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A tilting compound wing unmanned aerial vehicle with convenient battery replacement

An unmanned aerial vehicle and composite wing technology, applied in the field of unmanned aerial vehicles, can solve the problems of reducing the working efficiency of the battery of the tilting composite wing drone, shaking of the battery of the tilting composite wing drone, and inconvenient replacement of the battery, so as to avoid Efficiency of electricity resources, avoidance of water ingress, effect of optimizing the installation process

Active Publication Date: 2022-04-05
北京卫通新科测控技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention provides a tilting compound wing unmanned aerial vehicle that is easy to replace batteries, which can effectively solve the problem that the tilting compound wing unmanned aerial vehicle currently on the market proposed in the above background technology, in the actual use process, due to the lack of installation mechanism, causes It is inconvenient for the staff to replace the battery of the tilting compound wing drone, which reduces the work efficiency of the staff in replacing the battery of the tilting compound wing drone. At the same time, it also causes the battery of the tilting compound wing drone The problem of shaking phenomenon in

Method used

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  • A tilting compound wing unmanned aerial vehicle with convenient battery replacement
  • A tilting compound wing unmanned aerial vehicle with convenient battery replacement
  • A tilting compound wing unmanned aerial vehicle with convenient battery replacement

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Embodiment

[0051] Example: such as Figure 1-13 As shown, the present invention provides a technical solution, a tilting compound wing unmanned aerial vehicle that is easy to replace batteries, including a fuselage 1, in order to facilitate the staff to fix the position of the battery 208, a mounting mechanism is installed inside the fuselage 1 2;

[0052] The installation mechanism 2 includes a sealing cover 201, a sealing ring 202, a thread groove 203, an inner hexagon bolt 204, an L-shaped plate 205, a limiting plate 206, a rubber pad 207, a battery 208, a cross frame 209, a groove 210, and a limiting groove 211 , positioning block 212, fixed frame 213, limit block 214, buckle 215 and fixing bolt 216;

[0053] A seal cover 201 is installed in the middle of the top of the fuselage 1, and a seal ring 202 is connected to the bottom edge of the seal cover 201. The bottom of the seal ring 202 is connected to the top of the fuselage 1, and the top of the fuselage 1 is symmetrically provide...

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Abstract

The invention discloses a tilting compound-wing unmanned aerial vehicle which is convenient for battery replacement. It includes a fuselage, and a mounting mechanism is installed inside the fuselage. The mounting mechanism includes a sealing cover, a sealing ring, a thread groove, an inner hexagonal bolt, L-shaped plate, limit plate, rubber pad, battery, cross frame, groove, limit groove, positioning block, fixed frame, limit block, buckle and fixing bolt, and a sealing cover is installed in the middle part of the top of the fuselage, The invention facilitates the staff to dismantle and install the sealing cover through the installation mechanism, thereby facilitating the staff to replace the battery in the later stage, and at the same time, it is also convenient for the staff to pre-fix the position of the battery, thereby avoiding the process of staff fixing the battery The position of the middle battery is shifted, which reduces the difficulty for the staff to replace and install the battery, and facilitates the staff to limit the position of the buckle of the battery and the buckle of the drone.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a tilting compound wing unmanned aerial vehicle which is convenient for battery replacement. Background technique [0002] Unmanned aircraft is referred to as unmanned aerial vehicle, and the English abbreviation is UAV. It is an unmanned aircraft controlled by radio remote control equipment and its own program control device, or it is completely or intermittently operated autonomously by the on-board computer; [0003] However, in the actual use of the tilting compound wing UAVs currently on the market, due to the lack of installation mechanisms, it is inconvenient for the staff to replace the batteries of the tilting compound wing UAVs, thereby reducing the staff's need to replace the tilting compound wing. At the same time, the working efficiency of the battery of the UAV also causes the phenomenon of shaking during the use of the battery of the tilting compou...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/22B64D27/24H01M50/249B64D47/02B64C27/26B64C25/62
CPCB64C27/22B64D27/24B64D47/02B64C27/26B64C25/62B64U10/00
Inventor 闫兆
Owner 北京卫通新科测控技术有限公司
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