"> MAN Energy Solutions MAN TCR18
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MAN Energy Solutions

MAN TCR18

The MAN TCR18 is a radial‑flow marine turbocharger that delivers boost for medium‑speed diesel engines (600–6,850 kW) with a high‑speed rotor (>150 000 rpm) and DLC‑coated hydrodynamic glide bearings.

MAN Energy Solutions MAN TCR18
Per Hersteller-Datenblatt
Capacity
HFO / VLSFO / MGO
Medium

Inspector Detail

Common issues

  • Bearing wear (thrust and journal bearings) due to high rotational speeds, insufficient lubrication, or contamination, leading to increased axial/radial play and potential shaft damage.
  • Fouling of compressor wheel and diffuser by oil mist or airborne contaminants, reducing efficiency and potentially causing surging.
  • Fouling and erosion of turbine blades and nozzle ring by exhaust gas particulates and high temperatures, leading to reduced power output and increased exhaust gas temperatures.
  • Corrosion of casing components (especially compressor casing and water-cooled sections) due to saltwater exposure or condensation, compromising structural integrity and sealing.
  • Malfunction of electronic control components (e.g., speed sensors, actuators for variable turbine geometry if fitted) due to vibration, moisture ingress, or aging, affecting turbocharger performance and engine control.
  • Oil leakage from bearing housing seals, indicating seal wear or excessive bearing play, leading to oil consumption and potential fire hazard.
  • Cracks in turbine casing or exhaust gas manifold connections due to thermal stress and vibration, causing exhaust gas leaks and reduced efficiency.

Inspection checklist

  • Check axial and radial play of the rotor shaft (cold and warm if possible) against manufacturer's limits. Typical new axial play: 0.1-0.3 mm, service limit: 0.4-0.6 mm. Radial play: 0.08-0.2 mm, service limit: 0.3-0.4 mm.
  • Visually inspect compressor wheel for fouling, erosion, bent blades, or foreign object damage (FOD). Check for rubbing marks on the casing.
  • Visually inspect turbine blades and nozzle ring (if accessible without full disassembly) for fouling, erosion, cracks, or signs of overheating. Check for free movement of nozzle ring segments if VGT equipped.
  • Inspect turbocharger casing for external cracks, exhaust gas leaks, oil leaks, and secure mounting bolts. Check condition of insulation blankets.
  • Verify lubricating oil supply and drain lines for leaks, proper flow, and cleanliness. Check oil pressure and temperature at turbocharger inlet.
  • Inspect air filter condition and ensure air intake is clear. Check functionality of water washing system (if fitted).
  • Check functionality of overspeed trip device (if mechanical) or verify speed sensor readings against engine RPM. Inspect actuator for variable turbine geometry (if fitted) for smooth operation.
  • Monitor exhaust gas temperatures before and after the turbine, and boost pressure, comparing to engine load and historical data for performance deviations.
  • Check condition of vibration dampers and mounting feet for signs of wear or damage.

Service intervals

Minor Inspection (e.g., cleaning, bearing check) 4,000 - 8,000 running hours or annually
Major Overhaul (e.g., complete disassembly, bearing replacement, rotor balancing) 16,000 - 24,000 running hours or every 3-5 years
Class Survey Inspection Annually

Typical wear limits

Axial Rotor Play Max. 0.4 - 0.6 mm (refer to specific MAN TCR18 manual for exact value)
Radial Rotor Play Max. 0.3 - 0.4 mm (refer to specific MAN TCR18 manual for exact value)
Compressor Blade Tip Clearance Specific to model, typically 0.5 - 1.5 mm, check for rubbing marks indicating excessive play or deformation.
Turbine Blade Erosion/Cracks Any visible cracks or significant erosion (>10-15% material loss) on blades or nozzle ring requires replacement.
Shaft Run-out Max. 0.02 - 0.05 mm (measured at specific points, refer to manual).

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

Critical spares

  • Complete bearing cartridge assembly (thrust and journal bearings)
  • Set of O-rings and gaskets for casing and oil lines
  • Oil filter elements (if applicable to turbocharger's oil system)
  • Speed sensor and associated wiring
  • Nozzle ring segments (if VGT type and prone to wear/fouling)
  • Actuator repair kit (if VGT type)
  • Compressor wheel nut and locking washer

Safety

  • High surface temperatures (up to 500°C on turbine casing) posing severe burn hazards. Ensure insulation is intact.
  • High-speed rotating components (up to 60,000-100,000 RPM) present a risk of disintegration if bearings fail or foreign objects enter, leading to catastrophic damage and potential injury.
  • High noise levels (100-120 dB) requiring hearing protection in the vicinity during operation.
  • Risk of exhaust gas leaks (CO, NOx) from casing or manifold connections, leading to asphyxiation or fire hazard in enclosed spaces.
  • Oil leaks from bearing housing can create slip hazards and increase fire risk on hot surfaces.

