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TPL-A 65

Turbocharger · Turbochargers

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

The ABB/Accelleron TPL‑A 65 is a high‑capacity turbocharger for two‑stroke marine diesel engines, delivering up to 50 MW of boost with optimized aerodynamics for maximum fuel efficiency.

Specifications

Technical data.reference — unverified

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Frame Size65
Power max (kW)50000
Inspection

Inspector Detail

Common issues

  • Bearing wear (journal and thrust bearings) leading to increased axial/radial play and vibration.
  • Compressor fouling due to oil carry-over or dirty intake air, reducing air delivery and efficiency.
  • Turbine fouling from exhaust gas deposits (especially with HFO), leading to reduced power and increased exhaust back pressure.
  • Nozzle ring and diffuser erosion/damage, impacting turbine efficiency and gas flow.
  • Oil leakage from bearing housing seals (labyrinth seals) into compressor or turbine side, indicating seal wear or incorrect oil pressure.
  • Rotor imbalance causing excessive vibration, often due to blade damage, fouling, or bearing issues.
  • Surging, indicated by unstable operation, often due to engine load changes, severe fouling, or incorrect matching.

Inspection checklist

  • Check rotor axial and radial play (bump test) against manufacturer's limits. Listen for free rotation.
  • Inspect compressor wheel for cleanliness, blade damage, and tip clearance. Ensure no rubbing marks.
  • Inspect turbine wheel for cleanliness, erosion, blade damage, and tip clearance (if accessible).
  • Examine nozzle ring and diffuser for erosion, cracks, or deformation. Check for proper opening (if VTA).
  • Verify lubricating oil inlet pressure and temperature are within specified ranges. Check oil drain for proper flow.
  • Inspect air filter condition and ensure no restrictions in the air intake system.
  • Check for any signs of oil or exhaust gas leakage from casing joints, drain lines, or seal areas.
  • Monitor turbocharger vibration levels using onboard monitoring systems or portable equipment.
  • Check condition of washing nozzles (compressor and turbine) and confirm proper operation during washing cycles.
  • Inspect exhaust gas casing and insulation for cracks, hot spots, or signs of gas leakage.

Service intervals

Compressor water washDaily to weekly, depending on engine load and air quality.
Turbine water washWeekly to monthly, depending on engine load and fuel type (HFO operation typically weekly).
Bearing inspection/replacement8,000 - 12,000 running hours (or annually), depending on condition and monitoring.
Major overhaul (rotor out, full inspection)16,000 - 24,000 running hours (or every 2-3 years).
Rotor balancingDuring major overhaul or if excessive vibration persists after bearing replacement.

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: 0.20 - 0.25 mm. Wear limit: Typically +0.15 mm from new value, or specific manufacturer limit (e.g., 0.40 mm max).
Rotor radial playNew: 0.15 - 0.20 mm. Wear limit: Typically +0.10 mm from new value, or specific manufacturer limit (e.g., 0.30 mm max).
Compressor/Turbine blade tip clearanceManufacturer specific, typically 0.5 - 1.5 mm. Any rubbing marks or significant increase indicates bearing wear or casing deformation.
Nozzle ring openingVisual inspection for erosion/damage. Significant increase in opening due to wear reduces efficiency; replacement required.
Bearing surface conditionNo scoring, pitting, or excessive discoloration. Babbitt layer intact.

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 pads and thrust collar).
  • Labyrinth sealing rings (compressor and turbine side).
  • Gasket and O-ring sets for casing joints and service connections.
  • Air filter elements (if applicable for intake).
  • Nozzle ring segments or complete nozzle ring (especially for HFO operation).
  • Lubricating oil filter elements (if external oil pump/filter unit).
  • Overspeed trip sensor and solenoid valve (if applicable).

Safety

  • High surface temperatures of exhaust gas casings and piping, requiring proper insulation and warning signs.
  • High-speed rotating components (rotor) pose a severe hazard; never attempt to open while running or coasting.
  • Pressurized air and exhaust gas lines; ensure proper venting and depressurization before opening.
  • Risk of hot oil spray during maintenance if oil lines are not properly drained or isolated.
  • High noise levels requiring hearing protection in the vicinity of the turbocharger during operation.

Class survey

Class surveyors typically check the general external condition, cleanliness, and absence of leaks (oil, exhaust gas). They will review maintenance records, especially for bearing inspections and major overhauls. Operational parameters like exhaust gas temperatures, boost pressure, and vibration readings may be requested. If opened for inspection, bearing clearances (axial and radial play) will be measured and compared against limits. The overspeed trip mechanism and its last test date are also critical points of interest. Compliance with safety regulations regarding insulation and guarding is also verified.

Estimated lifetime: 100,000 - 150,000 hours with proper maintenance, regular overhauls, and timely component replacement. Major overhaul typically every 16,000-24,000 hours.

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