CN219237362U

CN219237362U - Unmanned aerial vehicle landing calibration support with magnetic attraction alignment structure

Info

Publication number: CN219237362U
Application number: CN202223160415.4U
Authority: CN
Inventors: 刘营波; 薛永江; 陈东
Original assignee: Wuhai Ruige Industry Trade Co ltd
Current assignee: Wuhai Ruige Industry Trade Co ltd
Priority date: 2022-11-28
Filing date: 2022-11-28
Publication date: 2023-06-23
Anticipated expiration: 2032-11-28

Abstract

The utility model discloses an unmanned aerial vehicle landing calibration support with a magnetic attraction alignment structure, which comprises a bottom plate, wherein a landing plate is arranged above the bottom plate, a buffer mechanism is arranged between the landing plate and the bottom plate, a mounting groove is formed in the landing plate, slots are formed in the inner walls of two sides of the mounting groove, a plugboard is arranged in the mounting groove, plug blocks are fixed at two ends of the plugboard and are inserted into the slots, second magnets are arranged on two sides of the surface of the plugboard, an unmanned aerial vehicle landing support is arranged on the landing plate, a first magnet is arranged at the bottom of the unmanned aerial vehicle landing support, and the first magnet and the second magnet are in ferromagnetic attraction connection.

Description

Unmanned aerial vehicle landing calibration support with magnetic attraction alignment structure

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle landing calibration support with a magnetic attraction alignment structure.

Background

The unmanned aerial vehicle is an unmanned aerial vehicle operated by a radio remote control device or a self-programming control device. It was first found in the 20 th century, 20, when used as a training target.

The unmanned aerial vehicle directly lands on the ground through the support when landing, and the unmanned aerial vehicle is easy to fall unstably due to the influences of control and external environment factors, so that the unmanned aerial vehicle is damaged.

Disclosure of Invention

The utility model aims to provide an unmanned aerial vehicle landing calibration support with a magnetic attraction alignment structure, so as to solve the problems in the background art.

In order to achieve the above purpose, the present utility model provides the following technical solutions: unmanned aerial vehicle that has magnetism and inhale alignment structure falls calibration support, which comprises a base plate, the bottom plate top is provided with the descending board, be provided with buffer gear between descending board and the bottom plate, the mounting groove has been seted up on the descending board, the slot has all been seted up on the inner wall of mounting groove both sides, the inside picture peg that is provided with of mounting groove, the picture peg both ends all are fixed with the inserted block, the inserted block is pegged graft with the slot, the second magnet is all installed to picture peg surface both sides, be provided with unmanned aerial vehicle on the descending board and descend the support, first magnet is installed to unmanned aerial vehicle descending support bottom, first magnet and second magnetism are ferromagnetic to inhale to be connected.

Preferably, the buffer mechanism comprises a supporting cylinder, a positioning cylinder, a buffer spring and a slide rod, wherein the supporting cylinder and the positioning cylinder are fixed on a bottom plate, a mounting plate is fixed at the bottom of the landing plate, one end of the buffer spring is fixed on the mounting plate, the other end of the buffer spring is inserted into the supporting cylinder and fixedly connected with the bottom end of the supporting cylinder, the slide rod is fixed at the bottom of the landing plate, and the slide rod is spliced with the positioning cylinder.

Preferably, the number of the positioning cylinders is two, and the positioning cylinders are symmetrically distributed about the supporting cylinder.

Preferably, a handle is installed on the plugboard.

Preferably, the bottom of the bottom plate is adhered with an anti-slip pad.

Compared with the prior art, the utility model has the beneficial effects that:

1. according to the utility model, the landing plate is provided with the plugboard, the plugboard is provided with the second magnet, the bottom of the unmanned aerial vehicle landing bracket is provided with the first magnet, and when the unmanned aerial vehicle lands, the first magnet on the unmanned aerial vehicle landing bracket is in adsorption connection with the second magnet on the plugboard, so that the unmanned aerial vehicle lands with good stability.

2. According to the utility model, the buffer mechanism is arranged, and the landing plate is buffered by the buffer mechanism, so that the landing stability of the unmanned aerial vehicle is further improved.

Drawings

FIG. 1 is a schematic diagram of the structure of the present utility model;

FIG. 2 is a schematic rear view of the present utility model;

FIG. 3 is a schematic view of a board according to the present utility model;

fig. 4 is an enlarged schematic view of the structure of fig. 2 a according to the present utility model.

In the figure: 1. a bottom plate; 2. an anti-slip pad; 3. a landing plate; 4. inserting plate; 5. the unmanned aerial vehicle falls on the bracket; 6. a first magnet; 7. a support cylinder; 8. a positioning cylinder; 9. a mounting plate; 10. a buffer spring; 11. a slide bar; 12. inserting blocks; 13. a second magnet; 14. a handle; 15. a mounting groove; 16. a slot.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1-4, the present utility model provides a technical solution: the utility model provides an unmanned aerial vehicle landing calibration support with alignment structure is inhaled to magnetism, including bottom plate 1, bottom plate 1 top is provided with descending board 3, be provided with buffer gear between descending board 3 and the bottom plate 1, install the mounting groove 15 on descending board 3, slot 16 has all been seted up on the inner wall of mounting groove 15 both sides, the inside picture peg 4 that is provided with of mounting groove 15, picture peg 4 both ends all are fixed with insert 12, insert 12 and slot 16 peg graft, second magnet 13 is all installed to picture peg 4 surface both sides, be provided with unmanned aerial vehicle landing support 5 on the descending board 3, first magnet 6 is installed to unmanned aerial vehicle landing support 5 bottom, first magnet 6 and second magnet 13 magnetism are inhaled and are connected.

