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A100-M 100-M47

Turbocharger · Turbochargers

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

The ABB Turbocharging A100-M 100‑M47 is a high‑efficiency turbocharger designed for four‑stroke medium‑speed marine diesel engines up to about 8 MW, delivering compact power boost and reduced exhaust emissions.

Specifications

Technical data.reference — unverified

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Frame Size100-M47
Power max (kW)8000
Inspection

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Common issues

  • Bearing wear (journal and thrust) due to contaminated lube oil, insufficient flow, or high temperatures, leading to increased clearances and vibration.
  • Compressor and turbine fouling (deposits) reducing efficiency, increasing exhaust gas temperatures, and potentially causing surging.
  • Rotor imbalance and excessive vibration, often caused by uneven fouling, blade damage, or bearing wear.
  • Oil leakage from bearing housings (compressor or turbine side) indicating seal wear or pressure imbalances.
  • Cracks in turbine casing, exhaust gas manifold, or nozzle ring due to thermal stress and fatigue.
  • Surging during engine load changes, acceleration, or deceleration, often linked to fouling or incorrect engine tuning.
  • Damage or erosion to compressor impeller or turbine blades from foreign objects or abrasive particles.

Inspection checklist

  • Check bearing oil inlet/outlet pressures and temperatures against manufacturer's specifications. Look for deviations.
  • Inspect compressor and turbine wheels for fouling, erosion, or foreign object damage (FOD) via inspection ports. Note any significant deposits or blade damage.
  • Verify rotor axial and radial clearances (if accessible or during scheduled inspection) against wear limits. Typical axial clearance for A100-M is 0.15-0.30mm new.
  • Inspect bearing housing and associated piping for oil leaks, especially at the compressor and turbine side seals.
  • Check the condition of the air filter and exhaust gas silencer. Ensure no blockages or damage.
  • Verify the tightness of all mounting bolts and connections. Look for signs of fretting or movement.
  • Inspect exhaust gas casing, insulation, and associated ducting for cracks, hot spots, or signs of gas leakage.
  • Confirm proper operation of compressor water wash and turbine dry/wet wash systems, including nozzle condition and water/air supply.
  • Monitor turbocharger speed, boost pressure, and exhaust gas temperatures at various engine loads for consistency and adherence to engine maker's data.

Service intervals

Compressor Water WashDaily to Weekly (as per engine maker's recommendation and operational experience)
Turbine Dry/Wet WashWeekly to Monthly (as per engine maker's recommendation and operational experience)
Bearing Inspection/Renewal8,000 - 12,000 running hours (or annually, whichever comes first)
Rotor Inspection/Balancing16,000 - 24,000 running hours
Major Overhaul (full disassembly, inspection, renewal of wear parts)24,000 - 36,000 running hours

Typical wear limits

Rotor Axial ClearanceNew: 0.15 - 0.30 mm; Wear Limit: +0.10 mm from new (e.g., 0.25 - 0.40 mm)
Rotor Radial Clearance (Bearing Play)New: 0.20 - 0.40 mm; Wear Limit: +0.15 mm from new (e.g., 0.35 - 0.55 mm)
Bearing Shell Thickness/ConditionNo significant scoring, pitting, or delamination. Thickness reduction typically not exceeding 0.1 mm from new.
Shaft RunoutMaximum permissible runout typically 0.02 - 0.05 mm at specified points.
Blade Erosion/DamageMinor nicks/erosion acceptable within manufacturer's limits (e.g., depth < 10% of blade thickness, not affecting critical areas). Significant damage requires replacement or expert repair.
Nozzle Ring GapCheck for widening due to erosion; typically, max increase of 10-15% from new gap.

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 and pads).
  • Full set of O-rings, gaskets, and sealing rings for bearing housings and casings.
  • Oil filter elements (if the turbocharger has a dedicated lubrication system or fine filter).
  • Nozzle ring segments or complete nozzle ring (depending on design and wear).
  • Washing nozzles for compressor and turbine washing systems.
  • Sealing air labyrinth seals (if applicable).
  • Small repair kit for minor components (e.g., bolts, nuts, washers).

Safety

  • High surface temperatures of exhaust gas casing and associated piping (can exceed 400°C), posing severe burn hazards. Ensure insulation is intact.
  • High-speed rotating components (rotor operates at tens of thousands of RPM) – risk of severe injury or catastrophic failure if casing integrity is compromised or uncontained failure occurs.
  • High noise levels during operation (typically 100-120 dB), requiring hearing protection in the vicinity.
  • Pressurized air (boost air) and hot exhaust gas systems – ensure all connections are secure to prevent leaks and potential hazards.
  • Potential for uncontained failure (e.g., blade liberation) which can cause projectile hazards and significant damage to surrounding equipment and personnel.

Class survey

Class surveyors typically verify the following: 1. Maintenance records and service history (last major overhaul, bearing renewals, cleaning cycles). 2. Operational performance: observe boost pressure, exhaust gas temperatures, and turbocharger speed at various engine loads. 3. General condition: absence of oil leaks, cracks in casings/piping, secure mounting, and intact insulation. 4. Functionality of safety devices: overspeed trip, bearing temperature alarms (if fitted). 5. Integrity of exhaust gas system and air intake. 6. Availability of critical spare parts onboard. 7. Confirmation of compliance with manufacturer's service bulletins and recommendations.

Estimated lifetime: 24,000 - 36,000 running hours before major overhaul; total unit lifetime can exceed 80,000 hours with proper maintenance and multiple overhauls.

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