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Unmanned aerial vehicle

A drone and fuselage technology, applied in the field of drones, can solve problems such as unreasonable structure, failure to meet welding requirements, and inability to adjust the angle, and achieve the effect of convenient replacement and reduced manufacturing difficulty.

Active Publication Date: 2021-09-07
HUIZHOU IFLIGHT MOLD CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When the current drones are manufactured, their motors and ESCs are generally welded, which is inconvenient to replace and requires high welding requirements. Many companies fail to meet the welding requirements during welding. At the same time, it is necessary to design multiple electric Adjust the corresponding motor, the structure is unreasonable; in addition, drones generally need to be installed with a GPS module, but the GPS module generally cannot adjust the angle during installation, which cannot meet the needs of flying through different situations

Method used

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Examples

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Embodiment Construction

[0028] In order to make the above objects, features and advantages of the present invention more comprehensible, specific implementations of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0029] The following description of at least one exemplary embodiment is merely illustrative in nature and in no way taken as limiting the invention, its application or uses.

[0030] Techniques and devices known to those of ordinary skill in the relevant art may not be discussed in detail, but where appropriate, such techniques and devices should be considered part of the description.

[0031] In all examples shown and discussed herein, any specific values ​​should be construed as exemplary only, and not as limitations. Therefore, other instances of the exemplary embodiment may have different values.

[0032] It should be noted that like numerals and letters denote like items in the following figures, therefore, once an item is defin...

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Abstract

The invention relates to an unmanned aerial vehicle which comprises a vehicle body and a plurality of vehicle arms, a motor is arranged on each vehicle arm, an electronic speed controller is arranged on the vehicle body, one electronic speed controller can control the motor on each vehicle arm, the electronic speed controllers and the motors are connected in the mode that connecting assemblies are wired along the vehicle arms, and the connecting assemblies are fixed to the vehicle arms through buckling mechanisms. The connecting assembly comprises a first plug-in and a second plug-in, the first plug-in and the second plug-in are connected in a pluggable mode through a socket and a plug, and the connecting assembly is connected with the electronic speed controller through a first wire and connected with the motor through a second wire. The problem that a traditional electronic speed controller and a motor adopt a welding connection mode is effectively solved, the motor and the electronic speed controller can be connected without welding, the manufacturing difficulty is reduced, and the electronic speed controller or the motor is more convenient to replace when damaged.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle. Background technique [0002] UAVs are unmanned aircraft operated by radio-controlled equipment and self-contained program controls, or operated entirely or intermittently autonomously by an on-board computer. When the current drones are manufactured, their motors and ESCs are generally welded, which is inconvenient to replace and has high requirements for welding. Many companies fail to meet the welding requirements during welding. At the same time, it is necessary to design multiple Adjust the corresponding motor, and the structure is unreasonable; in addition, drones generally need to be installed with a GPS module, but the GPS module generally cannot adjust the angle during installation, which cannot meet the needs of flying through different situations. Contents of the invention [0003] Based on this, it is necessary to provide an unman...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D27/24B64D31/00
CPCB64D27/24B64D31/00Y02T50/60
Inventor 程启平张健李飞
Owner HUIZHOU IFLIGHT MOLD CO LTD