Further, buffer gear includes support section of thick bamboo 7, positioning tube 8, buffer spring 10 and slide bar 11, support section of thick bamboo 7 and positioning tube 8 are all fixed on bottom plate 1, descending board 3 bottom is fixed with mounting panel 9, buffer spring 10 one end is fixed on mounting panel 9, the buffer spring 10 other end inserts support section of thick bamboo 7 inside and with support section of thick bamboo 7 inside bottom fixed connection, slide bar 11 is fixed in descending board 3 bottom, slide bar 11 is pegged graft with positioning tube 8, when unmanned aerial vehicle falls on descending board 3, buffer spring 10 atress takes place deformation, thereby impel descending board 3 to move downwards along positioning tube 8 through slide bar 11, the buffering is effectual, unmanned aerial vehicle descending stability has been improved.

Further, the number of the positioning cylinders 8 is two, and the positioning cylinders are symmetrically distributed about the supporting cylinder 7, so that the stability of the landing plate 3 is improved.

Further, the handle 14 is installed on the plugboard 4, the plugboard 4 is inserted into the installation groove 15 through the insertion block 12, and when the plugboard 4 needs cleaning or maintenance, the plugboard 4 can be moved out by the handle 14, and the plugboard 4 is convenient to move out.

Further, the anti-slip pad 2 is adhered to the bottom of the bottom plate 1, and when the bottom plate 1 is placed on the ground, the bottom plate 1 is prevented from slipping through the anti-slip pad 2, so that the placement stability of the bottom plate 1 is improved.

Specifically, when the unmanned aerial vehicle landing support is used, firstly, the bottom plate 1 is carried to move to a proper position, the anti-slip pad 2 is arranged at the bottom of the bottom plate 1, the placement stability of the bottom plate 1 is good, then the unmanned aerial vehicle landing support 5 is controlled by the control equipment to stop on the landing plate 3, at the moment, the first magnet 6 at the bottom of the unmanned aerial vehicle landing support 5 is in adsorption connection with the second magnet 13 on the landing plate 3, the stopping is accurate, the stability is good, the unmanned aerial vehicle is stressed to deform in the landing stopping process, and therefore the landing plate 3 is driven to move downwards along the positioning cylinder 8 through the slide rod 11, the buffering effect is good, and the landing stability of the unmanned aerial vehicle is improved.

In the description of the present utility model, it should be understood that the terms "coaxial," "bottom," "one end," "top," "middle," "another end," "upper," "one side," "top," "inner," "front," "center," "two ends," etc. indicate orientations or positional relationships based on the orientation or positional relationships shown in the drawings, are merely for convenience in describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present utility model.

Furthermore, the terms "first," "second," "third," "fourth," and the like are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated, whereby features defining "first," "second," "third," "fourth" may explicitly or implicitly include at least one such feature.

In the present utility model, unless explicitly specified and limited otherwise, the terms "mounted," "configured," "connected," "secured," "screwed," and the like are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intermediaries, or in communication with each other or in interaction with each other, unless explicitly defined otherwise, the meaning of the terms described above in this application will be understood by those of ordinary skill in the art in view of the specific circumstances.

Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. Unmanned aerial vehicle descends calibration support with alignment structure is inhaled to magnetism, including bottom plate (1), its characterized in that: the utility model discloses a unmanned aerial vehicle landing support, including bottom plate (1), bottom plate (1) top is provided with descending board (3), be provided with buffer gear between descending board (3) and bottom plate (1), mounting groove (15) have been seted up on descending board (3), slot (16) have all been seted up on the inner wall of mounting groove (15) both sides, inside picture peg (4) that are provided with of mounting groove (15), picture peg (4) both ends all are fixed with inserted block (12), inserted block (12) peg graft with slot (16), second magnet (13) are all installed on picture peg (4) surface both sides, be provided with unmanned aerial vehicle landing support (5) on descending board (3), first magnet (6) are installed to unmanned aerial vehicle landing support (5) bottom, first magnet (6) and second magnet (13) magnetism are inhaled and are connected.

2. The unmanned aerial vehicle landing calibration support with a magnetic attraction alignment structure according to claim 1, wherein: the buffer mechanism comprises a supporting cylinder (7), a positioning cylinder (8), a buffer spring (10) and a sliding rod (11), wherein the supporting cylinder (7) and the positioning cylinder (8) are all fixed on a bottom plate (1), a mounting plate (9) is fixed at the bottom of a landing plate (3), one end of the buffer spring (10) is fixed on the mounting plate (9), the other end of the buffer spring (10) is inserted into the supporting cylinder (7) and fixedly connected with the bottom end of the supporting cylinder (7), the sliding rod (11) is fixed at the bottom of the landing plate (3), and the sliding rod (11) is spliced with the positioning cylinder (8).

3. The unmanned aerial vehicle landing calibration support with magnetic attraction alignment structure according to claim 2, wherein: the number of the positioning cylinders (8) is two, and the positioning cylinders are symmetrically distributed about the supporting cylinder (7).

4. The unmanned aerial vehicle landing calibration support with a magnetic attraction alignment structure according to claim 1, wherein: a handle (14) is arranged on the plugboard (4).

5. The unmanned aerial vehicle landing calibration support with a magnetic attraction alignment structure according to claim 1, wherein: the bottom of the bottom plate (1) is adhered with an anti-slip pad (2).