wartsila 2-stroke gas engine

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WÄRTSILÄ 2-STROKE GAS 1 © Wärtsilä Wärtsilä 2-stroke / Gas Engine / September 2012 Ship Power March 2013

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  • WRTSIL 2-STROKE GAS

    1 Wrtsil Wrtsil 2-stroke / Gas Engine / September 2012

    Ship PowerMarch 2013

  • Natural Gas as marine fuel

    Wrtsil 2-stroke / Gas Engine / September 20122 Wrtsil

    1965-72: low pressure loop scavenged engine 6RD76 tested in Winterthur7RNMD90 installed in 29400m3 LNG-carrier MV Venator in 1972

    60s-70s Today

    CO2

    NOx

    SOx

    Particulates

    Dual-Fuel enginein gas mode

    Dieselengine

    0

    10

    20

    30

    40

    50

    60

    70

    80

    90

    100

    Emissionvalues [%]

    -25%

    -85%

    -100%

    -99%

    4 stroke DF results

  • Basic concept (2 stroke low pressure)

    Wrtsil 2-stroke / Gas Engine / September 20123 Wrtsil

    Principles: Engine operating accordingly

    to Otto process

    Injection of gas at mid-stroke. Low pressure gas injection(

  • Other concept (2 stroke high pressure)

    Wrtsil 2-stroke / Gas Engine / September 20124 Wrtsil

    Principles: Engine operating accordingly

    to Diesel process

    Injection of gas close to TDC. Air is completely compressed and, therefore, high pressure gas injection (300 bar) is required.

    No significant NOX reduction

    Requires SCR or EGR (not proven) in order to meet IMO Tier III levelsScavenging/

    compressionPilot & HP gas

    injection Expansion

    Direct injection, diffusion combustion

  • Otto & Diesel cycle: effects on NOX

    Wrtsil 2-stroke / Gas Engine / September 20125 Wrtsil

    Big temperature difference

    NOx formation!

    Diesel, max flame temp.Otto, max flame temp.Otto, max flame temp.

  • Technical features Gas admission

    Wrtsil 2-stroke / Gas Engine / September 20126 Wrtsil

    Gas admission system

    2 x GAV (gas admission valve) per cylinder

    GAV actuated by hydraulically fast-switching solenoid valves

    Hydraulic power supply from exhaust valve servo oil system

  • Technical features Pilot fuel system

    Wrtsil 2-stroke / Gas Engine / September 20127 Wrtsil

    Pilot fuel system

    Pilot fuel utilized for ignition (as in four-strokes DF engines)

    Micro pilot valves utilization. Pilot fuel consumption < 1% of BSFC

    Pre-chamber technology for best ignition and combustion stability

    Fuel supply based on common-rail technology (as in four-strokes DF engines)

    Pilot fuel injectors

    Pre-chamber

  • Technical features Pilot fuel system

    Wrtsil 2-stroke / Gas Engine / September 20128 Wrtsil

    Pilot fuel system

    Single fuel oil pump serving all cylinders (common-rail technology)

    Filters and pressure regulation included

    Pilot fuel pump can be electrically or mechanically driven

    UNIC

  • Technical features Gas feed system

    Wrtsil 2-stroke / Gas Engine / September 20129 Wrtsil

    Gas Valve Unit (GVU)

    Wrtsil standardized and proven design applied

    Pressure regulation, gas filtering and safety valves included

    Emergency venting procedure and leakage test features introduced

  • Technical features Automation

    Wrtsil 2-stroke / Gas Engine / September 201210 Wrtsil

    Engine automation and control system

    UNIC based control system

    Individual control of combustion related parameters

    Safety functions related to gas operation included

    Pilot fuel injectorPilot fuel injector

    Gas admission valvesGas admission valves

    Test cylinder running on gas

    Control system

    2x Gas admission valves2x Gas admission valvesPilot fuel injectorsPilot fuel injectors

    Engine speed/CA-signalEngine speed/CA-signalEngine stop signalEngine stop signal

    Gas durationGas duration

    Gas pressureGas pressure

    (Pilot fuel pressure)(Pilot fuel pressure)

    Exhaust valve driveExhaust valve drive

    Exhaust valveExhaust valve

    Pilot fuel injector

    Gas admission valves

    Test cylinder running on gas

    Control system

    2x Gas admission valvesPilot fuel injectors

    Engine speed/CA-signalEngine stop signal

    Gas duration

    Gas pressure

    (Pilot fuel pressure)

    Exhaust valve drive

    Exhaust valve

  • Performance targets (
  • Project overall time schedule

    Wrtsil 2-stroke / Gas Engine / September 201212 Wrtsil

    Project activities 2010 2011 2012 2013 2014Pre-study Concept evaluations Product requirement spec.

