Powering Fixed-Wing UAVs, Short-Haul Transport, and Agricultural Aircraft
| Component | Size | Material | Temperature Range |
|---|---|---|---|
| Air Intake System | Intake duct diameter 400–900mm | Composite materials, aluminum alloy | -50°C to 150°C |
| Compressor and Combustion Chamber | Shaft length 600–1200mm | Nickel-based alloy, titanium alloy, ceramic coating | 400°C to 1500°C |
| Turbine System | Blade length 50–200mm | High-temperature alloy | 1000°C to 1700°C |
| Reduction Gear and Propeller Control | Reduction gear diameter 300–700mm | Alloy steel, titanium alloy | 50°C to 400°C |
| Auxiliary Piping and Systems | Diameter 10–50mm | Stainless steel, composite materials, titanium alloy | -50°C to 500°C |
Product Highlights
- Power Range: 150 ~ 1800 shp
- Drive Modes: Single propeller direct drive / gearbox-coupled drive
- Application Platforms: Fixed-wing trainer aircraft, aerial survey UAVs, light cargo aircraft
Technical Advantages
- Multistage axial compressor combined with high-pressure combustion system
- Electronic propeller control system
- Center of gravity-optimized structural design
- Hot section components optimized for extended service life
Service Offerings
- Full turboprop engine development and domestic substitution solutions
- Integrated aviation propeller shaft system design
- Customized control system development and calibration
- Performance optimization for agricultural operations and high-altitude flights
Typical Case Studies
- Customized propulsion solution for aerial survey UAVs operating in Northwest plateau regions
- Delivery of certified propulsion packages for unmanned cargo aircraft