Unmanned plane
A technology of unmanned aerial vehicles and fuselage, which is applied in the field of unmanned aerial vehicles, which can solve the problems of unstable installation of power arm, inconvenient installation of rotor, poor rigidity of fuselage, etc., and achieve compact structure, reduced model size, and improved stability Effect
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0019] Below, the substantive features and advantages of the present invention will be further described in conjunction with examples, and the present invention includes but is not limited to the listed embodiments.
[0020] see Figure 1-7 As shown, an unmanned aerial vehicle includes multiple groups of rotors 40, a fuselage 10 made of metal and a triangular truss type power arm 20 made of metal, and the triangular truss type power arm is connected to the rotor power system 30 through a limit mounting plate 80 (see Figure 6 As shown), the installation positions of the adjacent two groups of rotors are arranged one above and one below relative to the fuselage.
[0021] see figure 2 As shown, the fuselage includes an outer shell 12 and an openable upper cover 11 , a metal support frame 13 and a plurality of battery boxes 50 made of metal are arranged inside the outer shell, and a landing gear 60 is connected to the lower part of the fuselage.
[0022] Wherein, the battery ...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


