
41
High pressure turbine blades scratches are not
regular issues and they have to be treated instantly in
order to avoid serious turbine damages due to metal
particles which may enter to further turbine stages.
For this type of failure it is difficult to say what was
the exact cause but in similar cases this type of failure
is usually connected with water droplets at high
pressure stages which are carried over from the main
boiler or from undrained pipelines. High pressure
turbine casing drain is placed beyond 4
th
turbine stage
and if draining is not appropriate water may enter to
further stages with steam flow through the rotor.
Water droplets increase rotor vibrations and erode
turbine blades. Figure 2 shows high pressure turbine
second stage blade erosion at the same turbine
discovered during the third dry-dock.
Figure 2. High pressure turbine rotor blade erosion
Non critical failures which are listed due to
degradation of the materials are:
− Astern turbine safety control oil valve exchanged.
− Astern turbine steam temperature PT sensor
exchanged.
− Flexible spider clutch for coupling main turbine
control oil pump No1 and electromotor
exchanged.
− Flexible spider clutch for coupling main turbine
control oil pump No2 and electromotor
exchanged.
− Local manoeuvring side telegraph bell exchanged.
− Steam pressure transmitter at first stage outlet
exchanged.
− High pressure bleed steam shut of valve solenoid
valve exchanged.
− Main propulsion turbine revolution counter
exchanged.
− PT sensor for main turbine steam temperature at
steam chest exchanged.
− High pressure turbine bleed shut off valve limit
switch exchanged.
− Main turbine lube oil pump No2 electromotor
bearing exchanged.
− Main turbine reduction gear dry air fan
exchanged.
− Main turbine manoeuvring log unit at bridge
station exchanged.
− Main propulsion turbine bridge telegraph CPU
unit exchanged.
The most frequent and recurring failure is related
to flexible spider clutch for coupling the main turbine
control oil pump No1 and No2 with electromotor. As
this failure is recurring it may be assumed that
hydraulic pump and electromotor are not aligned
properly what causes frequent spider damage. This
type of failure may be corrected once vessel enters
dry-dock.
The second group of recurring failures refer to
monitoring equipment i.e. PT temperature sensors
and pressure sensors that were exchanged three
times. These failures are unavoidable because selected
PT sensors operate at high temperatures and have
limited working temperature range (slightly above
operating temperature). Owner decided to mount
cheap solution in the beginning but frequent failures
do not justify owner’s first choice.
Control equipment failures related to navigation
equipment include: local manoeuvring side telegraph
bell failure, main propulsion turbine revolution
counter failure, main turbine manoeuvring log unit at
bridge station failure and main propulsion turbine
bridge telegraph CPU unit failure. These failures are
not expected in such number. It is a compulsory
requirement that main turbine telegraph order log is
working due to safety requirements and restoration of
manoeuvring in the case of incident.
Miscellaneous failures are related to: astern
turbine safety control oil valve failure, high pressure
bleed steam shut of valve solenoid valve failure, high
pressure turbine bleed shut off valve limit switch
failure, main turbine lube oil pump No2 electromotor
bearing failure and main turbine reduction gear dry
air fan failure. Miscellaneous failures are of low
frequency and they are in expected occurrence range.
Incipient failures/faults are caused due to non-
perfect condition of equipment so that a degraded or
critical failure might occur [7]. In order to prevent
incipient faults, according to Table 2, corrective
actions were taken: forward labyrinth seal springs
were renewed and scale deposit at low pressure
turbine first stage was cleaned.
5 CONCLUSION
In this paper failure events of main propulsion
turbine on LNG carrier were analysed. Analysis
defined three main groups of failures for the main
propulsion turbine in presented time range: critical
failures, non-critical failures due to deterioration of
material and non-critical incipient failures or faults.
The non-critical failures due to material
deterioration are listed as: main propulsion turbine
control system failures related to the flexible spider
clutch with 7 failures, miscellaneous failures with 5
failures, control equipment related to navigation with
4 failures and monitoring equipment with 3 failures.
Incipient failures: related to labyrinth seal and scale
deposit at low pressure turbine with totally 2 events.
Non critical failures may be treated in the port or
during anchorage and they have low impact to
propulsion turbine reliability. The frequency
distribution of failures related to flexible spider clutch
has to be improved in order to avoid possible
dangerous situation with two control oil pumps in
failure. This will cause stoppage of the main
propulsion turbine. In order to avoid such risk, spare
part kit should be on board the vessel for quick repair.
The other weak points were control equipment