OceanSphereENGINES

9H35/40

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

Technical data from manufacturer or class sources · not yet verified by a person​‍​‍⁠‌⁠⁠⁠‍​‌​⁠​‌‌⁠​‌
9Cylinders
350 mmBore
400 mmStroke

The HiMSEN 9H35/40 engine operates on the principle of internal combustion, utilizing a diesel fuel source to generate power. This nine-cylinder, large bore engine boasts a "L" configuration, with a bore of 350 mm and a stroke of 400 mm. It is designed to operate at a speed of 720 rpm and delivers a power output of 5040 kW, making it a robust choice for demanding maritime applications. The 9H35/40 engine utilizes Common Rail Tier II technology, ensuring efficient combustion and emission control. It is capable of running on both Heavy Fuel Oil (HFO) and Marine Gas Oil (MGO), providing operational flexibility. The engine's specifications include a compression ratio of 17:1 and a maximum combustion pressure of 200 bar. The 9H35/40 is equipped with Enhanced Miller timing for NOx compliance, contributing to its environmental performance.

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 TypeHFO/MGO
TechnologyCommon Rail Tier II
Inspection

Inspector Detail

Common issues

  • Cylinder cover wear and surface corrosion, particularly in marine environments, requiring regular reconditioning.
  • Common Rail fuel injector nozzle wear, clogging, or leakage leading to poor combustion and increased fuel consumption.
  • Exhaust valve burning or seat recession, especially when operating on HFO, due to high temperatures and corrosive elements.
  • Piston ring sticking or breakage, causing increased blow-by, lubricating oil consumption, and potential liner scuffing.
  • Turbocharger bearing wear or fouling of compressor/turbine blades, impacting engine performance and efficiency.
  • Main and big end bearing wear due to lubrication issues or excessive load, requiring clearance checks.

Inspection checklist

  • Cylinder unit inspection: Check liner wear, piston crown condition, ring groove wear, and exhaust/inlet valve condition (visual and clearance checks).
  • Fuel injection system: Inspect high-pressure fuel lines for leaks, check injector spray patterns (if possible) or test bench values, and filter condition.
  • Lubricating oil system: Verify oil pressure and temperature, inspect filters, and review recent oil analysis reports for wear metals and contamination.
  • Cooling water system: Check for leaks, verify temperatures and pressures, and inspect heat exchangers for fouling or corrosion.
  • Turbocharger inspection: Check rotor free play (axial and radial), inspect compressor and turbine blades for damage or fouling, and verify bearing lubrication.
  • Crankshaft deflection: Perform deflection readings to assess main bearing alignment and potential crankshaft issues.
  • Engine safety devices: Test overspeed trip, low oil pressure shutdown, high temperature alarms, and emergency stop functionality.
  • Exhaust gas system: Inspect exhaust manifold and piping for leaks, cracks, and insulation integrity.

Service intervals

Cylinder unit overhaul (piston, liner, valves)8,000 - 12,000 running hours
Fuel injector overhaul/replacement3,000 - 6,000 running hours
Exhaust valve overhaul/replacement6,000 - 10,000 running hours
Turbocharger major overhaul12,000 - 18,000 running hours
Main and big end bearing inspection24,000 - 36,000 running hours
Major engine overhaul (incl. crankshaft inspection)48,000 - 72,000 running hours

Typical intervals for this design class, not the manufacturer’s figures for your model. The manufacturer’s manual is binding.

Typical wear limits

Cylinder liner wear (max ovality/taper)0.6 - 0.8 mm
Piston ring groove wear (increase in height)0.15 - 0.20 mm
Exhaust valve seat recession1.0 - 1.5 mm
Crankshaft deflection (max deviation between adjacent webs)0.05 - 0.08 mm
Main/Big end bearing clearance (max increase from new)0.20 - 0.30 mm

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

Critical spares

  • Complete fuel injector assembly (at least one per cylinder type)
  • Exhaust valve spindle and seat ring (at least one set)
  • Piston ring set (for at least one cylinder)
  • Main and big end bearing shells (one set of each type)
  • High-pressure fuel pipe (one length, specific to Common Rail)
  • Critical sensors (e.g., speed sensor, pressure/temperature sensors for fuel, oil, water)
  • Assortment of O-rings, gaskets, and seals for cylinder cover and fuel system components

Safety

  • High-pressure fuel leaks from the Common Rail system (up to 1800-2000 bar) pose a significant fire hazard and risk of injection injury.
  • Hot surfaces (exhaust manifold, turbocharger, engine block) can cause severe burns; ensure proper insulation and guarding.
  • Rotating machinery (flywheel, crankshaft, turbocharger rotor) presents entanglement risks; ensure guards are in place and LOTO procedures are followed.
  • Potential for crankcase explosions due to oil mist ignition; ensure crankcase ventilation and oil mist detector functionality.
  • Emergency stop system functionality must be regularly verified to ensure immediate engine shutdown in critical situations.

Class survey

Class surveyors will typically focus on verifying maintenance records and logbooks, confirming compliance with IMO Tier II (as per specs) and Type Approval conditions. Key checks include crankshaft deflection, cylinder pressure equalization (indicator diagrams), functionality of all safety devices (overspeed, emergency stops, alarms), integrity of high-pressure fuel lines, lubricating oil system performance (including oil analysis reports), and general engine room condition. They will also inspect the engine's structural integrity, foundation bolts, and exhaust gas system for leaks. Verification of spare parts inventory and crew competency for engine operation and emergency procedures is also common.

Estimated lifetime: 80,000 - 120,000 running hours before major engine rebuild (e.g., crankshaft removal)

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