CN218158923U

CN218158923U - Unmanned aerial vehicle group portable control platform

Info

Publication number: CN218158923U
Application number: CN202222277417.5U
Authority: CN
Inventors: 岳鹍; 刘冉; 王宝晶; 郝洋
Original assignee: Tianjin Modern Vocational Technology College
Current assignee: Tianjin Modern Vocational Technology College
Priority date: 2022-08-29
Filing date: 2022-08-29
Publication date: 2022-12-27
Anticipated expiration: 2032-08-29

Abstract

The utility model relates to an unmanned aerial vehicle controlgear technical field provides a unmanned aerial vehicle crowd portable control platform, include: the control mainboard, the display screen, the bottom plate, linear slideway, folding linking arm, main descending platform, first pair descending platform subassembly, the vice descending platform subassembly of second and portable handle, the control mainboard sets up on the bottom plate, the display screen lower extreme is articulated with the bottom plate rear side, two linear slideway settings are in main descending platform both sides, main descending platform passes through linear slideway and bottom plate swing joint, folding linking arm is used for connecting main descending platform and bottom plate, first pair descending platform subassembly sets up at main descending platform upside and articulates with main descending platform one end, the vice descending platform subassembly of second sets up at first pair descending platform subassembly upside, and articulate with main descending platform other end, portable handle sets up in the display screen upper end, the utility model discloses can effectively provide unmanned aerial vehicle crowd's descending place and control platform after expanding, and folding portable, high durability and convenient use.

Description

Unmanned aerial vehicle group portable control platform

Technical Field

The utility model relates to an unmanned aerial vehicle control equipment technical field has especially related to a portable control cabinet of unmanned aerial vehicle group.

Background

Unmanned planes, abbreviated as "drones" in english and "UAVs" in short, are unmanned planes operated by radio remote control devices and self-contained program control devices, or operated autonomously, either completely or intermittently, by an on-board computer, and are often more suitable for tasks that are too "fool, dirty, or dangerous" than unmanned planes, which can be classified into military and civilian applications, depending on the field of application. For military use, unmanned aerial vehicles are divided into reconnaissance aircraft and target drone, and for civil use, unmanned aerial vehicles + industrial application are really just needed for unmanned aerial vehicles; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.

The existing equipment for controlling the unmanned aerial vehicle is generally an unmanned aerial vehicle control platform.

As in application No.: CN201621316597.1 discloses a portable unmanned aerial vehicle control station, which comprises a computer, a battery, an electronic box, a switch assembly, an interface assembly, an antenna, a standby line, a display, and a warning light; the electronic box is a cube, the computer, the battery, the switch assembly and the interface assembly are communicated and then installed inside the electronic box, the antenna, the standby wire, the display and the prompting lamp are installed outside the electronic box respectively, the antenna is communicated with the interface assembly, the display is communicated with the switch assembly and the interface assembly respectively, and the prompting lamp is communicated with the battery.

As in application No.: CN202120922320.8 discloses a portable unmanned aerial vehicle aerial survey control point recognition device, including route intelligent recognition appearance and sealing mechanism, first magic subsides are installed to the inner wall of route intelligent recognition appearance, the polypropylene layer is installed to the outer wall of first magic subsides, one side externally mounted of route intelligent recognition appearance has rotatable sealing mechanism, the second hinge is installed to one side of sealing mechanism.

However, in the prior art, a portable control platform for the unmanned aerial vehicle group is lacked, and when the portable control platform is used, a landing place of the unmanned aerial vehicle group cannot be provided.

SUMMERY OF THE UTILITY MODEL

In order to solve prior art, lack the portable control platform to unmanned aerial vehicle crowd, and when using portable control cabinet, can't provide the problem in the landing place of unmanned aerial vehicle crowd, the utility model provides a portable control cabinet of unmanned aerial vehicle crowd solves this problem.

In order to achieve the above purpose, the utility model provides a following technical scheme:

an unmanned aerial vehicle cluster portable console, comprising: control mainboard, display screen, bottom plate, linear slideway, folding linking arm, main landing platform, first pair of landing platform subassembly, the vice landing platform subassembly of second and portable handle, the control mainboard sets up on the bottom plate, the display screen lower extreme is articulated with the bottom plate rear side, two linear slideway settings are in main landing platform both sides, main landing platform passes through linear slideway and bottom plate swing joint, folding linking arm is used for connecting main landing platform and bottom plate, first pair of landing platform subassembly sets up at main landing platform upside and articulates with main landing platform one end, the vice landing platform subassembly of second sets up at first pair landing platform subassembly upside, and it is articulated with main landing platform other end, portable handle sets up in the display screen upper end.

