178
injectionby5°ofcrankshaftanglearesimulatedinthe
article [5]. The results have revealed the changes in
specific fuel consumption (SFC), the increase of
exhaust temperature and the reduction of fuel
injection pressure. Other articles [6, 7] provided
insightintothefaultsoftheturbochargersystemand
its
effects on the main engine. The exhaust
temperaturewillincreasewiththefoulingofturbine
wheel or blockage of the air filter, which will
consequently affect the exhaust emissions. The
adequatemaintenanceoffuelsystemcomponentsand
optimizationoffuelinjectioniscrucialforanefficient
combustionprocess.
2
METHODOLOGY
The data used for the research in this paper was
obtained on the Wärtsilä ERS‐LCHS 5000 TechSim
engine room simulator, owned by the Maritime
departmentoftheUniversityofZadar.Themodelled
vesselisaLCCtankerwithaMANB&W6S60MC‐C,
two strokes, slow speed, turbocharged, reversible
main diesel engine [8]. The vessel simulated in this
modelisshowninfigure1.
Figure1.Simulatormodelvessel‐LCCtankerwithaMAN
B&W6S60MC‐Cmainengine[8]
Thedieselengine,typeMC,isatwo‐strokediesel
engine with direct injection and centrally located
exhaust valve. MAN Diesel & Turbo is one of the
worldʹs leading designers and manufacturers of
engineswithlowandmediumspeed.Enginetrialtest
report,the so‐calledshop test report,MAN
6S60MC
wasusedduringtheanalysisofoperatingparameters
andrecordingtheindicatordiagramoftheenginein
real conditions [9]. These data were compared with
data obtained on the ship simulator ERS 5000
TechSim. Obtained values for: mean effective
pressure,maximumcombustionpressure,fuelpump
index recordedin the
trial test were compared with
shipsimulatorinnormalconditionsataspeedof105
min‐1andtheyarealmostidentical.Therefore,itcan
beconcludedthattheshipsimulatorisvalidforthis
research [9]. The basic main engine particulars are
shownintable1.
Someofthemany
featuresofthesimulatormodel
are introducing various environmental and fault
variables during vessel navigation such as
environmental loads, late and early fuel injection,
pistonringwear, damagedfuelnozzle,turbocharger
airfilterblockageetc.Thefaultsusedfortheresearch
inthispaperarelatefuelinjection,earlyfuel
injection
andturbochargerairfilterblockage.Thelimitationsof
using simulated data for scientific research is the
possible inaccuracy of the mathematical model used
for simulator programming. This can only be
validatedusingdatafromonboardmeasurementson
actualvessels.
Table1.Mainengineparticulars[8]
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MainEngineParticulars
________________________________________________
TypeMANB&Wmodel6S60MC‐C
Ratedpower 13736kW
Cylindernumber 6
Bore600mm
Stroke2400mm
Ratedspeed 105Rpm
NominalMCR 13736kWat105RPM
________________________________________________
Area of navigation chosen for the simulations is
theAdriaticSea, however since environmental loads
i.e., wind, waves, wave spectrum and sea current,
werenotsimulatedforthepurposesof thisresearch
theareaofnavigationisoflittleimportanceandofno
impact.Fuel used for the combustion process in
the
main engines is a distillate marine diesel oil (MDO)
withlessthan0.5%ofsulphurcontent.Thesimulated
parametersrecordedforthepurposeofthisresearch
were average cylinder exhaust gas temperature
shown in degrees Celsius (°C), main engine fuel oil
consumption (FOC) shown in litres per hour
(L/h),
carbon dioxide emission (CO
2) shown in percentage
by volume (%), sulphur oxides emission (SO
X) and
carbon monoxide emission (CO) shown in parts per
million (ppm). The degree of late or early injection
timingwaschosenbasedonexperienceinthisfieldof
researchandwassetatvaluesexpressedinnegative
orpositivedegreesofcrankshaftposition(°)relative
toitspositionatnormal
injectiontiming[0(allcyl)]as
is shown in table 2. the degree chosen was the
maximumpossiblesettinginthesimulatormodeland
is thus only expressed in later text with respective
abbreviations ‘EI’for early injection and‘LI’ for late
injection.Earlyandlatefuelinjectionfaultparameters
were introduced in three stages at specific time
intervals chosen to give the parameters recorded
enoughtimetostabilizeatarelativelyconstantvalue.
Thefirststagewasearlyorlatefuelinjectiononone
cylinder[EIorLI(1cyl)],thesecondstagewasearly
or late fuel injection on
three cylinders [EI or LI (3
cyl)] and the third stage was early or late fuel
injections in all cylinders [EI or LI (all cyl)]. The
turbocharger air filter blockage fault parameter was
introduced in four stages at specific time intervals
same as the early and late fuel injection fault
parameter.Thefourstageswere10%,20%,30%and
40%turbochargerairfilterblockageshownintable2.
Theobservedtimeneededforparameterstabilization
was two minutes. All of the above‐mentioned
parameters were simulated under one engine load
setting. The engine load simulated is 85
% of
maximum continuous rate (MCR). This engine load
waschosenbasedonusualoptimumengineloadfor
the specific engine type used in the referent vessel
[8,10].
Table2.Injectiontimingandairfilterblockagedegree
relativetospecificsimulationtimeintervals
________________________________________________
T(min)0:00 2:00 4:00 6:00 8:00
________________________________________________
InjectionTiming0 EI EI EI /
(Early)(allcyl) (1cyl) (3cyl) (allcyl)
Injectiontiming0 LI LI LI /
(Late)(allcyl)(1cyl)(3cyl) (allcyl)
Turbocharger 0 10 20 30 40
AirFilter
Blockage
________________________________________________