|
|
A finite element model
of the propulsion shaft, up to the output shaft of the gearbox, was
constructed. The model is based on dimensions as given in relevant
drawings.
For the stiffness of
the support in the rubber bearing, the values for static and dynamic
stiffness were supplied by the manufacturer of the bearings, and are as
follows:
|
Bearing
position |
Static
stiffness |
Dynamic
stiffness |
|
Middle |
1.4E7
N/m |
5.6E4
N/m |
|
Aft |
5.6E7
N/m |
22.4E7
N/m |
For the propeller, the
amount of entrained water has been calculated on the basis of formulas
from Schwanecke. Basis for the calculation of the entrained water are the
dimensions of the propeller.
With these values, the
following natural frequencies are
calculated:
|
Situation |
1st
node vertical |
1st
node Hor. |
2nd
node hor. |
2nd node
ver. |
|
In
air |
15.2 |
16.0 |
33.2 |
33.9 |
|
In
water |
14.2 |
14.3 |
30.7 |
30.6 |
In the original calculation, made by the
manufacturer of the installation, the calculated natural frequency for the
1st and 2nd node shaft frequencies are 16.9 Hz and
36.2 Hz respectively. This means a difference with Techno Fysica’s
calculation of 6-10% when the influence of additional water is neglected
and 14-15% if the effect of additional water is taken into
account.
However, according to
the measurements, the problem existed due to excitation of the first
order, which amounts to approximately 11.3 Hz at nominal speed. Even in
the worst case of the above mentioned calculation results, a safe margin
between maximum excitation and the closest natural frequency should be
present, and the problem should not have existed.
However, the original
calculation omitted the stiffness of the strut, which proved to be of
vital importance.
Based on the geometry
of the aft ship, a finite element model was built. With this model, the
stiffness of the support of the aft bearing has been calculated by
applying a unit force at the location of the point of support of the shaft
in the aft bearing and determining the corresponding displacement. This
was done for both the original condition as well, in a later stage, for
the modified construction
The results
between the measurements and the theoretical stiffness were compared
and this yielded the following results:
|
Situation |
Calculated
stiffness |
Measured
stiffness |
|
Original |
3.92E6
N/m |
4.04E6
N/m |
|
Modified |
7.6E6
N/m |
10.1E6
N/m |
The calculated
stiffness of the model of the original condition closely matched that of
the measured stiffness. The stiffness of the modified installation is
wrong by almost 25%. This is probably caused by the fact that only a part
of the ship has been modelled. Since it is assumed that the measurements
have provided the correct stiffness, the modified model has been altered
in order to match it to the measured value.
This has been done by
increasing the thickness of the used plates. The final stiffness of the
modified model is 10.4E6 N/m, which closely represents the measured
stiffness.
In the model, the
propulsion shaft is modelled correctly with regards to mass and inertia
properties, and with respect to the support of the stern tube and the
rubber bearing.
It would also have
been possible to just use the value of the calculated stiffness in the
restricted shaft model, but in this way it is more easy to visualize what
actually happens.
With the combined
system, the natural frequencies have been calculated. Again, this has been
done with the properties of the propeller in air and in
water.
The following
frequencies and mode shapes are calculated:
In air:
|
Node |
Frequency |
Mode
shape |
|
I |
10.6 |
Shaft and strut
parallel and in phase, horizontal
direction |
|
II |
14.8 |
Vertical, shaft
only |
|
III |
17.2 |
Shaft and strut
in opposite direction, horizontally |
|
IV |
23.1 |
Vertical, shaft
and strut in opposite
direction |
And in
water:
|
Node |
Frequency |
Mode
shape |
|
I |
9.7 |
Shaft and strut
parallel and in phase, horizontal
direction |
|
II |
13.7 |
Vertical, shaft
and strut in phase |
|
III |
16.3 |
Shaft and strut
in opposite direction, horizontally |
|
IV |
22.5 |
Vertical, shaft
and strut in opposite
direction |
From the calculations can be
deducted that the problem is caused by the fact that the combination of
the shaft and the low stiffness of the strut shows resonance at the low
frequency of, in the calculation model, 10.6 Hz in air, and 9.7 Hz in
water. This is very close to the maximum excitation at operating speed,
and will be excited in the case of existing first order excitation
forces.
The finite element model was
adapted on the basis of the modifications as given in the mentioned
drawing. With this modified model, the following frequencies were
calculated
In air:
|
Node |
Frequency |
Mode
shape |
|
I |
14.7 |
Shaft and strut
parallel and in phase, horizontal
direction |
|
II |
16.2 |
Vertical, shaft
only |
|
III |
19.6 |
Shaft and strut
in opposite direction, horizontally |
|
IV |
30.7 |
Vertical, shaft
and strut in opposite
direction |
And in
water:
|
Node |
Frequency |
Mode
shape |
|
I |
12.9 |
Shaft and strut
parallel and in phase, horizontal
direction |
|
II |
14.9 |
Vertical, shaft
and strut in phase |
|
III |
20.6 |
Shaft and strut
in opposite direction, horizontally |
|
IV |
29.9 |
Vertical, shaft
and strut in opposite
direction |
As can
be seen, there is a considerable difference before and after modification.
The most critical first node shifts approximately 33%.
The
measured natural frequency (in air) after modification , measured in the
dock, varied between 12 Hz (SB) and 14 Hz (PS). Therefore, there is a
quite reasonable agreement between measurements and calculations,
especially on PS installation.
However, the calculated margin between nominal excitation and
closest calculated natural frequency is still too small (13%) to ensure
absence of vibrations. Based on the results of the calculations this can
be explained by the fact that, before the modifications, the installation
operated over-critical, on the flank of the first node resonance. After
modification, and despite a 33% shift, the installation operates
under-critical, but still in a flank of the same resonance. Therefore, the
stiffness will have to be increased further in order to increase the
margin between excitation and resonance.
The
purpose of this exercise was to restore the confidence in the
usefulness of applying advanced calculation methods in a design stage.
This report shows that the problem can be well reproduced in a computer
simulation. Ergo, the problem could have been prevented by performing in
an-depth analysis prior to construction.
The
analysis as originally performed was not extensive enough, and
had not captured all
problems. This is mainly due to the fact that the material used,
aluminium, has lower stiffness than is usually expected in a steel ship,
which is something an experienced engineer had realized.
However,
this fact was ignored and based on a standard
approach, no problems were expected.
|