CN219008162U

CN219008162U - Unmanned aerial vehicle equipment of collapsible accomodate

Info

Publication number: CN219008162U
Application number: CN202222962580.5U
Authority: CN
Inventors: 刘家洲
Original assignee: Shandong Vane Zhihang Equipment Co ltd
Current assignee: Shandong Vane Zhihang Equipment Co ltd
Priority date: 2022-11-08
Filing date: 2022-11-08
Publication date: 2023-05-12
Anticipated expiration: 2032-11-08

Abstract

The utility model discloses foldable unmanned aerial vehicle equipment which comprises a mounting plate, wherein the outer side of the mounting plate is connected with a positioning plate at equal angles, a first supporting plate is arranged at the bottom of the positioning plate, the positioning plate is connected with the first supporting plate through a locking bolt, a plurality of first through holes are annularly formed in the top of one end of the first supporting plate, a second supporting plate is arranged above the first supporting plate, the first supporting plate is connected with the second supporting plate through a working bearing, second through holes are annularly distributed in the top of one end of the second supporting plate, locking screws penetrate through the second through holes, and the locking screws are matched with the first through holes; this device can fold rotatory to unmanned aerial vehicle's wing, conveniently accomodate unmanned aerial vehicle when not using, and the ball height-adjustable that makes a video recording of device simultaneously is applicable to different topography, has improved the practicality of device.

Description

Unmanned aerial vehicle equipment of collapsible accomodate

Technical Field

The utility model relates to the technical field of unmanned aerial vehicle equipment, in particular to foldable unmanned aerial vehicle equipment.

Background

Unmanned aerial vehicles, abbreviated as "unmanned aerial vehicles", abbreviated as "UAVs", are unmanned aerial vehicles that are operated by means of radio remote control devices and self-contained programmed control devices, or are operated autonomously, either entirely or intermittently, by an onboard computer.

Unmanned aircraft tend to be more suitable for tasks that are too "fooled, messy, or dangerous" than manned aircraft. Unmanned aerial vehicles can be classified into military and civilian applications according to the field of application. For military purposes, unmanned aerial vehicles are classified into reconnaissance and drones. In civil aspect, the unmanned aerial vehicle and the industrial application are really just needed by the unmanned aerial vehicle; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer shooting, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, 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 the developed countries are also actively expanding the application of industries and developing unmanned aerial vehicle technologies.

The existing unmanned aerial vehicle equipment cannot fold the wings when in use, so that the unmanned aerial vehicle occupies a large space, and is inconvenient to store when not in use, so that the unmanned aerial vehicle is troublesome to carry, and the daily use of a user is affected.

Therefore, the utility model provides the foldable unmanned aerial vehicle equipment for storage, which solves the problems in the prior art.

Disclosure of Invention

The utility model provides foldable unmanned aerial vehicle equipment, which solves the problems that the existing unmanned aerial vehicle equipment cannot fold wings when in use, so that the unmanned aerial vehicle occupies a large space, the unmanned aerial vehicle is inconvenient to store when not in use, the unmanned aerial vehicle is troublesome to carry, and the daily use of a user is influenced.

In order to solve the problems, the utility model provides foldable unmanned aerial vehicle equipment which comprises a mounting disc, wherein the outer side of the mounting disc is connected with a positioning plate in an equal angle, a first supporting plate is arranged at the bottom of the positioning plate, the positioning plate is connected with the first supporting plate through a locking bolt, a plurality of first through holes are annularly formed in the top of one end of the first supporting plate, a second supporting plate is arranged above the first supporting plate, the first supporting plate is connected with the second supporting plate through a working bearing, second through holes are annularly distributed in the top of one end of the second supporting plate, locking screws penetrate through the second through holes, and the locking screws are matched with the first through holes.

Preferably, a rotating rod is installed at one end of the second supporting plate, a plurality of fan blades are welded on the outer wall of the rotating rod in an annular mode, and a motor is arranged at the input end of the rotating rod.

