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TCA88

Turbocharger · Turbochargers

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

The MAN TCA88 is an axial‑flow marine turbocharger that drives a turbine‑compressor unit to boost intake air pressure for large low‑speed diesel main engines, featuring DLC‑coated hydrodynamic slide bearings.

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 ✓ verified

Common issues

  • Bearing wear (journal and thrust) due to lubrication issues, contamination, or extended service intervals.
  • Compressor and turbine fouling (soot, oil mist, salt deposits) leading to reduced efficiency, increased exhaust gas temperatures, and potential surge.
  • Rotor imbalance caused by uneven fouling, blade damage, or bearing wear, resulting in excessive vibration.
  • Nozzle ring and turbine blade erosion/corrosion from exhaust gas impurities, high temperatures, or abrasive particles.
  • Oil leaks from bearing housings, sealing air systems, or oil supply/drain lines, indicating seal degradation or pressure issues.
  • Control system malfunctions (e.g., Variable Turbine Geometry (VTG) actuator issues, speed/temperature sensor failures) affecting turbocharger performance and engine load response.
  • Surge events due to engine operating conditions, heavy fouling, or control system anomalies, causing mechanical stress and potential damage.
  • Cracks in casing components (e.g., turbine casing, diffuser) due to thermal stress, vibration, or material fatigue.

Inspection checklist

  • Visual Inspection of Rotor & Casings: Check compressor impeller and turbine blades for fouling, erosion, cracks, and foreign object damage (FOD). Inspect casings for cracks, leaks, and corrosion.
  • Bearing Condition Check: Listen for abnormal noises. If possible without major disassembly, check axial and radial play. Review maintenance records for recent bearing inspections or replacements.
  • Lubricating Oil System: Verify correct oil pressure and temperature. Inspect for oil leaks around bearing housings, oil lines, and connections. Check oil filter condition.
  • Air Intake & Exhaust System: Inspect air filter/silencer for cleanliness and damage. Check exhaust gas ducts and expansion bellows for leaks and integrity.
  • Vibration Monitoring: Check current vibration levels against baseline and alarm limits. Investigate any significant deviations.
  • Control System & Actuators: Verify proper operation of VTG or wastegate actuators (if fitted). Check sensor readings (speed, boost pressure, exhaust gas temperatures) against expected values.
  • Safety Devices: Confirm overspeed trip functionality (review test records or witness test if required) and proper operation of pressure relief valves/bursting discs.
  • Cooling Water System (if applicable): Check for leaks, proper flow, and temperature in water-cooled bearing housings or intercoolers.
  • Maintenance Records: Verify adherence to MAN Energy Solutions' recommended service intervals and proper documentation of all maintenance, repairs, and inspections.

Service intervals

Compressor Cleaning (Water Wash)Every 250-500 operating hours or as required by performance drop.
Turbine Cleaning (Granulate/Liquid Wash)Every 500-1000 operating hours or as required by performance drop.
Minor Inspection (Visual, Bearing Play Check)4,000 - 8,000 operating hours (or annually, whichever comes first).
Intermediate Overhaul (Bearings, Seals, Nozzle Ring Inspection/Replacement)12,000 - 16,000 operating hours.
Major Overhaul (Full Disassembly, Rotor Balancing, Extensive Component Replacement)24,000 - 48,000 operating hours, depending on operating conditions and engine type.

Typical wear limits

Rotor Radial Bearing ClearanceNew: 0.15 - 0.30 mm. Wear Limit: Typically +50% of new value, e.g., 0.45 mm (refer to OEM manual for exact model-specific values).
Rotor Axial Bearing Clearance (Thrust Bearing)New: 0.10 - 0.25 mm. Wear Limit: Typically +50% of new value, e.g., 0.35 mm (refer to OEM manual for exact model-specific values).
Vibration Levels (at bearing housings)Alarm Limit: 8-12 mm/s RMS. Trip Limit: 15-20 mm/s RMS (ISO 10816-3 for rotating machinery, specific values in OEM manual).
Compressor/Turbine Blade Erosion/FoulingVisual inspection for significant material loss, cracks, or heavy, uneven deposits that cannot be removed by washing. Any visible crack is critical. OEM manual provides visual acceptance criteria.
Nozzle Ring Gap IncreaseTypically limited to a percentage increase from new (e.g., 10-15%) before requiring replacement due to efficiency loss. Exact values in OEM manual.

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

Critical spares

  • Bearing cartridges (complete sets for journal and thrust bearings)
  • Complete seal sets (oil and air seals, O-rings, gaskets for casing sections)
  • Lubricating oil filter elements
  • Speed sensor (magnetic pick-up)
  • Compressor washing nozzles and associated components (if not permanently installed)
  • Actuator for Variable Turbine Geometry (VTG) or wastegate (if fitted)
  • Set of bolts and nuts for casing connections (high-temperature applications)

Safety

  • High-Speed Rotating Parts: Risk of catastrophic failure (bursting) of the rotor if overspeed occurs or due to material fatigue, leading to high-velocity shrapnel projection.
  • Hot Surfaces: Exhaust gas casings, turbine outlet, and associated piping operate at extremely high temperatures (up to 600°C+), posing severe burn hazards.
  • High-Pressure Exhaust Gas: Leaks from the turbine casing or exhaust system can release hot, toxic exhaust gases into the engine room, creating a suffocation and burn risk.
  • Noise Hazard: Turbochargers generate very high noise levels during operation, requiring mandatory hearing protection in the vicinity.
  • Stored Energy: Even after engine shutdown, components remain extremely hot, and the rotor may continue to spin for an extended period, posing a hazard during immediate access.

Class survey

During the annual Class Survey, the surveyor typically checks for: Operational performance (boost pressure, speed, exhaust gas temperatures, oil parameters) against design and previous records. Verification of overspeed trip functionality (review test records or witness test). General condition, including absence of leaks (oil, water, exhaust gas), excessive vibration, and abnormal noises. Review of maintenance records to ensure adherence to manufacturer's service intervals. Inspection of foundation, mountings, and safety guards. Visual check of air intake and exhaust ducts for integrity and cleanliness.

Estimated lifetime: Major overhaul interval: 24,000 - 48,000 operating hours. Design life of main casings and rotor shaft (with proper maintenance and component replacement): 100,000+ operating hours.

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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