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A drone navigator with anti-vibration function

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

Active Publication Date: 2022-04-26
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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  • A drone navigator with anti-vibration function
  • A drone navigator with anti-vibration function
  • A drone navigator with anti-vibration function

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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, which belongs to the technical field of unmanned aerial vehicle navigation. The side of the navigator housing is provided with an axially symmetrical mounting plate, and the surface of the mounting plate is provided with a radially symmetrical mounting plate. Countersunk hole, there is a mounting groove in the navigator shell, the inner wall around the mounting groove is provided with a limited groove, the bottom of the mounting groove is provided with a through groove, the mounting groove is slidingly connected with a fixing plate, and the two ends of the fixing plate are respectively fixedly connected with The symmetrical slider, the shock-absorbing spring and the limit sleeve set by the UAV navigator with anti-vibration function make the upper and lower directions of the fixed plate have the function of buffering and shock absorption, so that the main body of the navigator installed on the surface of the fixed plate has The anti-vibration function, and the set cover plate, limit sleeve and fixed plate have the function of quick manual disassembly and assembly, thereby improving the assembly efficiency of the navigator, and at the same time facilitating the inspection and maintenance of the navigator in the later stage.

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 Patents(China)
IPC IPC(8): B64D47/00F16F15/067
CPCB64D47/00F16F15/067
Inventor 黄辰
Owner SHENYANG AEROSPACE UNIVERSITY
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