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Buffer device for aircraft

A buffer device, aircraft technology, applied in aircraft parts, transportation and packaging, chemical instruments and methods, etc., can solve the problems of inconvenient installation structure, complex installation structure, easy to hit buildings, etc., to prevent rust and aging, installation Simple structure and the effect of improving the service life

Inactive Publication Date: 2021-06-22
西安法雀孵化器科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to provide a buffer device for aircraft to solve the problem that the general unmanned aircraft buffer device proposed in the above-mentioned background technology is easy to hit the building due to blurred vision at night when the device is landing, and there is no good warning structure. Prevent vehicles and pedestrians from approaching the device. The stability of the UAV is poor when it is raised and lowered, which makes the UAV easy to cause structural damage due to the influence of gravity. At the same time, the interior of the device is prone to rust and aging due to the influence of humid air, which makes the service life of the device shorter. , it is not convenient to select the required installation structure for drones with different bottom specifications, and the installation structure is complicated

Method used

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Embodiment Construction

[0020] 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.

[0021] see Figure 1-3 , the present invention provides a technical solution: a buffer device for an aircraft, including a base 1, a bearing 2, a lamp tube 3, an outer cylinder 4, an inner cylinder 5, a slider 6, a limit rod 7, a desiccant 8, an upper plate 9. Rotating shaft 10, nut 11, fixed plate 12, mounting rod 13, sleeve block 14, threaded rod 15 and block 16, bearing 2 is installed on the top of base 1, and lamp tube 3 is installed above bearing 2, and t...

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Abstract

The invention belongs to the technical field of unmanned aerial vehicle buffer devices, and particularly relates to a buffer device for an aircraft, the buffer device comprises a base, an outer cylinder and an upper plate, a bearing is mounted at the top of the base, a lamp tube is mounted above the bearing, the outer cylinder is located on the outer wall of the base, and an inner cylinder is mounted on the inner side of the outer cylinder. Compared with an existing unmanned aerial vehicle buffer device, the buffer device for the unmanned aerial vehicle has the advantages that when the device lands, the device can be prevented from colliding with a building due to blurred sight at night, vehicles and pedestrians are prevented from approaching the device, the stability of the unmanned aerial vehicle during lifting can be improved, and the gravity influence of the unmanned aerial vehicle is reduced to the minimum; meanwhile, a damp-proof effect can be achieved for the interior of the device, the situation that a buffer structure rusts and ages due to the influence of wet air is prevented, the service life of the device is prolonged, the device can be suitable for unmanned aerial vehicles of different specifications, and a user can conveniently select a required mounting structure according to the bottom structure of the unmanned aerial vehicle.

Description

technical field [0001] The invention relates to the technical field of buffer devices for unmanned aircraft, in particular to a buffer device for aircraft. Background technique [0002] Unmanned aerial vehicles are also called unmanned aerial vehicles. Unmanned aerial vehicles are unmanned aerial vehicles controlled by radio or program control devices. Unmanned aerial vehicles have the advantages of small size, convenient use and strong battlefield survivability. The buffering device for driving the aircraft can provide a buffering effect for the lifting of the unmanned aircraft and prevent the shaking of the unmanned aircraft during the lifting process. [0003] When the unmanned aerial vehicle buffer device on the market is landing, it is easy to hit the building due to the blurred vision at night, and there is no good warning structure to prevent vehicles and pedestrians from approaching the device. UAVs are prone to structural damage due to the influence of gravity. At ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/02B64D47/04B64C25/62B64C25/32B01D53/26
CPCB01D53/26B64C25/32B64C25/62B64D47/02B64D47/04
Inventor 唐智勇
Owner 西安法雀孵化器科技有限公司
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