OceanSphereENGINES

6H35/40DF

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

Technical data from manufacturer or class sources · not yet verified by a person​‍​‍⁠‌⁠⁠⁠⁠‌‌‍‍‌‌‍‌​‌
3,360 kWPower
6Cylinders
350 mmBore
400 mmStroke

The HiMSEN 6H35/40DF is a powerful dual-fuel marine engine designed for efficient and reliable operation. This engine, with a 6-cylinder configuration and a bore of 350 mm and a stroke of 400 mm, operates at 720 rpm and delivers a rated power of 3360 kW. It is capable of running on both LNG and HFO, utilizing dual-fuel compression ignition technology to meet stringent emission standards. The engine's enhanced Miller timing ensures compliance with NOx regulations, and its advanced turbocharger design offers improved efficiency. Each cylinder produces 1250 kW, and the specific fuel oil consumption (SFOC) at 100% MCR and 85% MCR is 177 g/kWh and 174 g/kWh, respectively. The engine is certified to IMO Tier III standards and has received type approval from nine classification societies. Regular maintenance is crucial to prevent common issues such as cylinder cover wear, water contamination in the crankcase, abrasive particle wear on piston rings, and compressor/turbine wear, with water washing recommended every 200 to 500 operating hours.

Specifications

Technical data.reference — unverified

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Leistung pro Zylinder1250 kW
SFOC (100% MCR)177,0 g/kWh
SFOC (85% MCR)174,0 g/kWh
Trockengewicht H46/60V193-260 Tonnen (je nach Zylinderzahl)
Verdichtungsverhältnis17:1 (HiMSEN-Familie)
Max. Verbrennungsdruck200 bar
VentilverstellerEnhanced Miller timing für NOx-Compliance
TurboladerNeue Generation mit höherer Effizienz
ConfigurationL
Speed (rpm)720
Fuel TypeDual-Fuel LNG/HFO
TechnologyDual-Fuel CR
Power (kW)3360
Inspection

Inspector Detail ✓ verified

Common issues

  • Cylinder cover wear and surface corrosion, particularly in the fire deck area, requiring regular reconditioning during overhauls.
  • Fuel injection system malfunctions (pilot fuel and gas injectors) due to fuel quality variations, carbon build-up, or high-pressure component wear in the Common Rail system.
  • Gas admission valve and actuator issues, including sticking, leakage, or control system faults, impacting stable dual-fuel operation.
  • Exhaust valve burning or seat wear, especially when operating extensively on HFO, leading to loss of compression and performance.
  • Piston ring wear, breakage, or scuffing, resulting in increased blow-by, lube oil consumption, and potential liner damage.
  • Turbocharger fouling (compressor and turbine sides) and bearing wear, affecting engine efficiency and exhaust gas temperatures.
  • Liner wear and polishing, influenced by fuel type, lube oil quality, and piston ring condition.
  • Auxiliary system issues such as lube oil contamination, cooling water system corrosion/scaling, or fuel supply system blockages.

Inspection checklist

  • Visual inspection of cylinder heads for any signs of fuel, water, or exhaust gas leaks, paying close attention to the fire deck and injector areas.
  • Check exhaust manifold and turbocharger casing for hot spots, cracks, or insulation damage. Verify turbocharger bearing play (axial and radial) if accessible.
  • Inspect all high-pressure fuel lines (pilot fuel and HFO) for leaks, chafing, and proper securing. Verify double-walled piping integrity.
  • Monitor engine operating parameters (exhaust gas temperatures per cylinder, cooling water/lube oil pressures and temperatures, fuel consumption) for deviations from normal.
  • Inspect crankcase breathers for excessive blow-by and check the oil mist detector for proper functioning and cleanliness.
  • Verify the functionality of gas admission valves and associated safety interlocks during engine operation (if possible, or review logs).
  • Check engine foundation bolts and resilient mounts for tightness, cracks, or signs of deterioration.
  • Inspect the condition of all engine-driven pumps (lube oil, cooling water, fuel booster) for leaks, abnormal noise, and proper operation.
  • Perform a general check for abnormal noises, vibrations, or unusual smells emanating from the engine.

