"> Accelleron A100-L
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Accelleron

A100-L

The Accelleron A100-L is an axial‑type turbocharger specifically engineered for low‑speed two‑stroke marine diesel engines, providing boost air across a wide range of fuel grades.

Per Hersteller-Datenblatt
Capacity
Exhaust gas / charge air
Medium

Inspector Detail ✓ verified

Common issues

  • Compressor-side fouling reducing charge-air pressure and efficiency, leading to higher exhaust temperatures.
  • Turbine-side deposit build-up from poor combustion or low-load operation, causing reduced turbine efficiency and increased exhaust back pressure.
  • Bearing wear (axial and radial) caused by contaminated or degraded lubricating oil, leading to increased clearances, vibration, and potential rotor damage.
  • Surging during rapid load changes, fouled air/gas path, or charge air cooler blockage, resulting in unstable operation and potential damage.
  • Exhaust gas leaks from turbine casing flanges, expansion bellows, or cracks due to thermal stress.
  • Charge air leaks from compressor casing, diffuser, or associated ducting, reducing engine performance.
  • Air filter clogging, restricting airflow to the compressor and leading to reduced charge air pressure and surging.
  • Overspeed trip malfunction, either failing to activate when required or causing false trips.

Inspection checklist

  • **Visual Inspection (External)**: Check for oil leaks (bearing housing, seals), exhaust gas leaks (flanges, bellows, casing cracks), and charge air leaks (ducts, cooler connections). Verify insulation integrity.
  • **Air Filter Condition**: Inspect for cleanliness, damage, and proper sealing. Clean or replace as necessary.
  • **Compressor Side Inspection**: Open inspection port (if available) or remove casing for visual check of impeller blades for fouling, erosion, foreign object damage (FOD), or rubbing marks. Inspect diffuser for deposits.
  • **Turbine Side Inspection**: Open inspection port (if available) for visual check of turbine blades for fouling, erosion, foreign object damage (FOD), or rubbing marks. Inspect nozzle ring for deposits, distortion, or damage.
  • **Bearing Condition (Operational)**: Monitor bearing temperatures (local gauges or remote monitoring), vibration levels, and lubricating oil pressure/flow. Listen for unusual noises. Check oil sample quality if possible.
  • **Rotor Free Rotation Check**: With engine stopped and turbocharger cooled, manually turn the rotor to check for free movement, absence of rubbing, and excessive axial/radial play.
  • **Overspeed Trip Mechanism**: Verify last test date and functionality. Conduct an annual test as per class requirements.
  • **Instrumentation & Alarms**: Check accuracy of pressure gauges (charge air, exhaust gas, lube oil) and temperature sensors. Verify alarm setpoints and functionality.
  • **Drainage Systems**: Ensure condensate drains from charge air cooler and gas side are clear and functional.

Service intervals

Routine Checks (Performance Monitoring, Visual Leaks) Daily/Weekly
Minor Inspection (Air Filter, Compressor Wash, External Cleaning) 2,000 - 4,000 running hours or 3-6 months
Intermediate Inspection (Bearing Inspection/Replacement, Rotor Cleaning, Nozzle Ring Inspection) 8,000 - 12,000 running hours or Annually
Major Overhaul (Full Strip-down, Rotor Balancing, Component Replacement) 16,000 - 24,000 running hours or 2-3 years
Bearing Replacement (Journal & Thrust) Typically every 12,000 - 16,000 running hours
Overspeed Trip Test Annually (Class requirement)

Typical wear limits

Axial Bearing Clearance New: 0.15 - 0.30 mm; Max. Worn: 0.40 - 0.50 mm
Radial Bearing Clearance New: 0.10 - 0.20 mm; Max. Worn: 0.25 - 0.35 mm
Rotor Shaft Run-out (at bearing journals) Max. 0.02 - 0.03 mm
Compressor Impeller Blade Tip Clearance Varies by design, typically 0.5 - 1.5 mm. Check for rubbing marks.
Turbine Blade Tip Clearance Varies by design, typically 0.8 - 2.0 mm. Check for rubbing marks.
Nozzle Ring Opening/Distortion Max deviation from new condition often 5-10% (measured with specific tooling or feeler gauges).
Rotor Unbalance (after balancing) Typically < 50 g.mm

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 bearing, bearing bushes)
  • Sealing Rings (Labyrinth seals for compressor and turbine sides)
  • Gasket & O-ring Kit (For all flanges, inspection covers, and service points)
  • Air Filter Elements (Sufficient quantity for routine replacement)
  • Overspeed Trip Components (e.g., shear pin, spring, or complete trip mechanism)
  • Lubricating Oil Filter Elements (If turbocharger has a dedicated lube oil system)
  • Nozzle Ring Segments or Complete Nozzle Ring (Depending on operational profile and budget)

Safety

  • **High Temperatures**: Exhaust gas temperatures (300-550°C) and hot casing surfaces pose severe burn hazards. Ensure all insulation and guards are intact and in good condition.
  • **High Rotational Speeds**: Rotor speeds up to 15,000-20,000 RPM. Risk of catastrophic uncontained failure if bearings fail, foreign objects enter, or rotor becomes unbalanced. Always use proper PPE.
  • **High Pressure**: Charge air system operates at significant pressure (2-5 bar). Leaks can cause injury. Ensure system is depressurized before opening.
  • **Noise**: High noise levels during operation require mandatory hearing protection in the vicinity of the turbocharger.
  • **Hot Work/Entry**: Never open casings or perform maintenance while the engine is running or hot. Allow sufficient cooling time and ensure engine is secured against accidental start.

Class survey

A class surveyor typically checks the following: 1. **Maintenance Records Review**: Verification of scheduled maintenance, repairs, and component replacements as per Accelleron's manual and class requirements. 2. **Performance Log Analysis**: Review of operational parameters (turbocharger RPM, charge air pressure/temp, exhaust gas temp, lube oil pressure/temp) to identify trends, deviations, or signs of distress. 3. **External Condition Check**: Inspection for visible leaks (oil, exhaust gas, charge air), signs of overheating, cracks, or damage to casings, insulation, and mounting. 4. **Overspeed Trip Test Verification**: Confirmation that the overspeed trip device has been tested annually and functions correctly, often requiring documentation or witnessing of the test. 5. **Bearing Condition (if accessible/monitored)**: Review of bearing temperature and vibration monitoring data. In some cases, a visual check of bearing housing for leaks or unusual wear. 6. **Charge Air Cooler Condition**: Often inspected in conjunction with the turbocharger, checking for cleanliness, leaks, and proper drainage. 7. **Safety Devices**: Confirmation of proper guarding, insulation, and alarm functionality associated with the turbocharger. 8. **Spare Parts Inventory**: May inquire about the availability of critical spare parts onboard as per manufacturer's recommendations and class requirements.

Estimated lifetime: 80,000 - 120,000 running hours (with regular maintenance and scheduled major overhauls)

Components & Design

Component data being added…

Technical Data

turbine type Axial
engine type 2-stroke

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Common failures & inspection points

Compressor-side fouling reducing charge-air pressure
Turbine-side deposit build-up from poor combustion or low-load operation
Bearing wear caused by contaminated or degraded lubricating oil
Surging during rapid load changes or fouled air/gas path

Service & Maintenance

Maintenance per manufacturer manual and classification society requirements. Annual inspection at class survey. Stock spare parts per manufacturer specification.

Suppliers & Spare Parts

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Replacement Parts

Typical service spares include bearing set, sealing rings, nozzle ring, compressor wheel, turbine blades and complete cartridge/rotor assembly depending on OEM service concept.
Equipment Model #36953 · ✓ still in production