Product Description
ZS115 aero engine is a widely used turbocharged aircraft engine for ultralight and light-sport aircrafts as well as medium altitude long endurance unmanned aerial vehicles. ZS115 offers more performance at high altitude and the best power to weight ratio at better than 1.134 kW/kg.
Applications:
700kg-1200kg fixed wing UAV, 500kg UAV Helicopters and rotorcraft, etc.
Product Advantages：
4-cylinder
4-stroke liquid-/air-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
TBO 2,000 h
4-stroke liquid-/air-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
TBO 2,000 h
Technical Parameters
WEIGHT |
KG |
|
| Engine with propeller speed reduction gearbox i = 2.43 | 74.5 | |
| Overload clutch | 1.6 | |
| Engine suspension frame | 2.3 | |
| PERFORMANCE | ||
| 84.5 kW | 115 hp | 5800 RPM |
| TORQUE | ||
| 140 Nm | 4900 RPM | |
| MAX RPM | 5800 RPM | |
| BORE | STROKE | |
| 79.5 mm | 61.0 mm | |
| DISPLACEMENT | FUEL | |
| 1211.2 cm³ | Min. RON 95 Mogas/ 100LL Avgas | |
External characteristic curve
Height characteristic curve
