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MET-SE

Turbocharger · Turbochargers

Technical data from manufacturer or class sources · not yet verified by a person​​‍‌​​‍​‌⁠​⁠‌​​‌​​⁠‍
Per manufacturer datasheetCapacity
Exhaust gas / charge airMedium
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Regular servicing and adherence to the manufacturer's guidelines are crucial for maintaining the reliability and performance of large marine diesel engine auxiliary equipment. Mitsubishi's MET-SE is designed to handle exhaust gas and charge air in both 2-stroke and 4-stroke large marine diesel engines. This axial turbine is part of the MET-SE family and is known for its robust construction. However, common issues such as turbine blade erosion, compressor fouling, bearing distress due to lube-oil contamination, and rotor imbalance from deposits can affect its performance. To address these issues, it is recommended to stock spare parts such as bearing sets, seal kits, nozzle rings, and washing equipment consumables. Servicing should follow the manufacturer's manual and classification society requirements, with an annual inspection during the class survey to ensure optimal operation.

Specifications

Technical data.

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Turbine TypeAxial
Engine Type2-stroke / 4-stroke
Service

Service notes.

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

Servicing per the manufacturer's manual and classification society requirements. Annual inspection at class survey. Stock spare parts as specified by the manufacturer.

Inspection

Common failures & inspection points

Inspection

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Common issues

  • Turbine blade erosion, fouling, or cracking due to high temperatures, corrosive exhaust, or foreign object damage.
  • Compressor fouling or erosion caused by dirty intake air, moisture ingress, or foreign particles.
  • Bearing wear and damage (journal and thrust bearings) often resulting from lube oil contamination, insufficient oil supply, or excessive vibration.
  • Rotor imbalance due to uneven deposits on blades, blade damage, or bearing wear, leading to increased vibration.
  • Exhaust gas leaks from casing joints, expansion bellows, or manifold connections, reducing efficiency and posing safety risks.
  • Oil leaks from bearing housing seals, indicating seal wear or improper installation.
  • Nozzle ring and/or diffuser vane damage, distortion, or heavy fouling, impacting gas flow and turbocharger performance.
  • Air filter clogging, leading to reduced air intake, lower boost pressure, and increased compressor load.

Inspection checklist

  • Visual inspection of turbine and compressor blades (through inspection ports) for erosion, fouling, cracks, or foreign object damage.
  • Monitor bearing temperatures (local gauges or remote system) and vibration levels; investigate any anomalies.
  • Inspect air filter condition and cleanliness; replace or clean as necessary.
  • Check for exhaust gas leaks from all casing joints, expansion bellows, and exhaust manifold connections.
  • Inspect the lube oil system for leaks, proper oil level, and signs of contamination (e.g., discolouration, water presence).
  • Verify turbocharger RPM, boost pressure, and exhaust gas temperatures are within normal operating parameters as per engine load.
  • Inspect casing for cracks, deformation, or signs of overheating, especially around hot gas inlet/outlet.
  • Check drain lines from the bearing housing for blockages or restrictions.
  • Listen for unusual noises (e.g., rubbing, whistling, grinding) during operation.
  • Confirm proper functioning of safety devices such as overspeed trip and emergency shutdown (where applicable and testable).

Service intervals

Minor Inspection (visual, cleaning)4,000 - 8,000 running hours
Bearing Inspection/Replacement8,000 - 16,000 running hours (depending on bearing type and engine duty)
Rotor Overhaul (removal, cleaning, balancing, bearing replacement)16,000 - 24,000 running hours
Major Overhaul (complete disassembly, inspection, replacement of worn parts, balancing)32,000 - 48,000 running hours
Annual Class Survey InspectionAnnually

Typical wear limits

Turbine Blade Tip ClearanceMax allowable increase 0.2-0.5 mm from new (new typically 0.5-1.5 mm cold). Any visible cracks require replacement.
Compressor Blade Tip ClearanceMax allowable increase 0.2-0.4 mm from new (new typically 0.4-1.2 mm cold). Any significant damage or erosion requires replacement.
Journal Bearing Radial ClearanceMax allowable increase 0.05-0.1 mm from new (new typically 0.1-0.3 mm).
Thrust Bearing Axial ClearanceMax allowable increase 0.03-0.05 mm from new (new typically 0.1-0.2 mm).
Rotor Run-outMax allowable radial run-out at shaft ends typically 0.02-0.05 mm.
Casing CracksAny visible crack in pressure-retaining or structural parts requires immediate attention, repair, or replacement as per manufacturer guidelines.

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

Critical spares

  • Complete set of journal and thrust bearings (including O-rings and seals)
  • Gasket and O-ring sets for casing, oil lines, and inspection covers
  • Air filter elements (if applicable to turbocharger's own filter system)
  • Lube oil filter elements (if applicable to turbocharger's own oil system)
  • High-temperature bolts and nuts for critical casing connections
  • Emergency repair kit for minor leaks (e.g., sealing compounds, small pipe fittings)
  • Nozzle ring segments (if prone to wear or damage in specific applications)

Safety

  • High Temperatures: Exhaust gas and casing surfaces can reach 400-600°C. Risk of severe burns. Ensure insulation is intact.
  • High Rotational Speed: Rotor operates at 10,000-30,000+ RPM. Risk of catastrophic failure (bursting) if overspeed or severe imbalance occurs. Never open inspection ports during operation.
  • Noise: High noise levels during operation, requiring mandatory hearing protection in the vicinity.
  • Hot Oil/Steam: Potential for hot oil spray or steam leaks from bearing housing or cooling lines, especially during operation or immediately after shutdown.
  • Heavy Components: Lifting and handling of rotor and casing parts during maintenance requires proper lifting gear, procedures, and trained personnel to prevent injury.

Class survey

Class surveyors typically verify the last major overhaul/inspection dates and review associated records. They conduct an external visual inspection for leaks (exhaust gas, oil), cracks, and general condition of insulation. Operational parameters (boost pressure, RPM, bearing temperatures, exhaust gas temperatures) are checked against normal values. Confirmation of proper functioning of safety devices (e.g., overspeed trip, if tested during survey) is crucial. The condition of the air filter and exhaust gas silencer/spark arrestor is also inspected. Surveyors will look for excessive vibration or unusual noises during operation and may review lube oil analysis reports. Finally, they confirm that critical spare parts inventory is maintained as per manufacturer and class requirements.

Estimated lifetime: 80,000 - 120,000 hours for the main rotor assembly with regular maintenance and overhauls. Casing and static components can last the lifetime of the engine if properly maintained.

Spares

Replacement Parts

Spare parts notes

Common planned spares include bearing set, seal kit, nozzle ring and washing equipment consumables.

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