"> Everllence TCA88
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Everllence

TCA88

The Everllence TCA88 is an axial‑flow marine turbocharger originally developed by MAN (TCA series) for medium‑speed diesel engines, providing boost pressure to improve engine power and fuel efficiency.

Per Hersteller-Datenblatt
Capacity
Exhaust gas / charge air
Medium

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Common issues

  • Heavy turbine-side fouling, especially during low-load or transient operation, leading to reduced efficiency, increased exhaust back pressure, and potential surging.
  • Compressor diffuser and volute contamination (e.g., oil mist, dust), impacting air flow, compressor efficiency, and potentially causing surging.
  • Bearing and thrust bearing wear, indicated by increased rotor axial and radial clearances, elevated vibration levels, or abnormal oil analysis results.
  • Rotor imbalance after deposit shedding (e.g., carbon deposits from turbine side), causing significant vibration, noise, and accelerated bearing wear.
  • Oil leakage from bearing casings, seal rings, or oil supply/drain lines, leading to excessive oil consumption and potential contamination of air/gas streams.
  • Exhaust gas leakage from casing joints, expansion bellows, or insulation defects, posing fire hazards, reducing efficiency, and creating hot spots.
  • Foreign Object Damage (FOD) to compressor or turbine blades, leading to imbalance, efficiency loss, and potential catastrophic failure.
  • Surging, often a symptom of severe fouling, engine combustion issues, or improper operation.

Inspection checklist

  • Check rotor axial and radial clearances (free play) using a dial gauge; compare measurements against manufacturer's new and wear limits.
  • Visually inspect turbine and compressor blades for fouling, erosion, cracks, bending, or foreign object damage (FOD). Pay close attention to blade tips and roots.
  • Inspect compressor diffuser and nozzle ring for fouling, damage, cracks, or excessive wear/deformation.
  • Check for oil leaks from bearing housings, oil supply/drain lines, and gas leaks from casing joints, expansion bellows, or insulation.
  • Inspect exhaust gas casing and insulation for cracks, hot spots, discoloration, or signs of overheating.
  • Verify condition of air filter elements and ensure clean air supply to the compressor. Check for signs of oil ingress.
  • Check condition of expansion bellows for cracks, thinning, signs of fatigue, or excessive movement.
  • Monitor turbocharger vibration levels (if sensors are fitted) and listen for unusual noises (e.g., rubbing, whistling, knocking) during operation.
  • Inspect turbocharger mounting bolts, chocks, and foundations for security, signs of fatigue, or corrosion.

Service intervals

Routine operational checks Daily/Weekly (e.g., visual inspection, noise, vibration, temperatures)
Minor inspection (bearings, cleaning, rotor clearance check) 4,000 - 8,000 running hours (or annually, whichever comes first)
Major overhaul (rotor out, full inspection, balancing, component replacement) 16,000 - 24,000 running hours (or every 3-5 years, depending on operating profile and fuel)
Annual inspection As per Class Survey requirements

Typical wear limits

Rotor axial clearance (cold) New: 0.25 - 0.40 mm; Wear Limit: +0.15 mm from new (e.g., 0.40 - 0.55 mm). Exceeding this indicates thrust bearing wear.
Rotor radial clearance (cold) New: 0.35 - 0.50 mm; Wear Limit: +0.15 mm from new (e.g., 0.50 - 0.65 mm). Exceeding this indicates radial bearing wear.
Bearing shell thickness Manufacturer's specified minimum thickness (e.g., 0.5 mm below nominal). Check for signs of scoring or pitting.
Turbine/Compressor blade tip clearance Visual inspection for rubbing marks on casing. Specific measurement values are manufacturer-dependent (e.g., 0.5 - 1.0 mm new).
Nozzle ring gap Visual inspection for excessive erosion, deformation, or carbon build-up. Manufacturer specific limits apply for replacement.

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

Critical spares

  • Bearing shells (radial and thrust bearings) - complete sets.
  • Gasket sets and O-rings (especially for casing joints, oil lines, and seal rings).
  • Oil filter elements (if applicable for dedicated turbocharger lube oil system).
  • Nozzle ring segments (if replaceable and prone to wear/fouling, often kept as a set).
  • Locking plates, washers, and specialized fasteners for critical connections.
  • Cleaning agents and equipment for compressor and turbine washing (onboard cleaning kits).
  • Air filter elements (if applicable for turbocharger intake).

Safety

  • High surface temperatures of exhaust gas casing and associated piping (exceeding 200°C) – severe risk of burns and potential fire hazard if insulation is damaged or oil leaks occur.
  • High-speed rotating machinery (rotor operating at tens of thousands of RPM) – potential for catastrophic uncontained failure if maintenance is neglected or severe imbalance occurs.
  • Pressurized air (up to 5 bar) and hot exhaust gas (up to 400°C) – risk of injury from sudden release or leakage during operation or maintenance.
  • Hot lubricating oil – risk of burns during maintenance or from leaks, and potential for oil mist fires.
  • High noise levels (often exceeding 100 dB) – requires mandatory hearing protection in the vicinity during operation.

Class survey

Class surveyors typically review the turbocharger's maintenance records, running hours, and previous survey reports. They will conduct a thorough visual inspection for external condition, signs of leaks (oil/gas), and integrity of insulation. Critical checks often include witnessing rotor axial and radial clearance measurements, inspecting bearing condition (if opened for maintenance), and verifying the functionality of safety devices such as the overspeed trip and associated alarms. The overall operational performance, compliance with manufacturer's service recommendations, and the condition of exhaust gas piping and expansion bellows are also assessed.

Estimated lifetime: 100,000+ running hours for the main rotor assembly (shaft, turbine, compressor wheel) with diligent maintenance and no catastrophic damage. However, a comprehensive major overhaul and refurbishment cycle is typically performed every 16,000-24,000 running hours.

Components & Design

Component data being added…

Technical Data

former brand MAN
series TCA
turbine type Axial

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Common failures & inspection points

Heavy turbine-side fouling on low-load operation
Compressor diffuser contamination
Bearing and thrust bearing wear
Rotor imbalance after deposit shedding

Service & Maintenance

Wartung per Hersteller-Handbuch und Klassifikationsgesellschafts-Anforderungen. Jährliche Inspektion bei Class Survey. Ersatzteile per Herstellerangabe bevorraten.

Suppliers & Spare Parts

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Replacement Parts

Large-frame TCA spares should be planned well ahead; nozzle ring, bearings, seals and exchange rotor are critical items.
Equipment Model #36975 · discontinued