Unmanned aerial vehicle control load reducing device

A technology of lightening devices and drones, applied in weight loss, travel or camping equipment, travel bags, etc., can solve problems such as rigidity, low flexibility, and high joints, so as to reduce the degree of joint rigidity and avoid limb movements. Effect

Pending Publication Date: 2022-05-27
GUANGDONG POWER GRID CO LTD +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In view of this, the purpose of this application is to provide a UAV control load reduction device, which is used to solve the problem that the existing UAV control aids have low flexibility, resulting in high joint stiffness of the staff after long-term use. risk issue

Method used

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  • Unmanned aerial vehicle control load reducing device
  • Unmanned aerial vehicle control load reducing device
  • Unmanned aerial vehicle control load reducing device

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Embodiment Construction

[0040] The technical solutions of the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are part of the embodiments of the present application, but not all of the embodiments. Based on the embodiments in the embodiments of the present application, all other embodiments obtained by persons of ordinary skill in the art without creative work fall within the scope of the claimed protection of the present application.

[0041] In the description of the embodiments of the present application, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" The orientation or positional relationship indicated by "" etc. is based on the orientation or positional relationship shown in the accompanying drawings, which is only for the convenience of describing the embodiments of the present application and simplifyin...

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PUM

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Abstract

The invention discloses an unmanned aerial vehicle control load reducing device which comprises a neck hanging support and a waist supporting tool. The neck hanging support comprises a hanging frame and two elbow brackets. The waist brace comprises a waist belt and two triangular supports. The elbow bracket can be used for lifting the periphery of a worker; the hanging frame is hung on the shoulder or neck position of a worker and provides supporting force for the elbow bracket; the waistband can be worn on the waist of a worker, so that the two triangular brackets can be combined for placing tools such as a remote controller. A hand supporting plate on the elbow bracket and an object supporting plate of the triangular support can be adjusted to proper positions, it is avoided that a worker keeps rigid limb movement for a long time, force needed for operating the unmanned aerial vehicle can be dispersed and transferred to the neck and the waist, and the joint stiffness degree of the worker is reduced.

Description

technical field [0001] The present application relates to the technical field of UAV operation aids, and in particular, to a device for reducing the control load of UAVs. Background technique [0002] UAVs are widely used in power grid line inspections. After the staff operates the drone by holding the remote control for a long time, the arm joints tend to become rigid. To this end, the staff will use auxiliary tools such as arm braces to reduce the burden on the wrist. The existing auxiliary tools often only play the role of sharing the force, and the staff will still have a high possibility of joint stiffness after long-term use. SUMMARY OF THE INVENTION [0003] In view of this, the purpose of the present application is to provide a device for reducing the weight of drone control, which is used to solve the problem of low flexibility of existing drone control aids, which leads to high joint stiffness in the case of long-term use by staff. question of risk. [0004] ...

Claims

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Application Information

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IPC IPC(8): A45F3/10
CPCA45F3/10Y02T50/40
Inventor 田亮孟繁琪
Owner GUANGDONG POWER GRID CO LTD
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