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Mitsubishi MET

SD 53SD

Turbocharger · Turbochargers

Technical data from manufacturer or class sources · not yet verified by a person​‍​‍⁠‍⁠‌​⁠​​‌⁠‍‌‍​⁠​

The MET‑SD 53SD is a high‑performance marine turbocharger from Mitsubishi MET designed for two‑stroke main engines, delivering up to 50 000 kW of boost with a compact, low‑back‑pressure turbine.

Specifications

Technical data.reference — unverified

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Frame Size53SD
Power max (kW)50000
Inspection

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Common issues

  • Turbine side fouling (due to HFO combustion products), leading to reduced efficiency, increased exhaust back pressure, and higher exhaust gas temperatures.
  • Bearing wear (journal and thrust bearings), indicated by increased axial/radial clearances, excessive vibration, or abnormal noise.
  • Compressor wheel fouling or erosion, reducing charge air pressure and flow, and potentially causing surging.
  • Oil leakage from bearing housings or seals, leading to oil consumption and potential contamination of charge air or exhaust gas.
  • Rotor imbalance or shaft bending, causing excessive vibration and accelerated bearing wear.
  • Nozzle ring erosion or distortion, affecting turbine efficiency and gas flow.
  • Exhaust gas leakage from casing joints, expansion bellows, or turbine outlet, posing safety risks and reducing efficiency.
  • Surging, often due to compressor fouling, air filter blockage, or rapid engine load changes, causing severe vibrations and potential damage.

Inspection checklist

  • Visual inspection for oil leaks (bearing casings, oil lines) and exhaust gas leaks (turbine casing, expansion joints).
  • Check rotor free rotation (after engine shutdown) and measure axial and radial clearances of the rotor shaft. Compare with manufacturer's limits.
  • Inspect compressor wheel for fouling, erosion, or foreign object damage (FOD). Check for blade tip rubbing marks.
  • Inspect turbine blades and nozzle ring for fouling, erosion, cracks, or damage (requires opening the turbine casing).
  • Check condition of air filter elements and charge air cooler for cleanliness and blockage.
  • Monitor lubricating oil pressure and temperature to the turbocharger, and inspect oil filter condition.
  • Record and analyze exhaust gas temperatures before and after the turbine, and charge air pressure and temperature. Look for deviations from normal operating parameters.
  • Check turbocharger vibration levels using portable or permanently installed monitoring equipment.
  • Inspect casing bolts for tightness and signs of thermal stress or cracking.
  • Verify proper operation of the turbocharger washing system (water washing for compressor, dry/wet washing for turbine).

Service intervals

Minor Inspection (visual, cleaning, performance check)2,000 - 4,000 running hours
Intermediate Inspection (bearing replacement, cleaning of gas/air paths)8,000 - 12,000 running hours
Major Inspection (rotor overhaul, complete cleaning, component replacement as required)16,000 - 24,000 running hours
Overhaul (full strip-down, NDT, replacement of all wear parts, rebalancing)32,000 - 48,000 running hours or every 4-5 years

Typical wear limits

Rotor Axial Clearance (Thrust Bearing)New: 0.15 - 0.30 mm; Wear Limit: 0.40 - 0.50 mm (consult specific manual for exact values)
Rotor Radial Clearance (Journal Bearing)New: 0.08 - 0.15 mm; Wear Limit: 0.20 - 0.25 mm (consult specific manual for exact values)
Turbine Blade ErosionVisual assessment for significant material loss, pitting, or cracking. No specific thickness limit without NDT.
Nozzle Ring DistortionVisual assessment for warping or cracking. Max allowable gap increase between segments typically 1-2 mm.
Compressor Wheel Blade Tip ClearanceVisual check for rubbing marks. Specific clearance limits are in the manual, typically 0.5-1.5 mm.

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

Critical spares

  • Complete bearing cartridge assembly (journal and thrust bearings)
  • Seal rings (labyrinth seals, piston rings for oil sealing)
  • O-rings and gaskets for casing joints and oil lines
  • Air filter elements
  • Lubricating oil filter elements
  • Nozzle ring segments (if applicable, or complete nozzle ring)
  • Turbine casing insulation materials
  • High-temperature bolts and nuts for casing joints

Safety

  • Extremely high temperatures of exhaust gas (up to 550°C) and turbocharger casings, posing severe burn risks. Ensure insulation is intact.
  • High-speed rotating components (rotor operates at tens of thousands of RPM), presenting a severe hazard if casings are opened or damaged during operation.
  • High pressure within the charge air system (up to 5 bar or more), requiring careful depressurization before maintenance.
  • Potential for casing rupture in extreme fault conditions (e.g., severe overspeed, internal explosion from unburnt fuel), which can release high-energy fragments.
  • Hot lubricating oil under pressure, posing burn and slip hazards during maintenance or leakages.

Class survey

Class surveyors typically focus on: 1. Review of maintenance records, running hours, and spare parts inventory. 2. Visual inspection for external oil/gas leaks, casing integrity, and insulation condition. 3. Verification of operational performance parameters (boost pressure, exhaust gas temperatures, vibration levels) against design values and historical trends. 4. Confirmation of proper functioning of safety devices (e.g., overspeed trip, low oil pressure alarms). 5. If opened for maintenance, verification of bearing clearances and general condition of rotor, compressor, and turbine components. 6. General cleanliness and accessibility for inspection and maintenance. 7. Confirmation of compliance with manufacturer's service bulletins and recommendations.

Estimated lifetime: 32,000 - 48,000 hours before major overhaul; total design life can exceed 100,000 hours with proper maintenance and component replacement.

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