
Carbon Fiber Foam-Core Technology Powers Next-Gen VTOL UAV for Precision Agriculture, Power Inspection, and Emergency Response
[xiamen, China – Date] – WUYING, a global leader in advanced unmanned aerial systems, today announced the official launch of its groundbreaking Z-4020 PNP, a 20kg-class VTOL (Vertical Takeoff and Landing) drone engineered to outperform traditional fuel-powered UAVs while operating under streamlined regulatory frameworks. Combining aerospace-grade carbon fiber foam-core construction with intelligent multiwing design, this VTOL UAV delivers an industry-leading 8+ hours of flight time – a 300% improvement over conventional electric drones – and eliminates airworthiness certification requirements, positioning it as the ultimate tool for mission-critical operations.
Engineering Breakthrough: How VTOL Design Meets Lightweight Innovation
At the heart of the Z-4020 PNP lies WUYING patented multiwing VTOL architecture, seamlessly integrating vertical lift efficiency with fixed-wing endurance. The fusion of carbon fiber inner foaming technology reduces structural weight by 35% compared to aluminum alloys while maintaining military-grade durability. This innovation enables:
- Extended Range: 8-hour continuous flight (400-600 km² coverage per sortie)
- Heavy Payload Flexibility: 5kg modular capacity for LiDAR, multispectral sensors, or emergency payloads
- Zero-Runway Deployment: VTOL capability eliminates infrastructure dependencies in remote areas
Z-3015 | Z-4020 | Z-3020S(Expected to be released by the end of June 2025) | |
Description | The classic models released in 2022 The standard flight time is 6 hours, suitable for traditional measurement The drawing and carrying capacity is 1.5 kilograms, with a diameter A pod of about 120mm |
It will make its maiden flight in May 2024 and be officially released And May 2025. At the base of 3015 On this basis, enhance the strength of the middle section and extend the machine The outer wing segments and the tail wing have been replaced with brand new ones Rotor power system and enlarged fuselage |
The designed rated cruising speed is 90km/h. 3 The wingspan of a meter can provide an appropriate liter This model is more suitable for those over 10 meters Efficient operation in windy weather |
Typical applications | Pipelines, coastlines, forest inspections, short Large-scale mapping of time |
On the same left, it can also carry the diameter of a sphere A high-specification pod of about 170mm, small A payload of 2-4kg for type lidar, etc |
The same as the left, and at the same time, it can complete tasks more quickly service |
Wingspan | 3000mm | 3700mm | 3000mm |
Length | 1650mm | 1750mm | 1750mm |
Take-off weight | 14-16kg | 17-20kg | 16-20kg |
Typical load capacity | 1-2kg | 2-4kg | 2-4kg |
Shared payload(Battery + Load) | 8kg | 12kg | 12kg |
Maximum voyage range | 440km (Test Flight) | 614km(Test Flight) | 500km+(No Test Flight) |
Maximum flight time | 6H(@1kg20m/s) | 8H(@1kg20m/s) | |
5h(@4kg20m/s) | |||
Economic cruising speed range | 65-80km/h | 65-80km/h | 80-100km/h |
Rotor system power surplus | 250% | 260% | 270% |
Airborne cruise battery energy | 32V 1800wh | 48V 2700wh | 48V 2700wh |
Packaging box size | 135cm*55cm*40cm | 138cm*55cm*40cm |
Availability & Resources
Explore the Z-4020 PNP’s VTOL drone specifications or schedule a live demo:
📩 info@uavmodel.com | 🌐 http://www.uavmodel.com/*****vtol-z4020