. our products. The standard is quite
explicit when
it comes to unbalance tolerance for an assembly (impeller and motor), as
the
complete assembly has to meet the balancing tolerance. If this cannot
be
achieved by balancing each component separately, the assembly shall be
balanced
as a unit. Therefore both the motor and the impeller have to meet G6.3
and
unbalance must not be added in the fitting of the components.
Permissibile
Unbalance
The more
mass in the impeller,
the greater the permissible residual unbalance. The permissible
residual
specific unbalance value (eper) is given by the
following formula:
Where Uper
[mm · s] is the
permissible residual unbalance and m is the rotor mass.
The relationship between the
upper limit of eper
and the maximum service speed are shown in figure 1 below.
If you have any further questions regarding any of these topics please
do not hesitate to contact Charles Burgess
Multi-Wing Australia P/L
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