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A180-L 180-L25

Turbocharger · Turbochargers

Technical data from manufacturer or class sources · not yet verified by a person​‍​‍⁠‍‍⁠‍​⁠‍‌‌‍‌​‌‌⁠

The ABB A180-L turbocharger is a high‑capacity axial‑flow unit built for large two‑stroke slow‑speed diesel engines, providing up to 40 MW of boost power and improving overall propulsion efficiency.

Specifications

Technical data.reference — unverified

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Frame Size180-L25
Power max (kW)40000
Inspection

Inspector Detail

Common issues

  • Journal and thrust bearing wear or failure due to lubrication issues, contamination, or excessive loads, leading to increased vibration and noise.
  • Compressor side fouling (dirt, oil mist) on impeller and diffuser, causing reduced air flow, lower boost pressure, and decreased efficiency.
  • Turbine side fouling (soot, carbon deposits) on turbine blades and nozzle ring, leading to higher exhaust gas back pressure, reduced power, and potential surging.
  • Rotor imbalance or vibration due to fouling, blade damage (erosion, foreign object impact), or bearing wear, potentially leading to catastrophic failure.
  • Nozzle ring distortion, cracking, or erosion, affecting turbine efficiency and gas flow dynamics.
  • Oil leakage from bearing housings (e.g., through labyrinth seals) into the compressor or turbine side, leading to increased oil consumption and potential carbon build-up.
  • Cracks or distortion in the exhaust gas casing, particularly around the inlet, due to thermal stresses and fatigue.
  • Malfunction of the water washing system (clogged nozzles, pump failure), hindering effective cleaning of compressor and turbine.

Inspection checklist

  • Check turbocharger lubricating oil pressure and temperature; inspect oil filters for contamination and ensure no oil leaks from bearing casings.
  • Visually inspect compressor impeller and diffuser for fouling, erosion, or foreign object damage (FOD) through the air inlet/outlet.
  • Inspect turbine blades and nozzle ring for fouling, erosion, cracks, or FOD using a boroscope via the exhaust gas inlet/outlet (when safe and cold).
  • Manually check rotor for free rotation (when cold and safe) and axial/radial play to assess bearing condition. Listen for unusual rubbing or grinding sounds.
  • Verify tightness of all mounting bolts, foundation bolts, and connections for air, exhaust gas, and oil piping. Check for any signs of cracks in the foundation.
  • Monitor turbocharger RPM, boost pressure, exhaust gas temperatures (before and after turbine), and differential pressure across compressor/turbine for deviations from normal operating parameters.
  • Inspect the air filter for cleanliness and damage; ensure the water washing system nozzles are clear and operational.
  • Check the integrity of thermal insulation on hot surfaces (exhaust gas casings, pipes) to prevent burn injuries and maintain efficiency.
  • Verify the functionality of any associated safety devices, such as overspeed trip mechanisms (if fitted) or pressure relief valves.

Service intervals

Daily/WeeklyVisual inspection, performance monitoring, compressor washing (as required)
Weekly/MonthlyTurbine washing (as required)
8,000 - 12,000 hoursJournal bearing inspection and/or renewal
16,000 - 24,000 hoursThrust bearing inspection and/or renewal, nozzle ring inspection, minor rotor balancing if needed
32,000 - 48,000 hoursMajor overhaul (rotor removal, full inspection, cleaning, balancing, replacement of wear parts)
Every 5 years or 20,000 hours (whichever comes first)Class survey inspection of internal components during major overhaul

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

Typical wear limits

Journal Bearing Radial ClearanceTypically 0.15 - 0.30 mm (check manufacturer's manual for exact values)
Thrust Bearing Axial ClearanceTypically 0.20 - 0.40 mm (check manufacturer's manual for exact values)
Rotor Shaft Run-outMax permissible deviation usually < 0.05 mm at bearing journals
Compressor/Turbine Blade ThicknessMinimum permissible thickness reduction due to erosion (e.g., > 10-15% reduction from new is critical)
Nozzle Ring Gap/DistortionMax permissible increase in nozzle gap or distortion affecting gas flow (e.g., > 0.5 mm distortion)
Bearing Housing Bore DiameterMax permissible ovality or increase from nominal diameter

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 pads, sleeves, O-rings)
  • Labyrinth seal rings (compressor and turbine side)
  • Set of O-rings and gaskets for casing joints and oil lines
  • Lubricating oil filter elements (if dedicated turbocharger oil system)
  • Nozzle ring segments or complete nozzle ring
  • Water washing nozzles (compressor and turbine)
  • High-speed balancing weights and shims

Safety

  • Extreme rotational speeds (e.g., 8,000-12,000 RPM for A180-L) pose a severe hazard of disintegration and projectile release in case of rotor failure.
  • Very high exhaust gas temperatures (300-550°C) and hot casing surfaces present a significant burn risk; proper insulation and guarding are essential.
  • High noise levels during operation necessitate hearing protection in the vicinity of the turbocharger.
  • High-pressure boost air and exhaust gas systems require careful handling during maintenance to prevent injury from sudden pressure release.
  • Working at height on engine platforms for inspection and maintenance requires strict adherence to fall prevention procedures.

Class survey

Class surveyors will primarily focus on the overall structural integrity, secure mounting, and operational safety of the turbocharger. This includes visual inspection for any signs of leaks, cracks, or corrosion on casings, piping, and foundations. They will verify that the turbocharger's performance parameters (RPM, boost pressure, temperatures) are within acceptable limits by reviewing logbook entries. Maintenance records, particularly for major overhauls (e.g., 5-year survey intervals), bearing renewals, and rotor inspections, must be up-to-date and demonstrate compliance with manufacturer's recommendations and class requirements. The functionality of safety devices, such as overspeed protection (if applicable) and any pressure relief arrangements, will be checked. Insulation integrity on hot surfaces and proper guarding will also be confirmed.

Estimated lifetime: 150,000 - 200,000 hours (total operational life of the unit with regular maintenance and component renewal during overhauls)

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