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AT AT-14

Turbocharger · Turbochargers

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

IHI Marine AT AT-14 — AT, 5000 kW max.

Specifications

Technical data.reference — unverified

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Frame SizeAT-14
Power max (kW)5000
Inspection

Inspector Detail ✓ verified

Common issues

  • Bearing wear and failure (journal and thrust bearings) due to contaminated oil, insufficient lubrication, or imbalance.
  • Compressor fouling leading to reduced air flow, surging, and decreased engine performance.
  • Turbine fouling (carbon deposits) and erosion (due to abrasive particles or high-temperature corrosion) causing reduced efficiency and potential blade damage.
  • Oil leakage from compressor or turbine side seals, indicating seal wear or bearing issues, leading to oil consumption and potential engine intake/exhaust contamination.
  • Rotor imbalance causing excessive vibration, accelerated bearing wear, and potential damage to the compressor/turbine wheels or casing.
  • Cracks in the turbine casing or exhaust gas inlet/outlet ducts due to thermal stress or vibration.
  • Nozzle ring distortion or damage, affecting exhaust gas flow to the turbine and reducing efficiency.
  • Loss of boost pressure due to internal leakage, fouling, or mechanical damage.

Inspection checklist

  • Check for abnormal noise or vibration during operation (use a stethoscope or vibration meter).
  • Inspect oil inlet and outlet lines for leaks, proper flow, and oil condition (discoloration, presence of water/carbon).
  • Monitor boost pressure and exhaust gas temperatures (before and after turbine) for deviations from normal operating parameters.
  • Inspect the compressor wheel and diffuser for fouling, rub marks, foreign object damage (FOD), and blade integrity (if accessible via air filter removal).
  • Inspect the turbine wheel and nozzle ring for fouling, erosion, and damage (requires opening, but external signs like exhaust temperature spread can indicate issues).
  • Check the turbocharger casing for cracks, loose bolts, proper insulation, and secure mounting.
  • Verify cooling water flow and temperature (if water-cooled) and inspect for leaks.
  • Inspect the air filter element for cleanliness and integrity; ensure proper sealing.
  • Check drain lines from the turbocharger for blockages or restrictions.

Service intervals

Routine operational checks (noise, vibration, temperatures, pressures)Daily/Weekly
Compressor side cleaning (dry or wet washing)1,000 - 2,000 running hours (or as indicated by performance drop)
Turbine side cleaning (water washing)500 - 1,000 running hours (depending on fuel quality and engine load)
Bearing inspection and replacement (cartridge type)8,000 - 12,000 running hours
Major overhaul (rotor balancing, casing inspection, nozzle ring/diffuser inspection/replacement)16,000 - 24,000 running hours

Typical wear limits

Rotor axial play (new)0.10 - 0.20 mm
Rotor axial play (service limit)0.30 - 0.40 mm
Rotor radial play (new)0.05 - 0.10 mm
Rotor radial play (service limit)0.15 - 0.20 mm
Compressor/Turbine blade tip clearanceSpecific to model, typically 0.3 - 0.6 mm (check for rub marks indicating excessive play or imbalance)
Bearing shell thicknessRefer to manufacturer's manual for specific minimum thickness; typically, wear beyond 10-15% of original thickness is critical.
Nozzle ring openingCheck for carbon build-up reducing effective area; distortion or cracks are critical.

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

Critical spares

  • Complete bearing cartridge assembly (including journal and thrust bearings, seals)
  • Oil seals and O-rings (especially for cooling water connections if applicable)
  • Nozzle ring assembly (or segments, depending on design)
  • Diffuser
  • Compressor wheel nut
  • Gasket sets for casing joints and exhaust connections
  • Air filter elements

Safety

  • High temperatures: Exhaust gas and casing surfaces can reach extreme temperatures (300-600°C), posing severe burn hazards. Ensure insulation is intact.
  • High rotational speeds: The rotor operates at very high RPMs (e.g., 20,000-60,000 RPM). Catastrophic failure can result in flying debris.
  • Pressurized air and exhaust gas: Ensure all connections are secure and relief valves (if fitted) are operational.
  • Hot oil: Lubricating oil can be very hot and under pressure. Exercise caution during oil system checks.
  • Potential for casing rupture: While rare, extreme overspeed or internal explosion (e.g., due to unburnt fuel in exhaust) can lead to casing rupture. Ensure exhaust gas temperatures are monitored.

Class survey

A class surveyor will typically verify the turbocharger's maintenance records, including dates of bearing replacements, major overhauls, and routine cleaning. They will conduct an external visual inspection for oil leaks, cooling water leaks, cracks in casings or exhaust ducts, proper insulation, and secure mounting. During engine operation, they will observe for abnormal noise, vibration, and verify operational parameters like boost pressure and exhaust gas temperatures. If the turbocharger has been opened for maintenance, the surveyor may request to inspect internal components such as bearings, rotor, nozzle ring, and diffuser for condition and adherence to wear limits. They will also confirm the integrity of the air intake filter system and exhaust gas system.

Estimated lifetime: 16,000 - 24,000 running hours before major overhaul; total design life of main casings and structural components can exceed 80,000 - 100,000 hours with proper maintenance and component replacement.

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