Introducing the PT1-124,a state-of-the-art hybrid drone propulsion system that combines a 2-stroke single-cylinder engine with an 11 kW booster-generator. This unit is specifically engineered for vertical takeoff and landing (VTOL) unmanned aerial vehicles (UAVs) that demand considerable electrical power, allowing for prolonged flight at steady speeds.
Equipped with a durable twin contour liquid cooling mechanism, electronic fuel injection, and a built-in gearbox transmission featuring an idle clutch, the PT1-124 ensures optimal performance and reliability.
Adhering to the stringent standards of ASTM F3366-19 and EU Regulation 2018/1139, this propulsion unit guarantees exceptional safety and efficiency.
key Specifications:
| Dimensions (L x W x H) | 450 x 300 x 150 mm |
| Weight | 8.9 kg |
| Displacement | 124 cc |
| Bore | 54 mm |
| stroke | 54 mm |
| Power Output | 29 hp @ 8800 rpm |
| Maximum Continuous Speed | 10,000 rpm |
| Fuel Efficiency | 200 – 220 g/kW/hr |
