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A200-L 200-L37

Turbocharger · Turbochargers

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

The ABB A200‑L 200‑L37 is a high‑capacity two‑stroke slow‑speed marine turbocharger designed to boost the performance of large diesel main engines up to about 60 MW.

Specifications

Technical data.reference — unverified

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Frame Size200-L37
Power max (kW)60000
Inspection

Inspector Detail ✓ verified

Common issues

  • Bearing wear and failure (journal and thrust bearings) due to lubrication issues, contamination, or excessive vibration, leading to increased clearances and potential rotor damage.
  • Compressor side fouling (dirt, oil mist, salt deposits) leading to reduced efficiency, surging, increased exhaust gas temperatures, and higher fuel consumption.
  • Turbine side fouling (soot, unburnt fuel particles, vanadium deposits) on nozzle ring and blades, causing reduced efficiency, increased exhaust back pressure, and potential blade erosion/corrosion.
  • Rotor imbalance and vibration, often caused by blade damage, uneven fouling, or bearing wear, leading to increased stress on bearings and potential catastrophic failure.
  • Oil leakage from bearing housings, often due to worn labyrinth seals, incorrect oil pressure, or blocked drain lines, posing fire risk and performance degradation.
  • Exhaust gas leakage from casing joints, expansion bellows, or drain pipes, leading to energy loss, hot spots, and potential hazards in the engine room.
  • Turbocharger surging, indicated by unstable operation, fluctuating pressures, and characteristic 'whooshing' sounds, often due to engine load changes, fouling, or air filter blockage.
  • Speed sensor malfunction or inaccuracy, leading to incorrect speed readings, overspeed trip failures, or performance monitoring issues.

Inspection checklist

  • External visual inspection for oil leaks, exhaust gas leaks, signs of overheating, cracks on casings, and general cleanliness around the unit.
  • Check rotor free rotation (if safe and engine stopped) and manually check axial/radial clearances (if accessible and specified by manufacturer's procedure).
  • Inspect air filter condition for blockage or damage; ensure charge air cooler is clean and free of leaks on both air and water sides.
  • Check lubricating oil system: oil pressure, temperature, level, and condition (via sight glass or lab analysis). Inspect oil lines for leaks or damage.
  • Monitor turbocharger speed, exhaust gas temperatures (inlet/outlet), and charge air pressure for deviations from normal operating parameters and trends.
  • Listen for abnormal noises (whining, grinding, surging sounds) and check for excessive vibration using a portable vibration meter, comparing to baseline data.
  • Inspect turbine and compressor blades (via inspection ports, if available) for fouling, erosion, corrosion, or impact damage.
  • Verify proper functioning of the overspeed trip mechanism and associated alarms during routine tests as per PMS.
  • Check integrity of expansion bellows on exhaust gas inlet/outlet and charge air piping for cracks, leaks, or signs of fatigue.
  • Ensure all drains (oil, water) from the turbocharger are clear and functioning correctly, especially the exhaust gas casing drains.

Service intervals

Minor inspection and cleaning (compressor wash, visual checks, oil sample)4,000 - 8,000 running hours
Intermediate inspection (bearing inspection/replacement, nozzle ring cleaning, gas side cleaning)12,000 - 16,000 running hours
Major overhaul (rotor balancing, full bearing replacement, comprehensive cleaning/inspection of all components)24,000 - 36,000 running hours
Complete overhaul/factory service (if required, depending on condition and accumulated hours)48,000 - 72,000 running hours

Typical wear limits

Journal BearingsRadial clearance exceeding manufacturer's specified maximum (e.g., >0.15-0.25 mm) or signs of scoring, pitting, or material fatigue on bearing surfaces.
Thrust BearingsAxial clearance exceeding manufacturer's specified maximum (e.g., >0.20-0.30 mm) or visible wear/damage to thrust pads and collar.
Rotor ShaftRunout exceeding 0.02-0.05 mm TIR (Total Indicator Reading) at bearing journals, or visible scoring/grooves that cannot be polished out.
Compressor/Turbine BladesErosion or corrosion reducing blade thickness by more than 10-15%, presence of cracks, or significant impact damage (e.g., foreign object damage).
Nozzle RingDistortion, cracking, or increased gap between segments exceeding manufacturer's limits, leading to inefficient gas flow and reduced turbocharger performance.
Labyrinth SealsExcessive wear or damage causing increased oil consumption, reduced sealing air effectiveness, or gas leakage into the bearing housing.

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

Critical spares

  • Complete bearing cartridge assembly (journal and thrust bearings)
  • Set of labyrinth seals (compressor and turbine side)
  • O-ring and gasket kit for casing joints and inspection covers
  • Turbocharger speed sensor
  • Air filter elements (if applicable, for intake silencer)
  • Lubricating oil filter elements (if external oil filter is used)
  • Nozzle ring segments (if modular design and prone to damage/fouling)
  • Emergency repair kit for minor casing cracks (e.g., high-temperature sealant/putty)

Safety

  • High-temperature surfaces (exhaust gas casing, turbine outlet, gas pipes) posing severe burn hazards. Always use appropriate PPE and allow for sufficient cooling before inspection/maintenance.
  • High-speed rotating machinery: Risk of severe injury from contact with rotating parts or from catastrophic disintegration due to overspeed, severe imbalance, or material failure.
  • High noise levels (typically 100-120 dB) requiring mandatory hearing protection during operation and maintenance in proximity.
  • Pressurized systems (exhaust gas, charge air, lubricating oil) can cause injury if released suddenly or if components fail under pressure. Ensure systems are depressurized before opening.
  • Oil mist and leakage: Potential fire hazard, especially in hot engine room environments. Ensure proper sealing, ventilation, and immediate cleanup of any oil spills.

Class survey

Class surveyors typically focus on: 1. Review of maintenance records, running hours, and previous survey reports to confirm adherence to the Planned Maintenance System (PMS) and manufacturer's recommendations. 2. External inspection for leaks (oil, gas), signs of overheating, securing arrangements, and general condition of the turbocharger and its associated piping. 3. Verification of safety devices, particularly the overspeed trip mechanism and associated alarms, including functional testing if required by class rules or PMS. 4. Monitoring of operational parameters (speed, temperatures, pressures) to ensure stable and efficient performance within design limits. 5. Assessment of vibration levels, often requiring a vibration analysis report. 6. Inspection of exhaust gas piping, expansion bellows, and charge air system for integrity, signs of corrosion, or cracks. 7. Lubricating oil system integrity, oil quality, and alarm functions. 8. Opening for internal inspection of turbine and compressor sides (e.g., nozzle ring, blades, bearings) may be required based on accumulated running hours, condition-based monitoring results, or specific class society rules.

Estimated lifetime: 100,000 - 150,000 running hours (for main casing and rotor assembly, assuming regular scheduled overhauls, component replacements, and adherence to maintenance guidelines)

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