Preferably, the folding connecting arm comprises: first linking arm, second linking arm, first articulated shaft, second articulated shaft and third articulated shaft, first linking arm one end is articulated through first articulated shaft and bottom plate rear side, and the first linking arm other end is articulated through second articulated shaft and second linking arm one end, and the second linking arm other end is articulated through third articulated shaft and main landing platform.

Preferably, the first secondary landing platform assembly comprises: first pair is descended platform and first folding bracket component, first pair is descended platform one end and is descended platform one end with main articulated, a plurality of first folding bracket component symmetry sets up at first pair and descends platform upside.

Preferably, the first folding bracket assembly comprises: articulated seat, articulated shaft and supporting leg, articulated seat sets up at first pair descending platform upside, and supporting leg one end is passed through the articulated shaft and is articulated with articulated seat, and the supporting leg top is provided with the vice descending platform subassembly of second.

Preferably, the second sub-landing platform assembly comprises: the vice landing platform of second and the folding bracket component of second, the vice landing platform one end of second is articulated with the main landing platform other end, and is a plurality of the folding bracket component symmetry of second sets up at the vice landing platform upside of second.

Preferably, the second folding bracket assembly is identical in structure to the first folding bracket assembly.

Preferably, the supporting leg other end is provided with the magnetite, first pair descending platform material is the magnetic metal material.

Preferably, the second pair of landing platform other end still is provided with first magnet, first pair of landing platform one end still is provided with the second magnet, first magnet and second magnet magnetism are opposite, and first magnet and the cooperation of second magnet are used.

The utility model has the advantages of: the utility model discloses an adopt linear slide rail and folding linking arm, with control mainboard and display screen part and the partial folding joint of main landing platform, when needs use, expand linear slide rail and folding linking arm, make control mainboard and the separation of main landing platform, the staff's operation of both being convenient for can make things convenient for unmanned aerial vehicle to descend, and use folding first pair landing platform subassembly, the vice landing platform subassembly of second, can enlarge the descending area, through using portable handle, when putting up whole device again, use portable handle and conveniently carry.

Drawings

The accompanying drawings, which form a part hereof, are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the invention without undue limitation. In the drawings:

FIG. 1 is a perspective view of the fully expanded structure of the present invention;

FIG. 2 is an isometric view of the collapsed construction of the present invention;

FIG. 3 is a structural perspective view of the foldable connecting arm of the present invention;

figure 4 is a structural isometric view of the first set of landing platform assemblies of the present invention;

fig. 5 is a structural isometric view of a first folding bracket assembly of the present invention;

figure 6 is a structural isometric view of a second auxiliary landing platform assembly of the present invention;

fig. 7 is a structural axial view of the first and second magnets of the present invention.

Description of reference numerals:

1. a control main board; 2. a display screen; 3. a base plate; 4. a linear slide rail; 5. folding the connecting arm; 6. a main landing platform; 7. a first secondary landing platform assembly; 8. a second auxiliary landing platform assembly; 9. a portable handle; 51. a first connecting arm; 52. a second connecting arm; 53. a first hinge shaft; 54. a second hinge shaft; 55. a third hinge shaft; 71. a first secondary landing platform; 72. a first folding bracket assembly; 721. a hinged seat; 722. hinging a shaft; 723. supporting legs; 81. a second auxiliary landing platform; 82. a second folding bracket assembly; 724. a magnet; 811. a first magnet; 711. a second magnet.

Detailed Description

It should be noted that, in the case of no conflict, the embodiments and features of the embodiments of the present invention may be combined with each other.

In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are used merely for convenience of description and for simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention. Furthermore, the terms "first", "second", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first," "second," etc. may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.

Example (b):

with reference to fig. 1 and 2, a drone group portable console includes: control mainboard 1, display screen 2, bottom plate 3, linear slide 4, folding linking arm 5, main landing platform 6, first pair landing platform subassembly 7, the vice landing platform subassembly 8 of second and portable handle 9, control mainboard 1 sets up on bottom plate 3, and control mainboard 1 is used for controlling unmanned aerial vehicle to take off, cruises, descends, and control mainboard 1 is used for prior art, no longer gives unnecessary details here.

2 lower extremes of display screen are articulated with 3 rear sides of bottom plate, and display screen 2 is used for showing unmanned aerial vehicle's the picture of taking photo by plane, and the operating personnel of being convenient for knows unmanned aerial vehicle's current position and developments in real time, and 2 accessible articulated shafts of display screen expand or merge, the operation of being convenient for during the expansion, and the protection screen of being convenient for during the merge is not harmed, and display screen 2 is no longer repeated here for prior art.

