BDPT-EZY-HM450 Heavy-Lift UAV Helicopter
This model meets all requirements for heavy-lift operations, including mission planning, high operational readiness, reliability, airframe strength, varied payload capabilities, and takeoff/landing in complex terrain. During heavy-lift missions, flight routes are established through route planning. The primary goal of mission planning is to integrate flight performance, heavy-lift payload capacity, arrival time, fuel consumption, and operational area constraints based on mission and route data. This ensures successful mission completion and safe return to base. 1. Features advanced flight capabilities such as automatic takeoff/landing, automatic hover, and Beyond Visual Line of Sight (BVLOS) flight. 2. Supports pre-programmed flight, online route re-planning, and wireless upload. 3. Includes automatic fault diagnosis and identification for key unmanned helicopter components.
Product Specifications
Key Technical Specifications for Single-Rotor Heavy-Lift UAV Helicopter
Project | Parameters |
Cruise Speed | 90Km/h |
Maximum Rate of Climb | 6 m/s |
Maximum Flight Speed | 110Km/h |
Maximum Working Height | Elevation 3200m |
Battery Life | 100 minutes @ 100kg load |
Takeoff and Landing Method | Remote takeoff and landing, autonomous takeoff and landing, or fully autonomous takeoff and landing |
Maximum Wind Resistance | Maximum wind speed of 7 level (17.2m/s) during hover |
Body Weight | 263kg (excluding fuel) |
Maximum Takeoff Weight | 422KG |
Maximum Payload | 150kg (sea level) |
Aircraft Power Supply Type | Lithium Iron Phosphate (Li-Fe) Battery 7000mAh |
Voltage | 12V |
Airborne Generator Power | 12V 600W |
Engine Type | Piston engine |
Cylinder Count, Configuration | Four-cylinder, flat |
Fuel Type | Gasoline 95 |
Cooling Method | Liquid cooling |
Start-up Method | Airborne electric start |
Articulated Rotor | Free-swinging or conical; rigidly connected in-plane |
Blade Count | 2 |
Rotor Diameter | 6090 mm |
blade chord length | 2695 mm |
Blade Twist Angle | 0° |
Constant Speed | 1300 RPM |
Drive System
Project | Parameters |
Engine to clutch | Friction plate transmission |
Clutch to Main Transmission Box | Belt drive |
Main gearbox to rotor | Gear Drive |
Main transmission case to tail rotor | Belt drive |
Power Unit
Project | Parameters |
articulated tail rotor | Swing freely |
Number of Blades | 2 |
Tail Rotor Configuration | Rigid connection in plane |
blade chord length | 406 mm |
Blade twist angle | 43.5 mm |
Preset Cone Angle | 0° |
Model | ROTAX-912 100 HP |
Constant Speed | 5800 RPM |
Constant Power | 80 kW |
Fuel
gasoline | GB 95# |
Pricing Details
Product price is negotiable and determined by order quantity, configuration requirements, and delivery terms.
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Product Details
Key Technical Specifications for Single-Rotor Heavy-Lift UAV Helicopter
Drive System
Power Unit
Fuel
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