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Supporting equipment for unmanned drone aircraft

A technology for unmanned aerial vehicles and support equipment, which is applied to aircraft parts, landing gear, chassis, etc., and can solve problems such as poor cushioning performance, poor use effect, and poor stability

Inactive Publication Date: 2017-05-10
洪东科
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] In order to overcome the disadvantages of poor cushioning performance, poor stability and poor use effect of the existing support equipment for unmanned aircraft, the technical problem to be solved by the present invention is to provide a support equipment for unmanned aerial vehicles

Method used

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  • Supporting equipment for unmanned drone aircraft
  • Supporting equipment for unmanned drone aircraft
  • Supporting equipment for unmanned drone aircraft

Examples

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Embodiment 1

[0029]A support device for an unmanned aerial vehicle, such as Figure 1-4 As shown, it includes a support frame 2, a support plate 3, a partition 4, a slide rail 5, a slider 6, a first electric wheel 7, a stay cord 8, a wedge block 9, a guide plate 10, a second electric wheel 12, the first electric wheel A spring 13, a moving block 14, a moving rod 15, a contact ball 16, a U-shaped frame 17, and a support mechanism 18; the bottom of the unmanned aerial vehicle 1 is welded to the left and right with a support frame 2, and the bottom of the support frame 2 is welded to a support plate 3, The upper part of the support frame 2 on the left and right sides is welded and connected with a partition 4, and the bottom of the partition 4 is connected with a slide rail 5 through bolt connection, and a slide block 6 is slidably connected to the slide rail 5, and the slide block 6 and the slide rail 5, the bottom of the slide block 6 is connected with a wedge block 9 by means of screw conn...

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Abstract

The invention relates to supporting equipment, in particular to supporting equipment for an unmanned drone aircraft. A technical problem to be solved is that the supporting equipment for the unmanned drone aircraft, which has the advantages of good buffering performance, good stability and good use effect, cannot be provided. To solve the technical problem, the invention provides the supporting equipment for the unmanned drone aircraft. The supporting equipment for the unmanned drone aircraft comprises a supporting frame, a supporting plate, a partition plate, a slide rail, a slide block, a first electric wheel, a pull rope, a wedge block, a guide plate, a second electric wheel, a first spring, a moving block and so on, wherein the supporting plate is welded at the bottom of the supporting frame;the partition plate is welded between the upper parts, on the left and right sides, of the supporting frames; the bottom of the partition plate is connected with the slide rail through a bolt; and the slide block is connected to the slide rail in a sliding way. As two buffering defenses are arranged, the supporting equipment for the unmanned drone aircraft is advantaged in that the impact force of the unmanned drone aircraft during landing can be buffered in a maximized way, parts in the unmanned drone aircraft can be prevented from being damaged by impact and the supporting equipment is provided with two supporting systems.

Description

technical field [0001] The invention relates to a support device, in particular to a support device for an unmanned aircraft. Background technique [0002] Unmanned aerial vehicle is referred to as " unmanned aerial vehicle ", is the unmanned aircraft that utilizes radio remote control equipment and self-contained program control device to manipulate. There is no cockpit on board, but equipment such as autopilot and program control device are installed. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. Under the radio control, it can take off like an ordinary aircraft or be launched into the air with a booster rocket, and it can also be taken into the air by the parent aircraft for flight. When recovering, it can automatically land in the same way as the common aircraft landing process, and can also be recovered by remote c...

Claims

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Application Information

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IPC IPC(8): B64C25/26B64C25/62B64C25/32
CPCB64C25/26B64C25/32B64C25/62
Inventor 洪东科
Owner 洪东科
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