Unmanned aerial vehicle navigator with anti-vibration function

A navigator and drone technology, applied in the field of drone navigation, can solve the problems of loose, falling off, cumbersome and time-consuming parts of the navigator, and achieve the effects of improving assembly efficiency, easy disassembly, and easy maintenance

Active Publication Date: 2021-02-05
SHENYANG AEROSPACE UNIVERSITY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, in the UAV structure system, the navigation system is essential for the UAV, but the existing navigator may cause the UAV to frequently collide with the ground when the user performs landing exercises on the UAV , so that the navigator will inevitably be affected by the vibration force, which may loosen or fall off the internal parts of the navigator, which will cause the navigator to fail to work normally. At the same time, when the navigator is assembled, most of them are fastened by screws. , is more cumbersome and time-consuming, and it is not convenient for the disassembly and maintenance of the navigator in the later stage. Therefore, we have designed a UAV navigator with anti-vibration function to solve the above problems

Method used

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Embodiment Construction

[0028] 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 without making creative efforts belong to the protection scope of the present invention.

[0029] see Figure 1-5 , a drone navigator with anti-vibration function, including a navigator housing 1, see Figure 1-5 , the side of the navigator housing 1 is provided with an axially symmetrical mounting plate 11, the mounting plate 11 is installed and fixed with the UAV housing by screws, and the surface of the mounting plate 11 is provided with a radially symmetrical countersunk hole 12. The instrument housing 1 is provided with an installation groove ...

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Abstract

The invention discloses an unmanned aerial vehicle navigator with an anti-vibration function, and belongs to the technical field of unmanned aerial vehicle navigation.The side face of a navigator shell is provided with axially-symmetrical mounting plates, the surfaces of the mounting plates are provided with radially-symmetrical counterbores, a mounting groove is formed in the navigator shell, andlimiting grooves are formed in the inner walls of the periphery of the mounting groove; through grooves are formed in the bottoms of the mounting grooves, fixing plates are slidably connected into the mounting grooves, and symmetrical sliding blocks are fixedly connected to the two ends of each fixing plate correspondingly, according to the unmanned aerial vehicle navigator with the anti-vibration function, the damping springs and the limiting sleeves are arranged, so that the fixing plate has buffering and damping effects in the vertical direction, therefore, the navigator body installed onthe surface of the fixing plate has the anti-vibration function, the cover plate, the limiting sleeve and the fixing plate have the function of rapid manual disassembly and assembly, the assembly efficiency of the navigator is improved, and meanwhile overhauling and maintenance of the navigator in the later period are facilitated.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicle navigation, and more specifically, relates to an unmanned aerial vehicle navigator with an anti-vibration function. 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. [0003] At present, in the UAV structure system, the navigation system is essential for the UAV, but the existing navigator may cause the UAV to frequently collide with the ground when the user performs landing exercises on the UAV , so that the navigator will inevitably be affected by the vibration force, which may loosen or fall off the internal parts of the navigator, which will cause the navigator to fail to work normally. At the same time, when the navigator is assembled, most of them are fastened by screws , is more cumbersome and time-consuming, and it is not convenient for the disassem...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/00F16F15/067
CPCB64D47/00F16F15/067
Inventor 黄辰
Owner SHENYANG AEROSPACE UNIVERSITY
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