Two linear slideway 4 sets up in main landing platform 6 both sides, and main landing platform 6 passes through linear slideway 4 and bottom plate 3 swing joint, and main landing platform 6 expandes or folds with 3 accessible linear slideway 4 of bottom plate, when needs use, takes main landing platform 6 out through linear slideway 4, when need not use, withdraws main landing platform 6, has reduced the whole volume that occupies when carrying, and linear slideway 4 is prior art, no longer gives unnecessary details here.

Folding linking arm 5 is used for connecting main landing platform 6 and bottom plate 3, and folding linking arm 5 can prevent to connect main landing platform 6 roll-off under the effect of gravity, harm important part when avoiding carrying.

First pair of descending platform assembly 7 sets up at 6 upsides of main descending platform and is articulated with 6 one end of main descending platform, the vice descending platform assembly 8 of second sets up at first pair 7 upsides of descending platform assembly, and it is articulated with 6 other ends of main descending platform, portable handle 9 sets up in 2 upper ends of display screen, so set up, first pair descending platform assembly 7 and the vice descending platform assembly 8 of second can expand, be convenient for many unmanned aerial vehicle's descending, when need not use, fold can, portable handle 9 convenient to use personnel carry.

As explained in connection with fig. 3, the folding connecting arm 5 comprises: the main landing platform comprises a first connecting arm 51, a second connecting arm 52, a first hinge shaft 53, a second hinge shaft 54 and a third hinge shaft 55, wherein one end of the first connecting arm 51 is hinged with the rear side of the bottom plate 3 through the first hinge shaft 53, the other end of the first connecting arm 51 is hinged with one end of the second connecting arm 52 through the second hinge shaft 54, the other end of the second connecting arm 52 is hinged with the main landing platform 6 through the third hinge shaft 55, and the arrangement is characterized in that one end of the first connecting arm 51 can rotate around the first hinge shaft 53, the other end of the first connecting arm 51 can rotate around one end of the second connecting arm 52, the other end of the second connecting arm 52 can rotate around the third hinge shaft 55, and due to the fact that the friction force of the linear sliding rail 4 is small, when the main landing platform 6 is in a vertical carrying state, the main landing platform 6 can slide down under the action of gravity, and the gravity action can be counteracted and the main landing platform 6 can be prevented from sliding out by arranging the first connecting arm 51 and the second connecting arm 52.

As explained in connection with fig. 4, the first secondary landing platform assembly 7 comprises: the first auxiliary landing platform 71 and the first folding support assembly 72 are arranged, one end of the first auxiliary landing platform 71 is hinged to one end of the main landing platform 6, the first folding support assembly 72 is symmetrically arranged on the upper side of the first auxiliary landing platform 71, and therefore when the first folding support assembly is required to be used, the first auxiliary landing platform 71 and the first folding support assembly 72 are opened, and the first folding support assembly 72 plays a role in supporting the first auxiliary landing platform 71.

As will be described in conjunction with fig. 5, the first folding bracket assembly 72 includes: the hinged base 721, the articulated shaft 722 and the supporting leg 723, the hinged base 721 is arranged on the upper side of the first auxiliary landing platform 71, one end of the supporting leg 723 is hinged with the hinged base 721 through the articulated shaft 722, the second auxiliary landing platform assembly 8 is arranged above the supporting leg 723, the supporting leg 723 can rotate around the articulated shaft 722, when the supporting is needed, the supporting leg 723 is in contact with a supporting surface, and the supporting leg 723 can support the first auxiliary landing platform 71 to be horizontal after being unfolded.

As explained in connection with fig. 6, the second auxiliary landing platform assembly 8 comprises: the vice landing platform 81 of second and the folding bracket component 82 of second, the vice landing platform 81 one end of second is articulated with the main landing platform 6 other end, and is a plurality of the folding bracket component 82 symmetry of second sets up in the vice landing platform 81 upside of second.

The second folding bracket assembly 82 is identical in construction to the first folding bracket assembly 72.

The supporting leg 723 other end is provided with magnetite 724, first pair of landing platform 71 material is the magnetic metal material, so sets up, and magnetite 724 can guarantee that the supporting leg 723's of withdrawing supports the end and adsorbs at first pair of landing platform 71, and supporting leg 723 rotates round articulated shaft 722 when preventing to carry.

As described with reference to fig. 7, the other end of the second auxiliary landing platform 81 is further provided with a first magnet 811, one end of the first auxiliary landing platform 71 is further provided with a second magnet 711, the first magnet 811 is opposite to the second magnet 711 in magnetism, and the first magnet 811 is used in cooperation with the second magnet 711, so that when the second auxiliary landing platform 81 and the first auxiliary landing platform 71 are retracted, the first magnet 811 contacts with the second magnet 711 to generate an adsorption magnetic force, thereby preventing the second auxiliary landing platform 81 and the first auxiliary landing platform 71 from rotating around the hinge shaft with the main landing platform 6 during carrying.

