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Blade type connecting device for unmanned aerial vehicle arm

A connection device, a technology for unmanned aerial vehicles, applied in the field of unmanned aerial vehicles, can solve problems such as the decline of electrical connection stability, and achieve the effects of ensuring connection stability, improving connection stability, and improving flight safety and reliability.

Pending Publication Date: 2020-09-22
SHENZHEN GODO INNOVATION TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the embodiment of the present application is to provide a drone arm blade type connection device, which aims to solve the problem of the loose connection between the arm mechanism and the drone body in the prior art, which causes the flight power set on the arm mechanism The technical problem that the electrical connection stability of the related components of the device and the UAV body is reduced

Method used

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  • Blade type connecting device for unmanned aerial vehicle arm
  • Blade type connecting device for unmanned aerial vehicle arm
  • Blade type connecting device for unmanned aerial vehicle arm

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Embodiment Construction

[0034] Embodiments of the present application are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. Attached below by reference Figure 1~6 The described embodiments are exemplary and are intended for the purpose of explaining the application and are not to be construed as limiting the application.

[0035] In the description of the present application, it should be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", The orientation or positional relationship indicated by "horizontal", "top", "bottom", "inner", "outer", etc. are based on the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the application and simplifying the description, rather than Nothing to indicate or imply that a referenced de...

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Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and especially relates to a blade type connecting device for an unmanned aerial vehicle arm. The device comprises a vehicle arm mechanism, a power device, a connecting mechanism and an electric connector, the arm mechanism comprises a main arm body, the power device is arranged at the first end of the main arm body, the connecting mechanism comprises a fixing frame and a hoop mechanism arranged on the fixing frame and is used for hooping the main arm body, the fixing frame forms an installation cavity used for containingthe second end of the main arm body, and the electric connector is arranged in the installation cavity and is electrically connected with the power device. When the main arm body is inserted into theinstallation cavity, the hoop mechanism arranged on the fixing frame can firmly hoop the main arm body, so the connection stability of the main arm body and the fixing frame is remarkably improved, the connection stability of the arm mechanism and the unmanned aerial vehicle body is guaranteed, the electrical connection stability of the power device and related devices of the unmanned aerial vehicle body is guaranteed, and the flight safety and reliability of the unmanned aerial vehicle are remarkably improved.

Description

technical field [0001] The present application belongs to the technical field of unmanned aerial vehicles, and in particular relates to a blade type connection device for an unmanned aerial vehicle arm. Background technique [0002] In recent years, with the advancement of technology, the UAV industry has also developed rapidly, and it is gradually used in many fields such as aerial photography surveying and mapping, police work, fire fighting and disaster relief. The drone's arm mechanism is usually equipped with a flight power unit for the drone. [0003] In the prior art, the flight power unit is electrically connected to the relevant components of the drone body through the arm mechanism, and when the connection between the arm mechanism and the drone body is loose, it will affect the flight power unit and the drone. The stability of the electrical connection of the relevant components of the aircraft body may even cause the drone to crash. Contents of the invention ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/00B64C1/16B64D27/26B64D27/24B64D27/40
CPCB64C1/00B64C1/16B64D27/24B64U50/19B64D27/40Y02T50/60
Inventor 李坤煌和瑞江陈泽楠
Owner SHENZHEN GODO INNOVATION TECH CO LTD
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