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Auxiliary device for drone taking off

A technology for auxiliary devices and UAVs, which is applied to ground devices, propulsion devices, engines, aircraft parts, etc. It can solve problems that affect the take-off effect, unbalanced UAVs, and easy to be blown by the wind.

Active Publication Date: 2017-11-24
陕西尖丰盛达航天科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to overcome the disadvantages that the UAV is unbalanced due to the uneven ground when the UAV is taking off, the UAV cannot take off well, and is easily blown by the wind, which affects the take-off effect. The technical problem is to provide a UAV take-off auxiliary device that can balance the UAV so that the UAV can take off well, and at the same time block the wind and make the take-off effect better.

Method used

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  • Auxiliary device for drone taking off
  • Auxiliary device for drone taking off
  • Auxiliary device for drone taking off

Examples

Experimental program
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Effect test

Embodiment 1

[0039] A drone take-off assist device, such as Figure 1-9 As shown, it includes a frame body 1, a vertical rod 2, a wheel 3, a lifting device 4, a horizontal plate 5, an adjustment device 6 and a drone 7. The vertical rod 2 is symmetrically installed on the left and right sides of the outer bottom of the frame body 1, Wheels 3 are installed at the bottom of the vertical bar 2, and a lifting device 4 is provided in the middle of the bottom of the frame body 1. The lifting part of the lifting device 4 is connected with a horizontal plate 5, and the top of the horizontal plate 5 is provided with an adjustment device 6, and the adjustment device 6 is placed There are drones7.

Embodiment 2

[0041] A drone take-off assist device, such as Figure 1-9 As shown, it includes a frame body 1, a vertical rod 2, a wheel 3, a lifting device 4, a horizontal plate 5, an adjustment device 6 and a drone 7. The vertical rod 2 is symmetrically installed on the left and right sides of the outer bottom of the frame body 1, Wheels 3 are installed at the bottom of the vertical bar 2, and a lifting device 4 is provided in the middle of the bottom of the frame body 1. The lifting part of the lifting device 4 is connected with a horizontal plate 5, and the top of the horizontal plate 5 is provided with an adjustment device 6, and the adjustment device 6 is placed There are drones7.

[0042] The lifting device 4 includes a first slide rail 401, an electric reel 402, a first slide block 403, a backguy 404, a lifting frame 405, a second slide rail 406 and a second slide block 407, and the frame body 1 is provided with a first The slide rail 401 and the second slide rail 406, the first sl...

Embodiment 3

[0044] A drone take-off assist device, such as Figure 1-9 As shown, it includes a frame body 1, a vertical rod 2, a wheel 3, a lifting device 4, a horizontal plate 5, an adjustment device 6 and a drone 7. The vertical rod 2 is symmetrically installed on the left and right sides of the outer bottom of the frame body 1, Wheels 3 are installed at the bottom of the vertical bar 2, and a lifting device 4 is provided in the middle of the bottom of the frame body 1. The lifting part of the lifting device 4 is connected with a horizontal plate 5, and the top of the horizontal plate 5 is provided with an adjustment device 6, and the adjustment device 6 is placed There are drones7.

[0045] The lifting device 4 includes a first slide rail 401, an electric reel 402, a first slide block 403, a backguy 404, a lifting frame 405, a second slide rail 406 and a second slide block 407, and the frame body 1 is provided with a first The slide rail 401 and the second slide rail 406, the first sl...

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Abstract

The invention relates to an auxiliary device, in particular to an auxiliary device for drone taking off. The technical purpose to be achieved is to provide the auxiliary device for drone taking off which can place a drone in balance to provide a good takeoff for the drone and keep out wind to make a better effect on taking off at the same time. In order to achieve the technical purpose, the auxiliary device for drone taking off is provided. The device comprises a frame and the like; vertical bars are symmetrically installed on the left and right sides of the bottom of the exterior of the frame, wheels are installed at the bottom ends of the vertical bars, a lifting device is arranged in the middle of the bottom of the interior of the frame, a transverse plate is connected with a lifting part of the lifting device, an adjusting device is arranged on the top of the transverse plate, and the drone is placed on the adjusting device. According to the auxiliary device, through a pushing device, the drone can take off from a water surface, and the effects are achieved that the drone can be placed in balance, so that the good takeoff for the drone is provided, and the wind can be kept off at the same time, so that a better effect on taking off is achieved.

Description

technical field [0001] The invention relates to an auxiliary device, in particular to an auxiliary device for unmanned aerial vehicle take-off. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft that is controlled by radio remote control equipment and its own program control device, or is completely or intermittently operated autonomously by an on-board computer. [0003] Nowadays, people use drones to take pictures in order to capture better scenery. When the drone takes off, the uneven ground causes the drone to be unbalanced, which makes the drone unable to take off well, and it is easy to It is blown by the wind, which affects the take-off effect. Therefore, it is urgent to develop a drone that can be placed in a balanced position, so that the drone can take off well, and at the same time block the wind, so that the take-off effect is better. Drone take-off assist device. Contents of the invention [0004] (1) Technical pro...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F1/00B63H5/00B63H21/17
CPCB63H5/00B63H21/17B63H2021/171B64F1/00
Inventor 严杰豪徐珊赵静薇
Owner 陕西尖丰盛达航天科技有限公司
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