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M 46 DF

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

Data sheet on file · key figures checked​​‍​⁠⁠⁠​⁠‍‍‌‌‍⁠‍⁠​​⁠
900 kWPower
6 / 16Cylinders
460 mmBore
610 mmStroke
Per manufacturer datasheetCapacity
LNG/MDO/HFOMedium
View photo ↗

Designed with robust engineering and a focus on reliability, the Caterpillar MaK M 46 DF ensures minimal downtime and consistent performance in demanding maritime environments. With a powerful output of 900 kW, this engine is built to meet the stringent demands of modern shipping operations, providing reliable power that can be counted on for long voyages and critical missions. The advanced design of the MaK M 46 DF not only delivers high efficiency but also simplifies maintenance procedures, reducing operational costs over the lifespan of the equipment. This makes it an ideal choice for vessel owners and operators who prioritize both performance and reliability. Whether powering commercial vessels or specialized maritime applications, the Caterpillar MaK M 46 DF stands out as a dependable and powerful solution, ensuring that your operations run smoothly and efficiently.

Specifications

Technical data.from datasheet

Every value below comes from the manufacturer datasheet or class-society record on file for this model.

Displacement per cylinder101.3 liters
Power per cylinder900 kW/cylinder at 500-514 rpm
Bmep21.3/20.7 bar
Fuel consumption (diesel mode)186 g/kWh
Fuel injection systemCommon-Rail-Ignition fuel oil system with cylinder selective gas injection
Turbocharged charge air cooledYes
Four-stroke non-reversibleYes
IMO complianceIMO Tier II in diesel mode; IMO III in gas mode
Methane slip (gas mode)Minimal (stated as feature; specific values not publicly disclosed)
Power (kW)900🔖
Speed (rpm)500/514
📄
Download datasheet (PDF) (1486 KB)
Manufacturer documentation

Images from manufacturer documentation.

Photos, drawings and page previews from this model’s datasheet or catalog.

Caterpillar MaK MaK M 46 DF – Photo (Caterpillar MaK datasheet S. 1)
Photo · Caterpillar MaK datasheet · S. 1
Service

Service notes.

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

Dual-fuel service includes gas admission system, pilot fuel system, combustion control and normal cylinder unit inspections.

Inspection

Inspector Detail ✓ verified

Common issues

  • Gas admission valve malfunction (sticking, leakage, control issues)
  • Pilot injector fouling or wear, leading to poor ignition or misfires
  • Turbocharger fouling (compressor/turbine side) or bearing wear, affecting engine performance
  • Combustion control sensor faults (e.g., cylinder pressure, exhaust gas temperature sensors)
  • Fuel gas system leaks (piping, connections, seals) due to vibration or material degradation
  • Exhaust gas temperature deviations between cylinders, indicating combustion imbalance
  • Cylinder liner scuffing or excessive wear, potentially exacerbated by dual-fuel operation
  • Lube oil degradation or contamination, particularly with gas fuel operation

Inspection checklist

  • Visual inspection for any leaks (gas, MDO/HFO, lube oil, cooling water) around engine and fuel gas train.
  • Check exhaust gas temperatures (EGT) per cylinder for uniformity; significant deviations indicate combustion issues.
  • Verify pilot fuel system pressure and filter differential pressure; inspect pilot injectors for external leaks.
  • Listen for proper operation of gas admission valves; check for gas leaks around valve blocks and piping.
  • Inspect turbocharger for abnormal noise, excessive vibration, oil leaks, and cleanliness of compressor/turbine blades.
  • Monitor lube oil pressure, temperature, and filter differential pressure; check crankcase breather for excessive blow-by.
  • Verify cooling water system parameters (pressure, temperature, expansion tank level) and inspect for leaks.
  • Check functionality of engine safety devices (overspeed trip, low lube oil pressure, high cooling water temperature, gas detection alarms).
  • Inspect fuel gas supply system for proper ventilation, double-wall piping integrity, and condition of flame arrestors.
  • Review engine control system alarms and event logs for recurring faults or performance anomalies.

