PT2-124
A hybrid twin-engine motorunit for UAVsTwin-engine power plant with the integrated transmission. Electronically synchronized rotation of coaxial rotors.
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Twin-engine power plant with the integrated transmission. Electronically synchronized rotation of coaxial rotors.
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Each of two engine is 124cc 29hp—two-stroke with fuel injection and liquid cooling. An 11kw generator/booster/starter is integrated into the engine crankshaft. Reducer with a gear ratio of 1:5. Idling clutch. Duplicated cooling systems (two pumps for each of the dual cooling loops.). Dual ignition systems, two spark plugs per cylinder, two coils, and two controllers per cylinder.

| Engine type (each of two) | Hybrid, 2-stroke, 1 cylinder |
| Weight | 23.5 kg |
| Displacement | 124 cc |
| Length/Width/Height | 600x600x300 |
| Bore | 54 mm |
| Stroke | 54 mm |
| Power (total) | 55 hp at 8800 rpm |
| Maximum Continuous Speed | 9550 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 | JP8, Jet-A1, F54 |
| Fuel consumption | 200 – 220 g / kW / hr |
| TBO (estimate) | 1000h |
| Preferred oil type | API TC |
| 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 |

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