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Single rotor UAV
The independent motor driven constant pitch tail rotor structure is innovatively designed to replace the traditional main power driven variable pitch tail rotor structure, reducing the number of structural parts by 90% and the failure rate by 99%.
- Information
Single rotor UAV
Introduction
WZ-X50 unmanned helicopter, based on high-load and high-efficiency helicopter operation platform, is equipped with a new intelligent flight control system without pitch. The whole machine is modular design, and the wings can be folded and detachable, which greatly facilitates the maintenance and transportation of the aircraft. With customized high-efficiency carbon fiber OARS, it not only ensures the super load capacity.
Key Parameters
Max Size 1970x620×690(mm)
The task load is 30kg
Material carbon fiber + aviation aluminum
Operation speed 7m/s
Hover time: 25min
Specification parameter
dimension | 1985mm*615mm*670mm |
Folding size | 1305mm*615mm*680mm |
Empty weight | 22kg |
Maximum take-off weight | 50kg |
Flight speed | 10m/s |
Hover accuracy | Horizontal: 10cm, vertical: 10cm |
Mode of flight | Semi-automatic/fully automatic |
Operating ambient temperature | -20 ℃ to +45 ℃ |
battery | 28000mah*2 |
No-load endurance | 45min |
No-load mileage | 24km |
Battery life | ≥300 times |
Working radius | 10km |
