Optimal Choice for Light Aircraft, Trainer Aircraft, and Small UAVs
| Component | Size | Material | Temperature Range |
|---|---|---|---|
| Cylinder Assembly | Diameter 80–150mm | Aluminum alloy, cast iron | 100°C to 300°C |
| Moving Parts | Piston diameter 80–140mm | Aluminum alloy, alloy steel | 100°C to 400°C |
| Fuel and Ignition System | Spark plug length 80–120mm | Ceramic, copper alloy | -40°C to 800°C |
| Cooling System | Radiator size 300×400mm | Aluminum alloy, copper | -40°C to 150°C |
| Lubrication System | Oil sump capacity 3–10L | Aluminum alloy, alloy steel | -40°C to 150°C |
Product Features
- Power Output: 50 ~ 350 shp
- Ignition System: Electronic fuel injection with dual-spark ignition
- Cooling Options: Air-cooled / Liquid-cooled configurations available
- Fuel Compatibility: Supports both gasoline and aviation kerosene
Manufacturing and Optimization Capabilities
- Full in-house development of pistons, connecting rods, and crankshafts
- Lightweight cylinder block design
- ECU tuning and electronic ignition system optimization
- Complete traceability and batch management for all components
Application Scenarios
- Light general aviation aircraft
- Trainer aircraft and UAV platforms
- Hybrid auxiliary power systems for aircraft