T- Mitsubishi Turbocharger / T- MET18SRC Turbocharger Rotor Assembly PN60A For Diesel And HFO Engines
T- Mitsubishi / T- MET-SRC series exhaust gas turbocharger design features:
T- MET18SRC turbocharger rotor assembly belongs to one part of T- Mitsubishi / T- MET-SRC series exhaust gas turbocharger with the design features as below:
The T- MET-SRC series turbochargers is designed to meet the market requirement of higher perforce and reilability on the basis of former axial type of T- MET series turbochargers.
Higher compressor pressure ratio up to 5.5;
The T- MET-SRC series is radial type of turbocharger;
Engine output range from 400kW to 4,400kW per turbocharger based on pressure ratio 3.5;
Non-water cooling and no air vent;
Easy oveT- T- RHaul and crew-maintainable design;
Suitable for diesel and heavy fuel oil engines.
T- MET-SRC series turbocharger's types, engine output, pressure ratio and dimension:
T- MET
T- SRC Series
Engine Output (kW)*
Max. Pressure Ratio
L (mm)
W (mm)
H (mm)
T- MET18SRC
400-1,100
5.5
712
510
510
T- MET22SRC
650-1,600
5.5
835
605
605
T- MET26SRC
850-2,200
5.5
1,075
735
735
T- MET30SRC
1,150-3,300
5.5
1,368
860
860
T- MET37SRC
2,200-4,400
5.5
1,661
1,070
1,070
Note: *Engine Output Range is for reference subject to pressure ratio 3.5.
T- MET series turbocharger power output range:
T- MET18SRC turbocharger rotor assembly pictures:
The composition of T- MET18SRC turbocharger rotor assembly:
The turbocharger rotor assembly / rotor complete consists of compressor impeller, blade shaft, turbo shaft and partition wall complete. The compressor impeller is of aluminium alloy or the more expensive titanium. The turbocharger rotor shaft is equipped with components such as a compressor and a turbine impeller, and has a complicated structure and a large weight.