A super light 2-stroke single cylinder internal combustion hybrid engine with a compact integrated 22 kW generator,
Highly effective for sustained operation at constant speeds. Built for helicopter-type UAVs with electrical transmission.
| Engine type | Hybrid, 2-stroke, 1 cylinder |
| Weight | 14 kg |
| Displacement | 124 cc |
| Length/Wiath/Height | 450x300x150 mm |
| Bore | 54 mm |
| Stroke | 54 mm |
| Power | 22kW at 8800 rpm |
| Maximum Continuous Speed | 10000 rpm |
| Ignition | Electronic CDI. Twin spark plug. Variable ignition front |
| Cooling | Liquid cooling, pressured thermostated system with external electric cooling pump and radiators |
| Fuel system | Electronic Fuel Two Stage Injection Throttle body + Transfer port |
| Fuel type | Wide range of automotive and aviation gas, 2% premix w/TS Oil. External lubrication system options available |
| Fuel consumption | 200 – 220 g / kW / hr |
| TBO (estimate) | API TC |
| Preferred oil type | Up to 500 hours |
| Fuel to oil mixture | Premix 2%, Automix – 0,5-1% |
| Sensors / Telemetry | EGT – Exhaust gas temperature; CHT – Cylinder head temperature; CLT – Cooling liquid temperature; IAT – Intake air temperature; RPM – Rotation per mine; CSP – Crankshaft Position; KS – Knock sensor; Airflow, Throttle position, Fuel Flow |
| Control | CAN 2.0B J1339/29bit; ADLM + TrueTorgue |
| Electric System | Internet alternator / starter; Internal starter battery pack 5Ah |
Please fill in the form below or contact us using the details at the bottom of the page