CN220199624U

CN220199624U - Unmanned aerial vehicle ground station

Info

Publication number: CN220199624U
Application number: CN202321297999.1U
Authority: CN
Inventors: 邱暾; 郑伟; 王琨; 吕帅; 马思雨; 夏学毅
Original assignee: Liaoning Pangu Technology Co ltd
Current assignee: Liaoning Pangu Technology Co ltd
Priority date: 2023-05-26
Filing date: 2023-05-26
Publication date: 2023-12-19
Anticipated expiration: 2033-05-26

Abstract

The utility model discloses an unmanned aerial vehicle ground station, which comprises two bases, wherein one sides of the two bases adjacent to each other are respectively fixedly provided with a slide way and a slide way, the two bases are connected through the slide way and the slide way, and the tops of the two bases are fixedly provided with two buffer components.

Description

Unmanned aerial vehicle ground station

Technical Field

The utility model relates to the technical field of unmanned aerial vehicle ground stations, in particular to an unmanned aerial vehicle ground station.

Background

Unmanned aircraft is called unmanned aircraft for short, is unmanned aircraft that utilizes radio remote control equipment and self-contained program control device to operate, unmanned aircraft is in fact the collective term of unmanned aircraft, can divide into unmanned fixed wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned many rotor crafts, unmanned umbrella wing aircraft etc. from technical angle definition, ground station is as the operation command center of whole unmanned aircraft system, and its control content includes the flight course of aircraft, flight path, the mission function of payload, the normal work of communication link, and the transmission and the recovery of aircraft.

The unmanned aerial vehicle ground station that uses often is shut down the platform and exists and occupy the volume great, inconvenient circumstances of accomodating when idle can produce the impact with shutting down the platform when falling to the ground simultaneously current unmanned aerial vehicle, leads to unmanned aerial vehicle to produce unstable condition when taking off and land easily, can cause unmanned aerial vehicle to overturn, the safety problem such as roll has increased unmanned aerial vehicle damage's risk.

Disclosure of Invention

The utility model aims to provide an unmanned aerial vehicle ground station for solving the problems in the background art.

In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an unmanned aerial vehicle ground station, includes two bases, two the base sets up for the front and back, two the adjacent one side of base is fixed slide and spout respectively, two the base is connected through slide and spout, the fixed elasticity card ball that is provided with in top and the bottom of slide, the draw-in groove corresponding with elasticity card ball has been seted up at top and bottom in the spout, two the fixed two buffer components that are provided with in top of base.

Preferably, the buffer assembly comprises two brackets, two slide bars, two sliding blocks, two groups of springs, two groups of supporting rods and a stopping platform, wherein the two brackets are fixedly arranged at the top of the base, the two sliding bars are fixedly arranged between the two brackets, the two sliding blocks are movably sleeved on the two slide bars, the two groups of springs are fixedly arranged between the two sliding blocks and the two brackets, the two sliding bars are positioned at the inner sides of the two groups of springs, one ends of the two groups of supporting rods are movably connected with the tops of the two sliding blocks, and the bottom of the stopping platform is movably connected with the other ends of the two groups of supporting rods.

Preferably, the number of the springs in each group is two, and the number of the struts in each group is also two.

Preferably, a limiting plate is fixedly arranged on the left side of the sliding groove.

Preferably, a rubber pad is fixedly arranged at the top of the shutdown platform.

Compared with the prior art, the utility model has the beneficial effects that: according to the utility model, vibration and impact caused by the unmanned aerial vehicle in the landing process can be effectively reduced through the arrangement of the buffer assembly, damage of the unmanned aerial vehicle in the landing process is reduced, shaking of the unmanned aerial vehicle in the landing process can be reduced to a certain extent through the arrangement of the buffer assembly, influence caused by weather factors such as wind power, air flow and the like is reduced, a smoother and safer environment is provided for the landing of the unmanned aerial vehicle, two bases can be spliced together through the arrangement of the slide way and the slide groove, the assembly and disassembly operations are simple, the unmanned aerial vehicle can be conveniently moved to different working sites, and the unmanned aerial vehicle is convenient to store and carry.

Drawings

FIG. 1 is a schematic diagram of an axial structure of two bases of the present utility model when assembled;

FIG. 2 is a schematic diagram of an axial structure of a base and a buffer assembly according to the present utility model;

FIG. 3 is a schematic diagram of an axial structure of a damper assembly according to the present utility model;

FIG. 4 is a schematic diagram of an axial structure of a chute, a clamping slot and a positioning plate according to the present utility model;

fig. 5 is a schematic diagram of the axial structure of the slide way and the elastic clamping ball of the present utility model.

