Engine
C145 bases on the proven concept of the Zongshen aero engine C115, Four-stroke, four cylinders, horizontally opposed turbocharged, air intake system with intercooler, Dual constant depression carburetors. The best power and high reliability, C145 aero engine can be applied to light-sport aircrafts, ultralight aircrafts, autogyros and light helicopters.
4-cylinder
4-stroke liquid-cooled engine with opposed cylinders
With turbo charger
With automatic waste gate control
Dry sump forced lubrication
with separate oil tank
Automatic adjustment
by hydraulic valve tappet
2 carburetors
Dual electronic ignition Electric starter
Propeller speed reduction gearbox
Engine mount assembly
Air intake system
Exhaust system
SFC at cruise: 285 g/kW.h
TBO 1000 h
WEIGHT | KG | |
Engine with propeller speed reduction gearbox i = 2.43 | 80 | |
Overload clutch | 1.6 | |
Engine suspension frame | 2.3 | |
PERFORMANCE | ||
106.6 kW | 145 hp | 5800 RPM |
TORQUE | ||
189 Nm | 4900 RPM | |
MAX RPM | 5800 RPM | |
BORE | STROKE | |
86 mm | 61.0 mm | |
DISPLACEMENT | FUEL | |
1417 cm³ | Min. RON 95 Mogas/ 100LL Avgas |
Fix-wing aircraft
light drone
Unmanned helicopter
Rotor aircraft