Class survey

The class surveyor will typically review maintenance records, running hours, and any reported defects. They will conduct an external visual inspection for leaks (oil, exhaust gas), cracks, and secure mounting. Key checks include verifying rotor axial and radial play, inspecting the condition of the air filter, checking the functionality of the overspeed trip device (if fitted), and confirming the integrity of the lubricating oil system and cooling water connections. Performance parameters like boost pressure and exhaust gas temperatures may be reviewed against design values. The surveyor will also ensure compliance with fire safety regulations regarding insulation and oil containment.

Estimated lifetime: 100,000 - 150,000 running hours before major component replacement (e.g., rotor shaft, casings), assuming regular maintenance and overhauls at specified intervals.

Components & Design

Component data being added…

Technical Data

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Common failures & inspection points

Radial bearing clearance excessive (>5 μm or visible axial displacement)

Measure axial rotor displacement with slide caliper; 'white-line method': paint white line on shaft, attach magnetic base with electrode, run motor ahead/astern, measure line distance with slide caliper. Should be <0.5 mm (new), max 2 mm. Replace bearing if exceeded.

Compressor/turbine fouling from soot deposits or seawater salt; reduced performance

Visual: inspect black/brown deposits on compressor/turbine blades. Elevated oil outlet temperature. Action: perform water/oil washing procedure. Wash compressor side at ~full load, turbine side at 20–40% load with demineralized water (recommended every 200–250 operating hours). Monitor drain water: clear water = light fouling; dark/granular residue = heavy deposits → more frequent washing required.

Surging (high-frequency pulsation, noise from compressor; air flow reversal at nozzle ring fouling)

Acoustic/RPM: high-frequency whistling/vibration from turbocharger compressor side during part load. RPM monitoring (magnetic sensor on rotor shaft, rpm indicator T110 type). Temperature measurement: dual thermocouple (different response times) in compressor inlet for surging detection through rapid temperature spikes. Inspect nozzle ring for blockage/slagging. After surging: stop engine, check compressor wheel for foreign object damage (FOD analysis). Contact: MAN TC-ASB-Feedback@man-es.com for damage images.

Ölverschmutzung/Wassereintritt in Lagersystem; korrodierte Lager, Lecks

Analyse oil samples: viscosity (±1 grade tolerated), water content <0.2% weight (critical >0.5%), contamination ≤2% weight. Check oil colour & consistency (dark/sludgy oils indicate overheating/contamination). Bearing system before servicing: flush oil backwards (reverse-flushing). Check oil inlet/outlet pipes for corrosion/deposits. Inspect bearing bushes for scratches/discolouration. Open oil drain valves before washing procedures to monitor drain water.

Bearing shell wear or bearing clearance outside tolerance (axial >2 mm, radial >5 μm); rotor binding

Axial clearance measurement: rotate rotor by hand (engine stopped) — should move easily without binding. Caliper: measure bearing bush inner diameter with slide caliper/gauge, compare with shaft outer diameter. Should yield clearance of 0.08–0.18 mm (typically 0.10–0.18 mm for plain bearings). Inspect bearing bushes for scratches/grooves through DLC coating (dark grey/black surface normal). If exceeded: replace bearing bushes/bearing shell.

Turbineneinlass-Temperatur abnormal hoch (>450°C), Abgaslecks; Lagergehäuse-Temperatur überhöht

Measure with thermometer/infrared pyrometer at turbine outlet pipe & bearing housing surface. Normal: ~350–380°C turbine inlet, bearing housing <150°C surface temperature at full load. Elevated values → compressor fouling, nozzle ring blockage or internal leak in rotor housing. Check housing for cracks/leaks (sooty spots indicate leaks). Temperature trend monitoring: sudden spikes = maintenance trigger.

Type-general inspection and maintenance points for this equipment category — not model-specific.

Service & Maintenance

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

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Replacement Parts

Spare parts via MAN Energy Solutions SE or approved distribution partners. Lead time: 2-6 weeks.
Equipment Model #1783 · ✓ still in production