Unmanned aerial vehicle structure
A technology of unmanned aerial vehicles and fuselages, which is applied to structural parts, unmanned aircrafts, fuselages, etc. It can solve problems such as long battery life, many lines, and complex fuselage structure, so as to reduce the overall weight and improve battery life. The effect of time and current output stability
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0059] Such as figure 1 and 2 As shown, an unmanned aerial vehicle structure disclosed in Embodiment 1 of the present invention includes a fuselage 1, a wing 2, a tripod 3, a wing power motor 4, a control module 5 and a communication module 6;
[0060] Fuselage package casing 11 and fuselage conductive structure 12 arranged in the casing, fuselage conductive structure 12 includes battery pack 121, fuselage assembly 122 and wing motor power supply wire 123;
[0061] The battery pack 121 includes a lithium battery pack body 1211 and a power supply circuit board 1212. The positive and negative output ends of the lithium battery pack body 1211 are welded with a single row in-line banana socket 1218. The power supply circuit board 1212 is a double-sided board, and the power supply circuit board 1212 Banana plugs 1217 are arranged on one side corresponding to the banana sockets 1218, inserted vertically through the banana sockets 1218 and welded on two pairs of banana plugs 1217, s...
PUM
| Property | Measurement | Unit |
|---|---|---|
| thickness | aaaaa | aaaaa |
| thickness | aaaaa | aaaaa |
Abstract
Description
Claims
Application Information
Login to View More 


