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Multi-rotor UAV with disassembled structure

A multi-rotor drone and rotor technology, applied in the field of drones, can solve problems such as poor heat dissipation performance of an ESC, and achieve the effect of reducing power loss

Inactive Publication Date: 2018-03-27
EWATT TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The invention provides a multi-rotor UAV with a disassembled structure, which solves or partially solves the technical defect of the poor heat dissipation performance of the ESC fixed inside the fuselage in the prior art

Method used

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  • Multi-rotor UAV with disassembled structure
  • Multi-rotor UAV with disassembled structure
  • Multi-rotor UAV with disassembled structure

Examples

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Embodiment Construction

[0039] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art belong to the scope of protection of the present invention; wherein the keyword "and / or" involved in this embodiment means and, or two Situation, in other words, A and / or B mentioned in the embodiment of the present invention represents two situations of A and B, A or B, and describes the three states that A and B exist, such as A and / or B, means: only includes A and does not include B; only includes B and does not include A; includes A and B.

[0040] Meanwhile, in the embodiments of the present invention, when a component is referred to as being “...

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Abstract

The invention discloses a multi-rotor unmanned aerial vehicle with a disassembly structure, which belongs to the technical field of unmanned aerial vehicles. The multi-rotor unmanned aerial vehicle includes: a first disassembly assembly, and the first disassembly assembly is fixed on the body; A rotor power assembly, the rotor power assembly is fixed on the rotor shaft, and the rotor power assembly includes at least one electric regulator; a quick release assembly, the first rotor is rotationally fixed to the on the rotor power unit. The invention solves the technical defect of the poor heat dissipation performance of the ESC fixed inside the fuselage in the prior art.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, in particular to a multi-rotor unmanned aerial vehicle with a detachable structure. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but it is equipped with autopilot, program control device, information collection device and other equipment. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. Under the radio control, it can take off like an ordinary aircraft or be launched into the air with a booster rocket, and it can also be taken into the air by the parent aircraft for flight. [0003] The unmanned aerial vehicle in the prior art includes a fuselage, a rotor shaft and a cl...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D47/08B64C27/14
CPCB64C27/14B64D47/08B64U2101/30
Inventor 赵国成罗伟范晖陈芳芳
Owner EWATT TECH CO LTD