Preferably, the bottom symmetry of mounting disc is equipped with two landing legs, the bottom fixedly connected with base of landing leg, the bottom of base is equipped with the rubber pad.

Preferably, the bottom symmetry of mounting disc is connected with the working plate, first rectangular hole has been seted up to the inside of working plate, the second rectangular hole that is linked together with first rectangular hole has been seted up to one side of working plate.

Preferably, the inside sliding connection of first rectangular hole has the diaphragm, one side fixedly connected with silk post of diaphragm, the silk post runs through the second rectangular hole, the one end threaded connection of silk post has the locking dish, the locking dish contacts with the working plate.

Preferably, a camera ball is mounted at one end of the transverse plate.

The beneficial effects of the utility model are as follows: when needs are folding to unmanned aerial vehicle's wing, make locking screw break away from locking state, rotate the second backup pad under the work bearing effect afterwards, after second backup pad angular adjustment is accomplished, first through-hole and second through-hole coincidence simultaneously, rotate locking screw again, locking screw and first through-hole looks adaptation, be convenient for to unmanned aerial vehicle's wing, conveniently accomodate and carry, when needs are adjusted the height of ball of making a video recording, the diaphragm drives the ball of making a video recording, and rotate the locking dish through the silk post, locking dish and working plate contact, be convenient for adjust and fix the mounted position of ball of making a video recording, this device can fold rotatory to unmanned aerial vehicle's wing, convenience is accomodate unmanned aerial vehicle when not using, the ball height-adjustable of making a video recording of device simultaneously is applicable to different topography, the practicality of device has been improved.

Drawings

FIG. 1 is a schematic view of the overall closure structure of the present utility model;

FIG. 2 is a schematic view of the overall open structure of the present utility model;

FIG. 3 is a schematic view of the overall bottom structure of the present utility model;

fig. 4 is an enlarged schematic view of the structure of fig. 3 a according to the present utility model.

Wherein: 1. a mounting plate; 2. a positioning plate; 3. a first support plate; 4. a locking bolt; 5. a first through hole; 6. a second support plate; 7. a second through hole; 8. locking the screw rod; 9. a rotating lever; 10. a fan blade; 11. a support leg; 12. a base; 13. a work plate; 14. a first rectangular hole; 15. a second rectangular hole; 16. a cross plate; 17. a camera ball; 18. and (5) a silk column.

Detailed Description

The present utility model will be further described in detail with reference to the following examples, which are only for the purpose of illustrating the utility model and are not to be construed as limiting the scope of the utility model.

According to the fig. 1, 2, 3 show, this embodiment provides a collapsible unmanned aerial vehicle equipment of accomodating, including mounting disc 1, the outside equiangular connection of mounting disc 1 has locating plate 2, first backup pad 3 is installed to the bottom of locating plate 2, be connected through locking bolt 4 between locating plate 2 and the first backup pad 3, a plurality of first through-holes 5 have been seted up to the annular top of one end of first backup pad 3, the top of first backup pad 3 is equipped with second backup pad 6, be connected through working bearing between first backup pad 3 and the second backup pad 6, the annular distribution of one end top of second backup pad 6 has second through-holes 7, locking screw 8 has been run through to the inside of second through-hole 7, locking screw 8 and the looks adaptation of first through-hole 5.

The dwang 9 is installed to the one end of second backup pad 6, the outer wall annular welding of dwang 9 has a plurality of flabellums 10, the input of dwang 9 is equipped with the motor, drives dwang 9 through the motor and rotates, and dwang 9 drives flabellum 10 rotation, provides the kinetic energy.

The bottom symmetry of mounting disc 1 is equipped with two landing legs 11, the bottom fixedly connected with base 12 of landing leg 11, the bottom of base 12 is equipped with the rubber pad, offsets the impulsive force that produces when some descends through the rubber pad, has improved the barrier propterty of product.