In the figure: 1. a base; 2. a slideway; 3. a chute; 4. an elastic clamping ball; 5. a clamping groove; 6. a buffer assembly; 61. a bracket; 62. a slide bar; 63. a slide block; 64. a spring; 65. a support rod; 66. a shutdown platform; 7. a limiting plate; 8. and a rubber pad.

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. 1-5, the utility model provides an unmanned aerial vehicle ground station, which comprises two bases 1, wherein the two bases 1 are arranged front and back, one side of each base 1 adjacent to the other base is fixedly provided with a slide way 2 and a slide way 3, the slide way 2 is connected with the front base 1, the slide way 3 is connected with the rear base 1, the slide way 2 is in sliding connection with the slide way 3, the two bases 1 are connected with the slide way 3 through the slide way 2 and the slide way 3, the top and the bottom of the slide way 2 are fixedly provided with elastic clamping balls 4, the top and the bottom of the slide way 3 are provided with clamping grooves 5 corresponding to the elastic clamping balls 4, when the elastic clamping balls 4 on the slide way 2 are inserted into the slide way 3, the clamping grooves 5 in the slide way 3 are provided with increased stability of connection between the slide way 2 and the slide way 3, the top of the two bases 1 is fixedly provided with two buffer assemblies 6, and the buffer assemblies 6 are used for buffering impact force of the unmanned aerial vehicle during landing.

Specifically, the buffer assembly 6 includes two brackets 61, two slide bars 62, two sliding blocks 63, two sets of springs 64, two sets of struts 65 and a stopping platform 66, two brackets 61 are fixedly arranged at the top of the base 1, two brackets 61 are arranged left and right, two sliding bars 62 are fixedly arranged between two brackets 61, two sliding bars 62 are arranged front and back, two sliding blocks 63 are movably sleeved on two sliding bars 62, two sets of springs 64 are fixedly arranged between two sliding blocks 63 and two brackets 61, two sliding bars 62 are located on the inner sides of two sets of springs 64, one ends of two sets of struts 65 are movably connected with the tops of two sliding blocks 63, the bottom of the stopping platform 66 is movably connected with the other ends of two sets of struts 65, the unmanned aerial vehicle can impact the stopping platform 66, impact force can act on the struts 65, the struts 65 can squeeze the sliding blocks 63 and the springs 64 towards two sides, the springs 64 can repeatedly elastically shrink after being squeezed, so that the impact force can be counteracted, and the shock and the impact force caused by the unmanned aerial vehicle in the landing process can be reduced.

Specifically, the number of springs 64 per set is two, as are the number of struts 65 per set.

Specifically, a limiting plate 7 is fixedly arranged on the left side of the chute 3, and the limiting plate 7 is used for positioning the sliding block 63.

Specifically, the top of the shutdown platform 66 is fixedly provided with a rubber pad 8, and the rubber pad 8 increases the friction between the shutdown platform 66 and the unmanned aerial vehicle.

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. An unmanned aerial vehicle ground station, characterized in that: including two base (1), two base (1) are the front and back setting, two base (1) are adjacent one side is fixed respectively and is provided with slide (2) and spout (3), two base (1) are connected through slide (2) and spout (3), the top and the bottom of slide (2) are fixed to be provided with elasticity card ball (4), draw-in groove (5) corresponding with elasticity card ball (4) have been seted up to top and bottom in spout (3), two the fixed two buffer modules (6) that are provided with in top of base (1).

2. A drone ground station as claimed in claim 1, wherein: the buffer assembly (6) comprises two supports (61), two sliding rods (62), two sliding blocks (63), two groups of springs (64), two groups of supporting rods (65) and a stopping platform (66), wherein the two supports (61) are fixedly arranged at the top of the base (1), the two sliding rods (62) are fixedly arranged between the two supports (61), the two sliding blocks (63) are movably sleeved on the two sliding rods (62), two groups of springs (64) are fixedly arranged between the two sliding blocks (63) and the two supports (61), the two sliding rods (62) are located on the inner sides of the two groups of springs (64), one ends of the supporting rods (65) are movably connected with the tops of the two sliding blocks (63), and the bottoms of the stopping platform (66) are movably connected with the other ends of the two groups of the supporting rods (65).

3. A drone ground station according to claim 2, wherein: the number of the springs (64) in each group is two, and the number of the supporting rods (65) in each group is also two.

4. A drone ground station as claimed in claim 1, wherein: a limiting plate (7) is fixedly arranged on the left side of the sliding groove (3).

5. A drone ground station according to claim 2, wherein: a rubber pad (8) is fixedly arranged at the top of the stopping platform (66).