Electric unmanned aerial vehicle
An electric unmanned aerial vehicle and fuselage technology, applied in the field of unmanned aerial vehicles, can solve the problems of inability to launch weapons obliquely upwards, only to carry out operations downwards, load layout restrictions, etc., and achieve easy expansion of load layout and low cost. The effect of transportation and optimized structural design
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0025] In order to have a clearer understanding of the technical features, purposes and effects of the present invention, the specific implementation manners of the present invention will now be described with reference to the accompanying drawings. Wherein, the same parts adopt the same reference numerals.
[0026] As mentioned above, most of the existing multi-axis drones adopt a fully symmetrical layout, resulting in the center of gravity being concentrated at one point, and the load layout is greatly restricted, and because the fully symmetrical rotors block all directions of the drone, resulting in The carried load cannot launch weapons or observe obliquely upwards, which limits the application range of existing drones.
[0027] In order to solve the above defects, the application provides an electric drone, such as Figure 1-4 As shown, among them, figure 1 Shown is a schematic diagram of the three-dimensional structure of an electric drone according to a specific embo...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


