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©2003 Rolls-Royce plc The information in this document is the property of Rolls-Royce plc and may not be copied or communicated to a third party, or used for any purpose other than that for which it is supplied without the express written consent of Rolls-Royce plc. This information is given in good faith based upon the latest information available to Rolls-Royce plc, no warranty or representation is given concerning such information, which must not be taken as establishing any contractual or other commitment binding upon Rolls-Royce plc or any of its subsidiary or associated companies. Bergen Engines AS - 2012

Bergen Engines AS - 2012 - SINTEF...40 % 60 % 80 % 100 % 120 % 140 % 2.5 6.2 12.5 18.6 24.9 749 749 748 751 749 Relative FSN Engine load [bar] and [rpm] Constant engine speed Reference

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  • ©2003 Rolls-Royce plc The information in this document is the property of Rolls-Royce plc and may not be copied or communicated to a third party, or used for any purpose other than that for which it is supplied without the express written consent of Rolls-Royce plc. This information is given in good faith based upon the latest information available to Rolls-Royce plc, no warranty or representation is given concerning such information, which must not be taken as establishing any contractual or other commitment binding upon Rolls-Royce plc or any of its subsidiary or associated companies.

    Bergen Engines AS - 2012

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    Market Segments

    Merchant

    Offshore NAVY Naval

    Fjord 1

    Energy

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    • Types: C25:33L6-8-9 • Bore: 250 mm • Stroke: 330 mm • Power: 330 kW / cyl • Speed: 500 – 1000 rpm • Power range: 1500 – 3000 kWmech

    • Types: B32:40L6-8-9 & B32:40V12, -16

    • Bore: 320 mm • Stroke: 400 mm • Power: 500 kW / cyl • Speed: 500 - 750 rpm • Power range: • 3000 - 8000 kWmech

    Bergen C25:33 & B32:40 Liquid fuel – MDO-HFO

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    RR-Bergen Diesel Engine Power Range

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    • Types: C26:33L6-8-9 • Bore: 260 mm • Stroke: 330 mm • Power: 270 kW / cyl • Speed: 600 – 1000 rpm • Power range: 1400 – 2500 kWmech • Efficiency: 48%mec • Types: B32:40L6-8-9 &

    B35:40V12, -16, -20 • Bore: 320 / 350 mm • Stroke: 400 mm • Power: 440 / 480 kW / cyl • Speed: 500 - 750 rpm • Power range: • 2400 - 9600 kWmech • Efficiency: 49 %mec

    Bergen C26:33 & B32/35:40 Spark ignited lean-burn gas engine

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    RR-Bergen Gas Engine Power Range

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    Natural Gas as Fuel for future vessels

    NOX ÷ 92 %

    CO2 ÷ 23 %

    SOX ÷ 100 %

    Particulate ÷ 98 %

    INVISIBLE

    SMOKE 2012

    No oil spil!

    • 35 daily port calls per vessel= 51000/year

  • ©2003 Rolls-Royce plc The information in this document is the property of Rolls-Royce plc and may not be copied or communicated to a third party, or used for any purpose other than that for which it is supplied without the express written consent of Rolls-Royce plc. This information is given in good faith based upon the latest information available to Rolls-Royce plc, no warranty or representation is given concerning such information, which must not be taken as establishing any contractual or other commitment binding upon Rolls-Royce plc or any of its subsidiary or associated companies.

    Variable Valve Timing VVT

    Low-load operation and Smoke

    Variable Valve Timing for the C25:33L engine

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    9

    Variable Valve Timing, background: Today’s modern engines run so-called Miller cycle. This

    means a relatively early closing of the air inlet valve, compared to more traditional engines.

    The Miller cycle makes it possible to reduce NOx emissions and still keep a low fuel consumption at medium to full load.

    The reduction of air to the cylinder is compensated by an increased charge air pressure.

    At medium to low load the turbocharger is loosing it’s effect. The low boost pressure combined with the early closing of the inlet valve results in a starvation of air

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    Low air consumption causing: Low load smoke from diesel engines Reduced transient response for both diesel

    and gas engines Reduced margin to turbo charger surge limit

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    Variable Valve Timing, C-engine

    Shifts timing of inlet valve to later opening/closing at low load

    Better filling of air to cylinder Established naming of positions of VVT:

    Miller position Low load position

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    Mechanism

    The original C-engine (2000-2008) uses swinging roller followers to drive the inlet and exhaust valves

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    Adoption:

    The engine was therefore well suited for an upgrade to a VVT mechanism of the type swinging roller follower on an eccentric shaft.

