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TCR14

Turbocharger · Turbochargers

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

The MAN TCR14 turbocharger employs a radial-flow turbine design, offering robust performance in marine applications. This model is part of the TCR family by MAN Energy Solutions, designed to handle a range of fuels including HFO, VLSFO, and MGO. The turbocharger features hydrodynamic sliding bearings coated with DLC (Diamond-Like Carbon) to reduce friction and extend maintenance intervals to 8,000–16,000 operating hours. It operates at typical speeds of 150,000 RPM, with an oil film thickness of 3–6 micrometers, ensuring optimal lubrication. Maintenance checks include axial rotor displacement measurements using a white line method to detect any excessive radial bearing clearance, which should not exceed 2–5 micrometers. Regular inspections and oil analysis are crucial to prevent common issues such as excessive radial bearing clearance, nozzle ring blockage, and oil contamination. Spare parts are available from MAN Energy Solutions or authorized distributors, with a lead time of 2 to 6 weeks.

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 (radial and axial) leading to increased rotor play and potential contact with casings.
  • Fouling of compressor impeller and turbine blades, reducing efficiency and potentially causing rotor imbalance.
  • Oil leakage from bearing housings (compressor or turbine side) due to worn seals or excessive bearing clearance.
  • Cracks, erosion, or corrosion in the turbine casing, nozzle ring, or diffuser, particularly in areas exposed to high temperatures and corrosive exhaust gases.
  • Surge events caused by engine load changes, exhaust gas system issues, or turbocharger component degradation.
  • Malfunction or wear of Variable Turbine Geometry (VTG) components or wastegate actuators, impacting engine performance and emissions.
  • Exhaust gas leaks from casing joints or expansion bellows, leading to reduced efficiency and potential fire hazards.
  • Electronic control unit (ECU) or sensor failures due to vibration, moisture ingress, or aging.

Inspection checklist

  • Visual Inspection (External): Check for oil leaks, exhaust gas leaks, casing cracks, loose fastenings, insulation integrity, and signs of overheating.
  • Rotor Free Play (Axial & Radial): Measure using a dial gauge (after cooling down) to ensure within manufacturer's specified limits. Pay close attention to any sudden increase.
  • Rotor Cleanliness & Condition: Inspect compressor impeller and turbine blades for fouling, erosion, foreign object damage (FOD), or signs of rubbing against casings.
  • Bearing Condition (Audible/Vibrational): Listen for unusual noises during operation; check vibration levels using a portable vibration meter if available. Look for oil contamination.
  • Lubricating Oil System: Verify oil pressure, temperature, and filter condition. Check for signs of carbonization or water ingress in the oil.
  • Air Filter Condition: Ensure air intake filters are clean, undamaged, and correctly installed to prevent FOD and fouling.
  • Exhaust Gas System Integrity: Inspect expansion bellows, exhaust pipes, and manifold connections for leaks, cracks, or signs of stress.
  • Safety Devices & Controls: Confirm overspeed trip functionality (if applicable) and alarm settings. Verify proper operation of VTG or wastegate actuators and associated sensors.
  • Drainage Systems: Check that all drain lines (oil, water) are clear and functioning correctly.

Service intervals

Minor Inspection (Visual/Operational)2,000 - 4,000 running hours or annually
Intermediate Inspection (Bearings/Seals)8,000 - 16,000 running hours (e.g., replacement of journal and thrust bearings, sealing rings)
Major Overhaul (Rotor/Casing/Components)24,000 - 48,000 running hours (e.g., complete rotor overhaul, inspection/replacement of nozzle ring, diffuser, casings)
Complete Overhaul/Refurbishment72,000 - 96,000 running hours (e.g., full factory refurbishment or replacement of major components)
Class Survey InspectionAnnually (external), Special Survey (internal, typically aligned with major overhaul intervals)

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

Typical wear limits

Rotor Axial PlayNew: 0.15 - 0.35 mm; Wear Limit: 0.5 - 0.7 mm
Rotor Radial PlayNew: 0.08 - 0.15 mm; Wear Limit: 0.25 - 0.35 mm
Journal Bearing ClearanceNew: 0.05 - 0.10 mm; Wear Limit: 0.15 - 0.20 mm (check manufacturer's manual for exact values)
Nozzle Ring/Turbine Blade Tip ClearanceIncreased clearance due to erosion/wear significantly reduces efficiency. Refer to manufacturer's specific values for maximum allowable clearance.
Compressor Impeller Blade Erosion/DamageAny significant erosion, cracking, or foreign object damage (FOD) requires replacement or repair as per manufacturer's guidelines.

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

Critical spares

  • Bearing Cartridge (complete, or individual journal and thrust bearings)
  • Sealing Rings (gas and oil side, especially for the turbine and compressor ends)
  • O-rings and Gaskets for casing joints and connections
  • Lubricating Oil Filter Elements
  • Air Filter Elements (if applicable to the turbocharger intake system)
  • Nozzle Ring (if fixed geometry, or key VTG components if variable)
  • Diffuser (if prone to damage or erosion in specific applications)
  • Actuator/Solenoid Valve for wastegate or VTG control (if applicable)

Safety

  • High-Speed Rotating Parts: Risk of severe injury from contact with the rotor during operation or if casing integrity is compromised due to overspeed or material failure.
  • Hot Surfaces: Exhaust gas casing and associated piping operate at extremely high temperatures (300-600°C), posing severe burn hazards. Ensure insulation is intact.
  • High-Pressure Exhaust Gas: Potential for exhaust gas leaks or casing rupture, leading to fire risk, personnel injury, and engine room contamination.
  • Noise Levels: High noise levels (typically >100 dB) necessitate hearing protection in the vicinity of the turbocharger during operation.
  • Overspeed: Catastrophic failure if the overspeed protection system fails, leading to rotor disintegration and potential projectile hazards within the engine room.

Class survey

Class surveyors typically check the following: Review of maintenance records, running hours, and previous inspection reports. External visual inspection for leaks, cracks, secure mounting, and intact insulation. Verification of safety devices, particularly overspeed trip functionality and alarm settings. Operational checks to confirm normal performance (boost pressure, exhaust gas temperatures). During special surveys or if deemed necessary, an internal inspection of the rotor, bearings, nozzle ring, and casings for wear, fouling, and damage may be required, often aligning with the engine's special survey schedule.

Estimated lifetime: 24,000 - 48,000 hours before major overhaul of critical components (bearings, seals, nozzle ring, diffuser). Main casings and rotor shaft can exceed 100,000 hours with proper maintenance and component replacement.

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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