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UAV airborne equipment vertical retractable mechanism and UAV

A technology of airborne equipment and retractable mechanism, applied in the field of aircraft, can solve the problems of poor assembly accuracy, easy jamming, poor assembly accuracy of vertical retractable mechanism, etc., and achieves simple and reasonable structure, stable lifting motion, installation and use. handy effect

Active Publication Date: 2021-07-13
成都纵横大鹏无人机科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The purpose of the present invention is to provide a vertical retractable mechanism for UAV airborne equipment to improve the poor assembly accuracy of the vertical retractable mechanism for UAV airborne equipment, which leads to the problem of easy jamming during the working process
[0008] The purpose of the present invention is to provide an unmanned aerial vehicle to improve the poor assembly accuracy of the vertical retractable mechanism of the traditional unmanned aerial vehicle onboard equipment, which leads to the problem of easy jamming during the working process

Method used

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  • UAV airborne equipment vertical retractable mechanism and UAV
  • UAV airborne equipment vertical retractable mechanism and UAV
  • UAV airborne equipment vertical retractable mechanism and UAV

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Embodiment

[0044] This embodiment provides a vertical retractable mechanism for the on-board equipment of the UAV, which is suitable for driving the on-board equipment 001 so that the on-board equipment 001 protrudes from the casing of the UAV to perform corresponding tasks, or when it is not needed When the airborne device 001 is used, the airborne device 001 is retracted into the casing of the drone without affecting the normal flight of the drone.

[0045] see figure 1 , the vertical retractable mechanism of the UAV on-board equipment provided in this embodiment includes a mounting frame 100, an equipment carrier 200 and at least two screw drive pairs 300, and the equipment carrier 200 is provided with a connected first limiting hole 240 and the second limit hole 250; the screw drive pair 300 includes a screw main body 310 and a drive nut 320, the drive nut 320 is screwed outside the screw main body 310, the screw main body 310 is rotatably connected to the mounting bracket 100, and t...

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Abstract

The invention provides a vertical retractable mechanism for on-board equipment of a UAV and a UAV, including a mounting frame, an equipment carrying frame and at least two screw drive pairs, and the equipment carrying frame is provided with a connected first limiting hole and the second limit hole; the screw drive pair includes a screw main body and a drive nut, the drive nut is screwed outside the screw main body, the screw main body is rotatably connected to the mounting bracket, the screw main body passes through the first limit hole, and the screw There is a gap between the outer peripheral surface of the rod main body and the hole wall of the first limiting hole; the transmission nut is inserted into the second limiting hole, and there is a gap between the outer peripheral surface of the driving nut and the hole wall of the second limiting hole. The drive nut is connected with the circumferential limit of the hole wall of the second limit hole. Through the improvement of the screw drive pair, adaptive adjustments can be made during the assembly process to ensure the coaxiality of the screw main body and the drive nut, and to adjust multiple nuts on the same level to avoid the occurrence of problems during the relative operation of the screw main body and the drive nut. Stuck situation.

Description

technical field [0001] The present invention relates to the field of aircraft, in particular to a vertical retractable mechanism for on-board equipment of an unmanned aerial vehicle and an unmanned aerial vehicle. Background technique [0002] When most UAVs perform tasks, the mission equipment they carry needs to be deployed outside the body for work; while in the non-mission phase, it needs to be retracted into the body to protect the equipment and reduce flight resistance. Therefore, it is necessary to design retractable mechanisms for these airborne devices to meet their application requirements. [0003] At present, the more common retractable mechanisms include rotary retractable mechanisms and vertical retractable mechanisms. [0004] The inventor found in the research that the retractable mechanism of the traditional UAV airborne equipment has at least the following disadvantages: [0005] First, the rotary retractable mechanism requires a large space in the horizo...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C39/02B64D47/00
CPCB64C39/02B64D47/00B64U2101/00
Inventor 王利光彭碧辉谭春林
Owner 成都纵横大鹏无人机科技有限公司