Service intervals

Daily/WatchVisual checks, log readings, alarm panel review, fuel gas system leak detection.
500-1000 hrsLube oil filter change, MDO/HFO fuel filter change, pilot fuel filter change.
2000-4000 hrsPilot injector inspection/overhaul, gas admission valve inspection, valve clearance check.
6000-8000 hrsCylinder head overhaul (valves, springs, seats), turbocharger inspection/cleaning.
12000-16000 hrsPiston crown and skirt inspection, connecting rod bearing inspection.
24000-36000 hrsMajor overhaul (liner wear measurement, crankshaft deflection, main bearing inspection, fuel pump overhaul).

Typical wear limits

Cylinder Liner WearMax 0.6-0.8 mm at top dead center (TDC) of top ring travel.
Piston Ring Gap (Top Ring)Max 1.5-2.0 mm (check manufacturer's specific limits).
Crankshaft DeflectionMax 0.05-0.08 mm between adjacent throws (check manufacturer's specific limits).
Connecting Rod Bearing ClearanceMax increase 0.10-0.15 mm over new component clearance.
Main Bearing ClearanceMax increase 0.10-0.15 mm over new component clearance.
Valve Seat RecessionMax 0.5-1.0 mm from original position (check manufacturer's specific limits).
Turbocharger Rotor Axial PlayMax 0.15-0.20 mm (check manufacturer's specific limits).
Turbocharger Rotor Radial PlayMax 0.30-0.40 mm (check manufacturer's specific limits).

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

Critical spares

  • Pilot injectors (complete units or nozzle tips)
  • Gas admission valves (or critical repair kits/seals)
  • Fuel filters (MDO/HFO, pilot fuel, gas filters if applicable)
  • Lube oil filters
  • Gaskets and O-rings for cylinder heads, fuel lines, and gas system components
  • Combustion control sensors (e.g., EGT, pressure transducers)
  • Turbocharger bearing cartridges (if field replaceable)
  • High-pressure pilot fuel pump elements

Safety

  • Gas Leaks: High risk of explosion or fire from LNG leaks, especially in enclosed spaces. Ensure gas detection systems are operational and ventilation is adequate.
  • High-Pressure Fuel: Risk of injection injury from MDO/HFO and pilot fuel systems. Always depressurize before working.
  • Hot Surfaces: Engine components, exhaust system, and turbocharger operate at high temperatures, posing burn hazards.
  • Rotating Machinery: Entanglement risk from crankshaft, flywheel, and turbocharger. Ensure proper lockout/tagout procedures.
  • Crankcase Explosion: Risk from excessive blow-by or localized overheating. Monitor crankcase pressure and temperature.
  • Oxygen Depletion: In areas with potential gas leaks, oxygen levels can drop rapidly, leading to asphyxiation.

Class survey

Class surveyors will rigorously check documentation (maintenance records, running hours, fuel consumption logs, alarm history). Focus areas include the integrity and functionality of the fuel gas supply system (leakage tests, ventilation, double-wall piping, gas detection, emergency shutdown), engine safety devices (overspeed, low oil pressure, high water temp, gas emergency stops), crankshaft deflection records, and general engine condition (leaks, corrosion, cleanliness). They will also verify the functionality of bridge and local control systems, interlocking mechanisms, and the overall performance of the combustion process (e.g., exhaust gas temperature uniformity, cylinder pressure analysis if available).

Estimated lifetime: 24,000 - 36,000 hours before major overhaul (e.g., piston/liner renewal, main bearing inspection). Total operational life can exceed 100,000 hours with continuous, diligent maintenance and component renewal.

Spares

Replacement Parts

Spare parts notes

Keep gas admission valve kits, pilot injectors, sensors, filters, exhaust valves and sealing kits.

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