Service intervals

Cylinder unit (piston, liner, rings) overhaul12,000 - 18,000 hours
Cylinder head overhaul (valves, springs, seats)6,000 - 12,000 hours
Fuel injector (pilot and gas) overhaul/replacement3,000 - 6,000 hours
Turbocharger minor overhaul (bearings, seals)12,000 - 24,000 hours
Turbocharger major overhaul36,000 - 48,000 hours
Connecting rod bearing inspection/renewal12,000 - 18,000 hours
Main bearing inspection/renewal24,000 - 36,000 hours
High-pressure fuel pump overhaul12,000 - 18,000 hours

Typical wear limits

Cylinder Liner Bore (max ovality/taper)0.6 - 0.8 mm from new
Piston Ring Groove Clearance (max increase)0.15 - 0.2 mm
Crankshaft Deflection (max permissible)0.05 - 0.08 mm (for 6-cylinder inline engine)
Main & Connecting Rod Bearing Clearance (max increase)0.1 - 0.15 mm from new
Exhaust Valve Seat Recession (max)1.5 - 2.0 mm from new
Turbocharger Rotor Axial Play (max)0.1 - 0.2 mm (refer to specific TC manufacturer data)
Turbocharger Rotor Radial Play (max)0.3 - 0.5 mm (refer to specific TC manufacturer data)

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

Critical spares

  • Complete cylinder unit (piston, rings, liner, connecting rod bearings) - at least one set.
  • Complete cylinder head assembly with valves and springs - at least one set.
  • Full set of pilot fuel and gas injectors for one cylinder.
  • Exhaust valves and seats (at least 2 per cylinder type).
  • Turbocharger cartridge or critical bearing/seal kits.
  • High-pressure fuel pump elements and delivery valves.
  • Assorted O-rings, gaskets, and seals for common maintenance tasks.
  • Key sensors (temperature, pressure, speed) for critical engine systems.

Safety

  • LNG Gas Leaks: High risk of explosion and fire in enclosed spaces. Ensure gas detection systems are operational, ventilation is adequate, and gas piping integrity is maintained.
  • High-Pressure Fuel Leaks: Common Rail systems operate at extreme pressures (up to 2000+ bar). A pinhole leak can create a jet fire hazard. Verify double-walled piping and leak detection systems.
  • Crankcase Explosions: Risk from oil mist accumulation. Ensure oil mist detector is functional and crankcase ventilation is effective.
  • Hot Surfaces & Exhaust Gas Leaks: Risk of severe burns and fire. Verify insulation integrity on exhaust components and fuel lines.
  • Emergency Shutdown System (ESD): Critical for dual-fuel engines. Must be fully functional and regularly tested to ensure safe shutdown in case of abnormal conditions or gas system failure.

Class survey

For a HiMSEN 6H35/40DF, a class surveyor will typically focus on: 1. Documentation Review: Scrutinize engine logbooks, maintenance records, lube oil analysis reports, fuel changeover logs, and verify compliance with IMO Tier III NOx emissions (e.g., UEC/NOx monitoring data). 2. Safety Systems: Thorough testing of overspeed trip, low lube oil pressure shutdown, high cooling water temperature shutdown, and especially the Emergency Shutdown (ESD) system for both diesel and gas modes. Verification of gas detection system functionality. 3. Gas System Integrity: Visual inspection of LNG gas piping, valves, and associated safety devices for leaks, corrosion, and proper securing. Check for proper ventilation of gas-safe areas. 4. Crankcase Inspection: Opening of selected crankcase doors for visual inspection of main and connecting rod bearings, crankshaft journals, and the functionality of the oil mist detector. 5. Cylinder Unit Condition: Spot checks (e.g., 1-2 cylinders) of cylinder heads for valve condition, injector integrity, and general cleanliness. Review of recent cylinder pressure diagrams if available. 6. Turbocharger: Inspection of the turbocharger for bearing play, general condition, and cleanliness of the compressor and turbine sides, including the air cooler. 7. Fuel System: Inspection of high-pressure fuel pumps, pilot fuel and gas injectors, and associated piping for leaks, wear, and integrity, especially the double-walled piping. 8. Engine Performance: Review of recent engine performance data (power output, RPM, specific fuel consumption, exhaust gas temperatures) to ensure operation within approved limits. 9. Foundation and Mounts: Inspection of engine foundation bolts, chocks, and resilient mounts for signs of loosening, cracking, or deterioration.

Estimated lifetime: 80,000 - 120,000 hours before major engine overhaul (e.g., crankshaft out, full bearing renewal)

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