The utility model discloses a theory of operation: the utility model discloses when using, pull open main landing platform 6, expand display screen 2, then open the vice landing platform 81 of second and first pair landing platform 71 according to the order, and open the vice landing platform 81 of second and the supporting leg on the first pair landing platform 71, make the vice landing platform 81 of second and first pair landing platform 71 keep the level, form as shown unmanned aerial vehicle crowd control platform in figure 1, after using up, folding supporting leg, pack up the vice landing platform 81 of second and first pair landing platform 71, make first magnet 811 and second magnet 711 contact, guarantee that the vice landing platform 81 of second and first pair landing platform 71 can not the drunkenness, then fold main landing platform 6 and bottom plate 3, pack up display screen 2, form as shown in figure 2, the portable handle 9 of rethread carries, the utility model discloses rational in infrastructure, convenient to use can effectively provide the landing place and the control platform of unmanned aerial vehicle crowd after expanding, and pack up back portable.

It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof; the present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

The above, only do the preferred embodiment of the present invention, not used to limit the present invention, all the technical matters of the present invention should be included in the protection scope of the present invention for any slight modification, equivalent replacement and improvement of the above embodiments.

Claims

1. An unmanned aerial vehicle cluster portable console, comprising: control mainboard (1) and display screen (2), its characterized in that still includes: bottom plate (3), linear slide rail (4), folding linking arm (5), main descending platform (6), first pair descending platform subassembly (7), the vice descending platform subassembly of second (8) and portable handle (9), control mainboard (1) sets up on bottom plate (3), display screen (2) lower extreme is articulated with bottom plate (3) rear side, two linear slide rail (4) set up and descend platform (6) both sides at main, main descending platform (6) are through linear slide rail (4) and bottom plate (3) swing joint, folding linking arm (5) are used for connecting main descending platform (6) and bottom plate (3), first pair platform subassembly (7) set up and descend platform (6) upside and articulate with main descending platform (6) one end at main, the vice landing platform subassembly of second (8) set up and descend platform subassembly (7) upside at first pair to articulate with main descending platform (6) other end, portable handle (9) set up and descend platform (2) upper end at display screen (2).

2. The drone group portable console according to claim 1, characterized in that the folding connection arm (5) comprises: first linking arm (51), second linking arm (52), first articulated shaft (53), second articulated shaft (54) and third articulated shaft (55), first linking arm (51) one end is articulated through first articulated shaft (53) and bottom plate (3) rear side, and first linking arm (51) other end is articulated through second articulated shaft (54) and second linking arm (52) one end, and second linking arm (52) other end is articulated through third articulated shaft (55) and main landing platform (6).

3. The drone swarm portable console according to claim 1, wherein the first secondary landing platform assembly (7) comprises: first pair is descended platform (71) and first folding bracket component (72), first pair is descended platform (71) one end and is descended platform (6) one end with main articulated, and is a plurality of first folding bracket component (72) symmetry sets up in first pair and descends platform (71) upside.

4. The drone swarm portable console according to claim 3, wherein the first folding bracket assembly (72) includes: articulated seat (721), articulated shaft (722) and supporting leg (723), articulated seat (721) set up in first vice landing platform (71) upside, and supporting leg (723) one end is passed through articulated shaft (722) and is articulated with articulated seat (721), and supporting leg (723) top is provided with vice landing platform subassembly of second (8).

5. The drone swarm portable console according to claim 4, wherein the second secondary landing platform assembly (8) comprises: the vice landing platform of second (81) and the folding bracket component of second (82), the vice landing platform of second (81) one end is articulated with main landing platform (6) other end, and is a plurality of folding bracket component of second (82) symmetry sets up in the vice landing platform of second (81) upside.

6. The drone swarm portable console of claim 5, wherein the second folding support assembly (82) is structurally identical to the first folding support assembly (72).

7. The unmanned aerial vehicle fleet portable console according to claim 4, wherein, magnets (724) are disposed at the other ends of the supporting legs (723), and the first auxiliary landing platform (71) is made of magnetic metal.

8. The drone group portable console according to claim 4, wherein the second secondary landing platform (81) is further provided with a first magnet (811) at the other end, the first secondary landing platform (71) is further provided with a second magnet (711) at one end, the first magnet (811) and the second magnet (711) are opposite in magnetism, and the first magnet (811) and the second magnet (711) are used in cooperation.