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Foldable unmanned aerial vehicle

A technology for drones and fuselage, applied in the field of drones, can solve the problems of unfoldable drones, not easy to assemble, and take up a lot of space, so as to achieve rapid deployment and recovery, save space, and facilitate tension adjustment and adjustment. replacement effect

Active Publication Date: 2021-09-21
ZHUHAI ZIYAN UAV CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Traditional unmanned aerial vehicles are not foldable. When assembling and transporting, not only is it not easy to assemble, but it also takes up a lot of space, which brings a lot of trouble to people's use.

Method used

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  • Foldable unmanned aerial vehicle
  • Foldable unmanned aerial vehicle
  • Foldable unmanned aerial vehicle

Examples

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Embodiment Construction

[0040] The present invention will be described in detail below with reference to the accompanying drawings and examples. It should be noted that in the case of no conflict, the following embodiments and the features in the embodiments can be combined with each other.

[0041] Such as figure 1As shown, a foldable UAV includes a fuselage 1, a tail 2, a battery 100, a main rotor 200, a tail rotor 300 and a plurality of tripods 400, the battery 100 is arranged on the fuselage 1, and the main rotor 200 is installed On the top of the fuselage 1, the tail rotor 300 is installed on the tail 2, and the tripod 400 is arranged under the fuselage 1. Specifically, as Figure 2-5 As shown, the fuselage 1 is provided with a fuselage power socket 101 and two battery hook seats 102, and the two battery hook seats 102 are located on both sides of the power socket 1 of the fuselage 1, and are fixed with the fuselage 1, and can be installed by screws On the fuselage 1, the battery hook seat 102...

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Abstract

The invention discloses a foldable unmanned aerial vehicle which comprises a vehicle body, a vehicle tail, a battery, a main rotor wing, a tail rotor wing and a plurality of foot stools, the battery is arranged on the vehicle body, the main rotor wing is installed on the top of the vehicle body, the tail rotor wing is installed on the vehicle tail, and the foot stools are arranged below the vehicle body. A vehicle body power socket and the battery power socket as well as the battery hook plate and the battery fixing slot are respectively inserted from the side part, after insertion, the front end of the battery lock catch wrench is a movable end, and a convex part arranged at the front end of the battery lock catch wrench is pressed in a curved surface groove of a curved surface boss of the slot seat and is locked with the curved surface boss of the slot; a shell of the fuselage and a shell of the tail are connected in a foldable mode through a connecting part. The battery is detachable, the tail is foldable, disassembly and transportation are convenient, and storage and transportation space is saved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a foldable unmanned aerial vehicle. Background technique [0002] Traditional drones are not foldable, not only difficult to assemble during assembly and transportation, but also take up a lot of space, which brings a lot of trouble to people's use. Contents of the invention [0003] In order to solve the above problems, the present invention provides a foldable drone, which is convenient for storage and transportation. [0004] Technical scheme of the present invention is: [0005] A foldable unmanned aerial vehicle, including a fuselage, a tail, a battery, a main rotor, a tail rotor and multiple tripods, the battery is arranged on the fuselage, the main rotor is installed on the top of the fuselage, and the tail rotor is installed on the tail. The tripod is arranged under the fuselage, and it is characterized in that: the body battery socket and two battery...

Claims

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Application Information

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IPC IPC(8): B64C1/30B64C3/56B64D27/24B64D27/26B64C25/14
CPCB64C1/30B64C3/56B64D27/24B64C25/14B64U10/10B64U30/20B64U50/19B64D27/40
Inventor 王江平李钊唐知杨梅粲文邓真真
Owner ZHUHAI ZIYAN UAV CO LTD