Combines Internal Combustion and Electric Drive for Extended Range and Adaptability
| Component | Size | Material | Temperature Range |
|---|---|---|---|
| Internal Combustion Section | Refer to turboprop or piston engines | High-temperature alloy, aluminum alloy | 100°C to 1700°C |
| Electric Section | Refer to electric motors | Carbon fiber, copper, aluminum alloy | -50°C to 150°C |
| Energy Management | Controller 300×200×100mm | Electronic components, aluminum alloy | -40°C to 85°C |
| Integrated Piping System | Diameter 10–50mm | Stainless steel, composite materials | -50°C to 500°C |
System Components
- Engine Module: (Piston/Small Turbine)
- Motor Module: (High Power Density Electric Motor)
- Hybrid Controller
- Energy Storage Battery Pack & Energy Management System
Features Overview
- Seamless Power Transition
- Significant Fuel Savings and Range Advantages
- Ideal for Long-Endurance UAVs and Multirotor Manned Aircraft
- Multi-mode Switching Logic Configurable Based on Mission Scenarios
Technical Support
- Flight Mission Scenario Simulation & Modeling
- System-Level Energy Efficiency Optimization
- High-Reliability Electric Drive Design & Validation
- Health Management System Based on Fault Modes
Client Application Examples
- Hybrid UAV Helicopter with Over 10-Hour Endurance
- Core Propulsion System Supplier for an eVTOL Project