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TCA44

Turbocharger · Turbochargers

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

The MAN TCA44 is an axial‑flow marine turbocharger designed to increase the air charge for large low‑speed diesel main engines, distinguished by its DLC‑coated hydrodynamic bearing system that extends maintenance intervals.

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 bearings) leading to excessive rotor play and potential shaft damage.
  • Compressor wheel fouling due to intake air contamination, reducing efficiency and causing surging.
  • Turbine wheel and nozzle ring fouling/erosion from exhaust gas impurities (e.g., heavy fuel oil combustion byproducts), impacting performance and increasing exhaust back pressure.
  • Rotor imbalance due to material accumulation or minor damage, causing vibration and accelerated bearing wear.
  • Oil leakage from bearing housings or sealing rings, indicating seal failure or excessive bearing clearance.
  • Cracks or erosion in the turbine casing or exhaust gas manifold due to thermal stress and high temperatures.
  • Actuator or control system malfunction for wastegate/variable turbine geometry (if equipped), affecting engine load response.
  • Air filter blockage or damage, leading to reduced air intake and increased compressor wear.

Inspection checklist

  • Check rotor axial and radial play (clearance) against manufacturer's limits using a dial gauge.
  • Visually inspect compressor and turbine wheels for fouling, erosion, cracks, or foreign object damage (FOD).
  • Inspect nozzle ring and diffuser for fouling, erosion, and proper seating/clearance.
  • Check for oil leaks around bearing housings, oil supply/drain lines, and casing joints.
  • Verify freedom of rotor rotation by hand (when engine is stopped and cooled), ensuring no rubbing or excessive resistance.
  • Inspect air filter elements for cleanliness and integrity; check intake ducting for leaks or restrictions.
  • Examine exhaust gas casing and manifold for cracks, hot spots, or gas leaks.
  • Check condition and tension of any associated drive belts (e.g., for auxiliary blowers, if fitted).
  • Monitor turbocharger speed, exhaust gas temperatures (in/out), and boost pressure during operation for abnormal readings.

Service intervals

Minor Inspection (visual, cleaning of compressor side)4,000 - 8,000 running hours or annually
Bearing Inspection/Replacement8,000 - 12,000 running hours
Major Overhaul (full disassembly, cleaning, inspection, balancing, replacement of wear parts)16,000 - 24,000 running hours
Annual Class Survey InspectionAnnually, as per classification society requirements

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

Typical wear limits

Rotor Radial Play (Journal Bearings)Max. 0.25 - 0.35 mm (new: 0.15 - 0.20 mm)
Rotor Axial Play (Thrust Bearing)Max. 0.15 - 0.25 mm (new: 0.08 - 0.12 mm)
Rotor Run-out (at shaft ends)Max. 0.05 mm
Nozzle Ring Clearance (between nozzle ring and turbine wheel)Varies by design, typically max. 0.3 - 0.6 mm increase from new value
Compressor/Turbine Blade Tip ClearanceVisual inspection for rubbing marks; specific values in manufacturer manual
Blade Erosion/CracksAny visible cracks or significant material loss (e.g., >10% of blade thickness) requires replacement.

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

Critical spares

  • Complete set of journal and thrust bearings (including sleeves/bushes)
  • Sealing rings (labyrinth seals for compressor and turbine sides)
  • O-rings and gaskets for casing joints, oil lines, and inspection covers
  • Oil filter elements (if applicable to the turbocharger's lubrication system)
  • Air filter elements (for engine intake, critical for turbocharger longevity)
  • Nozzle ring segments (if modular design and prone to wear/fouling)
  • Actuator diaphragm/repair kit (if wastegate or VGT equipped)
  • High-temperature bolts and nuts for casing assembly

Safety

  • High rotational speeds (up to 20,000 RPM for TCA44) pose a risk of uncontained failure (bursting) if rotor integrity is compromised.
  • Extremely high surface temperatures (exhaust casing can exceed 400°C) require proper insulation and guarding to prevent burns.
  • Potential for exhaust gas leaks, leading to toxic atmosphere in machinery spaces and fire risk.
  • Hot oil spray from failed bearings or seals can ignite on hot surfaces, causing fire.
  • High noise levels during operation necessitate hearing protection in the vicinity.
  • Risk of injury from rotating parts during inspection or maintenance if not properly isolated and secured.

Class survey

The class surveyor will typically review maintenance records, confirm adherence to manufacturer's service intervals, and visually inspect the turbocharger for external integrity, signs of leakage, and proper securing. They will check insulation, guarding, and ensure safety devices (e.g., overspeed trip, if fitted) are in place. Operational checks may include monitoring boost pressure and exhaust temperatures. Any significant vibration or abnormal noise will trigger a more in-depth investigation or require opening for internal inspection.

Estimated lifetime: 16,000 - 24,000 running hours before major overhaul (assuming adherence to maintenance schedule and proper operation)

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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