Hybrid UAV
Specifications
Key Features
1. System Overview:
Power Level: >100kW hybrid oil-electric system
Applications: Large industrial drones (100–200kg payload), VTOL, logistics, rescue, military
Takeoff Weight: Up to 580 kg
Endurance: 90 minutes full-load flight
Altitude Capability: >5000m, Wind resistance level 7
Main Components & Features:
A. Propeller Drive System
Integrated motor + controller + thermal management
23kW rated power, 120kg thrust, 100% peak load
Optional plateau blades for high-altitude performance
B. Intelligent Power Generation
Horizontally opposed 4-cylinder aircraft engine
Dual-function starter/generator
400–500V DC adaptive output
Modular, long life, low fuel consumption
C. High-Voltage DC Grid Energy Storage
Efficient BMS with thermal management and CAN communication
Supports parallel unit operation
Automatic charge/discharge control to extend battery life
Autonomous flight & one-key takeoff/landing supported
Performance & Technical Advantages
Engine output boost: +20%
Payload increase: +50%–60%
Quick mission prep (<5 minutes)
Decoupled powertrain enables flexible aircraft design
Modular design for easy deployment and maintenance
BIT (Built-in Test) and autonomous fault recovery
Application Scenarios
Logistics: Remote/plateau/desert/island supply
Emergency Rescue: Wildfire, earthquake, grid/power/network outage
Military: Reconnaissance, electronic warfare, precision strike
Police: Agile border patrol, urban surveillance
Others: Expandable to unmanned boats, mobile power stations