    This was introduced with the C25:33L 2. (C mk II), and inherited onto the C-gas.

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    Mode of operation: A shaft with eccentric journals that can be rotated 180º.

    The inlet swing-arm is mounted on an eccentric journal, while the exhaust swing-arm is mounted on the centre of the shaft.

    By rotating the shaft, the inlet swing arm moves from one side of the inlet cam, to the other side.

    The shaft is rotated by a pneumatic cylinder.

    The cylinder is activated by a solenoid valve, controlled from the PLC

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    15 Principle

    crankdeg..pu

    shro

    dlift

    Low load position CCW rotating engine

    Miller position CW rotating engine

    Miller position CCW rotating engine

    Low load position CW rotating engine

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    Instrumentation / automation / regulation

    Sensors on the pneumatic cylinder detects thr end position of the cylinder.

    The VVT mechanism can be manually locked, if required. This feature will cater for fault scenarios, such as lack of control air pressure, defect solenoid valve, or a faulty VVT cylinder.

    If the engine runs on full load with VVT in low load position, the combustion pressure will be very high. Because of this, a robust control- and alarm-system has been installed.

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    Results Smoke

    Smoke

    400 500 600 700 800 900 1000

    rpm

    Miller position

    Low load position

    Miller position & Low load position combined

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    Results NOx

    NOx

    400 500 600 700 800 900 1000

    rpm

    Miller position

    Low load position

    Miller position & Low load position combined

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    Fuel consumption

    400 500 600 700 800 900 1000rpm

    Fuel consumptionpropeller law

    Miller position

    Low load position

    Miller position & Low load position combined

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    Maximum combustion pressure

    P max

    400 500 600 700 800 900 1000

    rpm

    Miller position

    Low load position

    Miller position & Low load positioncombined

  • ©2003 Rolls-Royce plc The information in this document is the property of Rolls-Royce plc and may not be copied or communicated to a third party, or used for any purpose other than that for which it is supplied without the express written consent of Rolls-Royce plc. This information is given in good faith based upon the latest information available to Rolls-Royce plc, no warranty or representation is given concerning such information, which must not be taken as establishing any contractual or other commitment binding upon Rolls-Royce plc or any of its subsidiary or associated companies.

    Smoke reduction at low engine load by fuel injection optimization

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    22 Reduction of visible smoke

    Flow through nozzle reduced by 9% Opening pressure of injector increased by 33% to

    compensate for restricted nozzle flow Significantly reduced visible smoke on low-load operation Small increase on high-load operation

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    Reduced nozzle flow trough value and increased nozzle opening pressure

    100 % 100 % 100 % 100 % 100 %

    74 % 81 %

    92 %

    130 %

    120 %

    62 %

    75 % 82 %

    110 %

    120 %

    0 %

    20 %

    40 %

    60 %

    80 %

    100 %

    120 %

    140 %

    2.5 6.2 12.5 18.6 24.9

    749 749 748 751 749

    Rel

    ativ

    e FS

    N

    Engine load [bar] and [rpm]

    Constant engine speed

    Reference nozzle and NOP

    Nozzle flow through value reduced by 9%

    Nozzle flow through value reduced by 9% andNOP increased by 33%

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    Reduced nozzle flow trough value and increased nozzle opening pressure

    100 % 100 % 100 % 100 %

    78 % 77 %

    111 % 105 %

    78 % 79 %

    122 % 121 %

    0 %

    20 %

    40 %

    60 %

    80 %

    100 %

    120 %

    140 %

    9.9 15.6 20.5 24.9

    475 600 682 748

    Rel

    ativ

    e FS

    N

    Engine load [bar] and [rpm]

    Propeller curve

    Reference nozzle and NOP

    Nozzle flow through value reduced by 9%

    Nozzle flow through value reduced by 9% andNOP increased by 33%

    Bergen Engines AS - 2012��Market SegmentsBergen C25:33 & B32:40Slide Number 4Bergen C26:33 & B32/35:40Slide Number 6Slide Number 7Variable Valve Timing VVT ��Low-load operation and Smoke�Variable Valve Timing, background:Low air consumption causing:Variable Valve Timing, C-engineMechanismAdoption:Mode of operation:PrincipleInstrumentation / automation / regulationResults SmokeResults NOxFuel consumptionMaximum combustion pressureSmoke reduction at low engine load by fuel injection optimization Reduction of visible smokeReduced nozzle flow trough value and increased nozzle opening pressureReduced nozzle flow trough value and increased nozzle opening pressure