Turbocharger · Turbochargers
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.
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| 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 |
| 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 Erosion | Visual assessment for significant material loss, pitting, or cracking. No specific thickness limit without NDT. |
| Nozzle Ring Distortion | Visual assessment for warping or cracking. Max allowable gap increase between segments typically 1-2 mm. |
| Compressor Wheel Blade Tip Clearance | Visual 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.
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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