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TCA55

Turbocharger · Turbochargers

Technical data from manufacturer or class sources · not yet verified by a person​​​​‌‍⁠⁠​​‍‍⁠⁠​‌‌‌‍⁠
Per manufacturer datasheetCapacity
HFO / VLSFO / MGOMedium

The MAN TCA55 turbocharger utilizes a hydrodynamic sliding bearing with a diamond-like carbon (DLC) coating to ensure minimal wear and extended maintenance intervals. This axial-flow turbine is part of the MAN TCA family, designed to handle a wide range of applications from 5,400 to 32,400 kW. The turbocharger operates with high-efficiency lubrication, where oil is supplied through an integrated pipe system within the bearing housing, maintaining critical parameters such as viscosity, water content, and contamination levels. Regular inspections are recommended every 4,000 to 8,000 operating hours, with major overhauls required every 8,000 to 16,000 hours, thanks to the extended lifespan provided by the DLC coating. Maintenance includes periodic cleaning of the compressor and turbine sections to prevent performance degradation due to soot or salt buildup. Additionally, monitoring for high-frequency pulsations and axial play in the bearings ensures optimal performance and longevity.

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

Inspector Detail

Common issues

  • Bearing wear (journal and thrust) leading to increased clearances and vibration.
  • Compressor fouling (dirt, oil mist) reducing efficiency and causing surge.
  • Turbine fouling (soot, unburnt fuel) reducing efficiency and increasing exhaust back pressure.
  • Rotor unbalance due to fouling or component damage, leading to high vibration.
  • Oil leakage from bearing housings, oil supply/drain lines, or air/gas sides.
  • Corrosion of casing components, especially on the compressor side due to salt mist or exhaust side due to sulfuric acid dew point.
  • Actuator/control system malfunction (if applicable for VGT variants, though TCA55 is typically fixed geometry) due to moisture or vibration.
  • Cracks in turbine casing or exhaust gas manifold connections due to thermal stress.

Inspection checklist

  • Check rotor axial and radial play (manual check, compare to manufacturer's limits).
  • Inspect compressor wheel for fouling, erosion, and foreign object damage (FOD).
  • Inspect turbine wheel and nozzle ring (if applicable) for fouling, erosion, cracks, and thermal damage (borescope inspection recommended).
  • Check for oil leakage from bearing housings, oil supply/drain lines, and air/gas sides.
  • Verify exhaust gas temperatures (before/after turbine) and charge air pressure/temperature against operational norms.
  • Monitor vibration levels and compare to baseline and alarm limits.
  • Inspect air filter elements for cleanliness, damage, and proper sealing.
  • Check casing integrity, insulation condition, and tightness of mounting bolts.
  • Verify functionality of speed sensor and associated alarms/shutdowns.
  • Inspect drain lines (oil and water) for proper function and blockage.

Service intervals

Minor Inspection (e.g., cleaning of compressor/turbine, visual check)4,000 - 8,000 running hours
Bearing Inspection/Replacement8,000 - 16,000 running hours
Major Overhaul (rotor removal, full inspection, balancing, component replacement)16,000 - 24,000 running hours
Class Survey InspectionAnnually

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

Typical wear limits

Axial Play (Rotor)New: 0.15 - 0.30 mm; Service Limit: 0.40 - 0.50 mm (consult specific manual for TCA55).
Radial Play (Rotor)New: 0.08 - 0.15 mm; Service Limit: 0.20 - 0.25 mm (consult specific manual for TCA55).
Blade Thickness (Compressor/Turbine)Erosion/corrosion causing more than 10-15% reduction in original thickness, or significant notching/cracking.
Bearing Surface ConditionAny pitting, scoring, excessive wear, or discolouration indicating overheating.
Casing CracksAny visible cracks on hot casing components, especially around mounting points or exhaust gas inlets/outlets.

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

Critical spares

  • Complete bearing set (journal bearings, thrust bearing, and associated components).
  • Sealing rings (labyrinth seals, gas seals, oil seals).
  • Gasket and O-ring sets for overhaul.
  • Oil filter elements (if external oil pump/filter system).
  • Speed sensor.
  • Compressor cleaning fluid (e.g., MAN Turbocleaner).
  • Spare rotor complete (highly recommended for critical operations or remote routes).

Safety

  • High Temperatures: Exhaust gas temperatures can exceed 500°C. Risk of severe burns from hot surfaces and exhaust gas.
  • High Rotational Speeds: Rotor operates at tens of thousands of RPM. Uncontained failure (bursting) is catastrophic and can cause severe injury or death.
  • Hot Oil: Lubricating oil can be hot and under pressure. Risk of burns and slip hazards from leaks.
  • Confined Space/Heavy Lifting: Maintenance often involves working in tight spaces and lifting heavy components. Proper lifting gear and procedures are essential.
  • Noise: High noise levels during operation. Hearing protection is mandatory in the vicinity.

Class survey

Class surveyors typically check for: Verification of maintenance records and service reports (especially bearing replacements, major overhauls, and cleaning logs). Visual inspection for oil/gas leaks, general condition, and integrity of insulation. Operational checks to confirm turbocharger speed, exhaust gas temperatures (in/out), charge air pressure/temperature, and vibration levels are within acceptable limits. Confirmation of safety device functionality (e.g., overspeed trip, alarms). Inspection of air intake filter and exhaust gas silencer/spark arrestor (if applicable). Overall compliance with SOLAS and classification society rules for machinery.

Estimated lifetime: 16,000 - 24,000 running hours before major overhaul of rotating assembly (bearings, rotor balancing, seals). Static components (casings) can last longer with proper maintenance.

Spares

Replacement Parts

Spare parts notes

Spare parts via MAN Energy Solutions SE or authorised distribution partners. Lead time: 2-6 weeks.

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