    Technology development Simulations & design for 1 cyl Engine tests 1 cyl

    Industrialisation 6 cylinder engine design Full scale engine tests

    Introduction Concept release Pilot installation data release:

    information release installation manual (MIM)

    Full scale engine testing: customer demo (lab engine) validation at licensee

    First sailing validation

    Design, development, preparationEngine testing

  • 2-stroke gas engine development

    13 Wrtsil Wrtsil 2-stroke / Gas Engine / September 2012

    2-stroke gas engine development based on vastexperience from 4-stroke dual fuel engines/installations

    4-stroke dual fuel references: Power plants, Merchant, Offshore, Cruise & Ferry, Special ~190 installations > 5,000,000 running hours

  • Minimum gas quality requirements

    14 Wrtsil

    Property Unit ValueLower heating value (LHV), min 1) MJ/m3N 2) 28

    Methane number (MN), min 3) 90 (IMO Tier 1)

    80 (IMO Tier 2)Methane (CH4), min % volume 70

    Hydrogen sulphide (H2S), max % volume 0.05

    Hydrogen (H2), max 4) % volume 3

    Ammonia, max mg/m3N 25

    Chlorine + Fluorines, max mg/m3N 50

    Particles or solids at engine inlet, max mg/m3N 50

    Particles or solids at engine inlet, max size um 5

    Gas inlet temperature C 060

    Water and hydrocarbon condensates at engine inlet not allowed 5)

    1) The required gas feed pressure is depending on the LHV (see section Gas feed pressure in chapter Fuel system).2) Values given in m are at 0C and 101.3 kPa. 3) The methane number (MN) is a calculated value that gives a scale for evaluation of the resistance to knock of gaseous fuels. Above table is valid for a

    low Methane Number optimized engine. Minimum value is depending on engine configuration, which will affect the performance data.

    However, if the total content of hydrocarbons C4 and heavier is more than 1% volume Wrtsil has to be contacted for further evaluation. 4) Hydrogen content higher than 3% volume has to be considered project specifically.

  • BSFC characteristics for W5X72

    15 Wrtsil

    0

    1

    2

    3

    4

    5

    6

    134

    135

    136

    137

    138

    139

    140

    141

    142

    143

    144

    30 40 50 60 70 80 90 100 110

    Pilo

    t fue

    l MDO

    [g/k

    Wh]

    LNG

    BSFC

    [g/k

    Wh]

    Engine load [%]LNG consumption [g/kWh] Pilot fuel MDO [g/kWh]

    High efficiency turbocharger ABB A100 or MET MB / ISO, LCV of 42700 kJ/kgTol. +5% between 85 to 100% load, +6% between 65 to 84% load, +7% between 50 to 64% load

  • Fuel Gas Handling System

    Qh

    Qv

    LNG FUEL GAS MODULE

    Low pressure compressor set

    Heater

    Evaporator

    LNG tank

    Low pressurefeed pump

    16 Wrtsil

  • WRTSIL 2-STROKE GASRT-flex engine conversion to gas (DF)

    17 Wrtsil Wrtsil 2-stroke / Gas Engine /

    RT-flex (Dual Fuel)RT-flex

  • RT-flex engine conversion to gas

    Wrtsil 2-stroke / Gas Engine / 18 Wrtsil

    Cylinder

    CCM-20 (Additional)

    Exhaust valve

    2/3 Pilot fuel injectors & Pre-chambersReplacement of cylinder cover

    2 x Gas Admission Valves (GAV)Extra machining of cylinder liner 2 x Gas Rail

    MDO supply unitSupport platform for MDO SUMDO pipes to injectors

    PRELIMINARYPRELIMINARY

  • RT-flex engine conversion to gas

    Wrtsil 2-stroke / Gas Engine / 19 Wrtsil

    Action Component and description Quantity

    Existing components to be replaced Cylinder cover 1 per cylinder

    Existing RT-flex parts to be modified Machining cylinder liner for gas admission valves(might also need replacement) 1 per cylinder

    New fuel system related partsMDO pump unit for fuel pilot injectors 1 per engine

    MDO pipes to fuel pilot injectors 1 system per engine

    Ignition systemPilot fuel injectors 2/3 per cylinder

    Pre-chambers 2/3 per cylinder

    Turbocharging & Scavenge air system partsWaste gate on the turbocharger 1 per engine

    By-pass valve on the turbocharger (possibly) 1 per engine

    Gas admission system components

    Gas admission valves 2 per cylinder

    Servo oil piping to gas admission valves 2 per cylinder

    Gas rails (piping) 2 per engine

    New automation system related parts (Installed automation system dependant)

    CCM-20 1 per cylinder

    Booster 8 per cylinder

    Cylinder pressure sensor 1 per cylinder

    Knocking sensor 1 per cylinder

    Other Assembly, relocation of pipes, sensors, small components. -

    PRELIMINARYPRELIMINARY