OceanSphereENGINES

34DF

Main Engine 4-Stroke · Main Engines (4-Stroke)

Technical data from manufacturer or class sources · not yet verified by a person​​‍​⁠⁠⁠​​‌​​‍⁠‌⁠‍⁠⁠​
6 / 16Cylinders
340 mmBore
400 mmStroke
Per manufacturer datasheetCapacity
LNG/MDO/HFOMedium

The Wärtsilä 34DF is a medium‑speed, four‑stroke dual‑fuel main engine capable of running on LNG, MDO, HFO or biofuels, delivering up to 500 kW per cylinder (8 000 kW total in the 16‑cylinder version) with intercooled turbocharging.

Specifications

Technical data.reference — unverified

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Power per cylinder (main engine 34DF)500 kW @ 750 rpm
Power per cylinder (auxiliary 34DF)520 kW @ 720-750 rpm
Mean effective pressure (main)20.0-19.8 bar
Piston speed9.6-10.0 m/s
Compression ratio (16V/20V)12.6:1
Engine type4-stroke, turbocharged intercooled non-reversible
Swept volume per cylinder36.3 dm³
34DF Max output (16V main)8000 kW
34DF/34SG Max output (20V genset)9800 kW
34SG designSpark-ignited, lean-burn, pre-chamber
20V34SG dimensionsL:12.7m × W:3.3m × H:4.65m
20V34SG weight131,500 kg
Speed (rpm)720/750
Service

Service notes.

What our service work and the manufacturer documentation say about keeping this model running.

Service schedule includes pilot fuel system, gas admission system and normal cylinder unit inspections.

Inspection

Inspector Detail ✓ verified

Common issues

  • Pilot injector fouling and carbon build-up, leading to poor combustion and increased emissions.
  • Gas admission valve leakage or sticking, causing gas slip or misfires, impacting efficiency and safety.
  • Cylinder pressure sensor faults, leading to inaccurate combustion analysis and potential engine protection trips.
  • Turbocharger fouling (compressor and turbine sides), reducing engine efficiency and increasing exhaust temperatures.
  • Exhaust valve burning or seat wear, particularly when operating on MDO/HFO or with sub-optimal combustion.
  • Fuel Gas Supply System (FGSS) pressure and temperature control issues, affecting gas delivery stability.
  • Lubrication oil degradation or contamination, leading to increased wear on bearings and cylinder components.
  • Cooling water system blockages or leaks, impacting engine thermal management.

Inspection checklist

  • Visual inspection for fuel (LNG/MDO/HFO), lube oil, and cooling water leaks around the engine block, piping, and connections.
  • Check pilot fuel system for proper pressure, filter differential pressure, and signs of leakage at injectors.
  • Inspect gas admission valves for external leakage, actuator function, and ensure proper sealing.
  • Monitor cylinder exhaust gas temperatures and pressures for uniformity; significant deviations indicate combustion issues.
  • Check turbocharger for unusual noises, excessive bearing play (axial/radial), and cleanliness of compressor/turbine blades.
  • Verify functionality of engine safety devices, including overspeed trip, low lube oil pressure, high cooling water temperature, and gas detection systems.
  • Inspect engine room ventilation system, especially for gas-safe areas, ensuring proper airflow and alarm functionality.
  • Review engine control system alarms and event logs for recurring faults or operational anomalies.
  • Check condition of flexible hoses and expansion bellows in fuel, exhaust, and cooling systems.

Service intervals

Pilot Injector Overhaul4,000 - 8,000 hours
Gas Admission Valve Overhaul4,000 - 8,000 hours
Cylinder Unit Top Overhaul (Piston, Liner, Valves)8,000 - 12,000 hours
Turbocharger Inspection4,000 hours
Turbocharger Overhaul12,000 - 16,000 hours
Major Overhaul (Bottom End, Crankshaft Inspection)24,000 - 36,000 hours

Typical wear limits

Cylinder Liner Wear (Max. Ovality/Taper)0.6 - 0.8 mm from nominal bore
Piston Ring Groove Wear (Max. Axial Clearance Increase)0.15 - 0.20 mm over new specification
Crankshaft Deflection (Max. between adjacent throws)0.05 - 0.08 mm
Main/Connecting Rod Bearing Clearances (Max. Increase)0.15 - 0.25 mm over new specification
Exhaust Valve Seat Recession (Max. from reference)0.8 - 1.2 mm

Ranges are typical for this design class. Always confirm against the manufacturer documentation for your serial number.

Critical spares

  • Complete pilot injectors or nozzle tips and repair kits.
  • Gas admission valve assemblies or critical sealing components.
  • Cylinder pressure sensors.
  • Full set of fuel filters (MDO/HFO, pilot fuel) and lube oil filters.
  • Exhaust valve spindles and seats (or complete cylinder heads).
  • Piston rings and cylinder liner O-rings.
  • Turbocharger bearing cartridges and sealing rings.
  • Assorted O-rings, gaskets, and seals for critical systems (fuel, gas, cooling).

Safety

  • Risk of gas leakage (LNG) leading to fire or explosion in engine room or gas-safe areas; strict adherence to gas detection and ventilation protocols is paramount.
  • High-pressure gas lines (up to 300 bar for pilot fuel, 5-10 bar for main gas) pose a significant hazard during maintenance or in case of rupture.
  • Cryogenic temperatures of LNG fuel lines and components can cause severe frostbite; proper PPE is essential.
  • Malfunction of emergency shutdown (ESD) systems for fuel gas supply can lead to uncontrolled gas release or engine overspeed.
  • Potential for unburnt gas accumulation in exhaust system, especially during transient operations or misfires, creating explosion risk.

Class survey

Class surveyors will rigorously check compliance with the IGF Code for LNG-fuelled vessels. Key areas include: verification of all safety systems (gas detection, ESD, ventilation, fire suppression) functionality; integrity and leak testing of the entire fuel gas supply system (FGSS) and engine gas lines; review of engine performance records (power, fuel consumption, exhaust temperatures, cylinder pressures) to ensure stable operation on all fuel types; inspection of maintenance records and spare parts inventory; crankshaft deflection measurements; spot checks of bearing clearances; and overall engine room cleanliness and condition. Special attention is given to the condition of exhaust valves and turbochargers, and the functionality of pilot fuel injection systems.

Estimated lifetime: 24,000 - 36,000 hours (before first major engine overhaul requiring full disassembly and bottom-end inspection)

Spares

Replacement Parts

Spare parts notes

Keep pilot injector kits, gas admission valve kits, exhaust valves, filters and electronic sensor spares.

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