The bottom symmetry of mounting disc 1 is connected with work board 13, first rectangular hole 14 has been seted up to the inside of work board 13, the second rectangular hole 15 that is linked together with first rectangular hole 14 has been seted up to one side of work board 13, the inside sliding connection of first rectangular hole 14 has diaphragm 16, one side fixedly connected with silk post 18 of diaphragm 16, silk post 18 runs through second rectangular hole 15, the one end threaded connection of silk post 18 has the locking dish, the locking dish contacts with work board 13, camera ball 17 is installed to the one end of diaphragm 16, adjusts the height of diaphragm 16 through first rectangular hole 14, and diaphragm 16 drives camera ball 17 to rotate the locking dish through silk post 18, the locking dish contacts with work board 13, is convenient for adjust and fix the mounted position of camera ball 17.

The working principle of the foldable unmanned aerial vehicle device provided by the utility model is as follows:

when using, when needs fold unmanned aerial vehicle's wing, make locking screw 8 break away from locking state, then rotate second backup pad 6 under the work bearing effect, after second backup pad 6 angle modulation is accomplished, simultaneously first through-hole 5 and second through-hole 7 coincide, rotate locking screw 8 once more, locking screw 8 and first through-hole 5 looks adaptation, be convenient for accomodate and carry unmanned aerial vehicle's wing, when needs are to the height of making a video recording ball 17 be adjusted, adjust the height of diaphragm 16 through first rectangular hole 14, diaphragm 16 drives the ball 17 of making a video recording, and rotate the locking dish through silk post 18, the locking dish contacts with work plate 13, be convenient for adjust and fix the mounted position of ball 17 of making a video recording.

Compared with the related art, the foldable unmanned aerial vehicle device provided by the utility model has the following beneficial effects:

when this device needs to fold unmanned aerial vehicle's wing, make locking screw 8 break away from locking state, rotate second backup pad 6 under the work bearing effect then, after second backup pad 6 angle modulation is accomplished, simultaneously first through-hole 5 and the coincidence of second through-hole 7, rotate locking screw 8 once more, locking screw 8 and first through-hole 5 looks adaptation, be convenient for to unmanned aerial vehicle's wing, conveniently accomodate and carry, when need highly adjusting shooting ball 17, adjust diaphragm 16's height through first rectangular hole 14, diaphragm 16 drives shooting ball 17, and rotate the locking dish through silk post 18, the locking dish contacts with work plate 13, be convenient for adjust and fix shooting ball 17's mounted position, this device can fold rotatory unmanned aerial vehicle's wing, convenient accomodate unmanned aerial vehicle when not using, the shooting ball 17 height-adjustable of device simultaneously, be applicable to different topography, the practicality of device has been improved.

The foregoing description is only illustrative of the present utility model and is not intended to limit the scope of the utility model, and all equivalent structures or equivalent processes or direct or indirect application in other related technical fields are included in the scope of the present utility model.

Claims

1. Unmanned aerial vehicle equipment of collapsible accomodating, including mounting disc (1), its characterized in that: the outside equiangle of mounting disc (1) is connected with locating plate (2), first backup pad (3) are installed to the bottom of locating plate (2), be connected through locking bolt (4) between locating plate (2) and first backup pad (3), a plurality of first through-holes (5) have been seted up to the one end top annular of first backup pad (3), the top of first backup pad (3) is equipped with second backup pad (6), be connected through working bearing between first backup pad (3) and second backup pad (6), the one end top annular distribution of second backup pad (6) has second through-hole (7), the inside of second through-hole (7) is run through and is had locking screw (8), locking screw (8) and first through-hole (5) looks adaptation.

2. The foldable stowable drone device of claim 1, wherein: the utility model discloses a fan, including second backup pad, rotatory pole (9) are installed to one end of second backup pad (6), the outer wall annular welding of rotatory pole (9) has a plurality of flabellum (10), the input of rotatory pole (9) is equipped with the motor.

3. The foldable stowable drone device of claim 1, wherein: two supporting legs (11) are symmetrically arranged at the bottom of the mounting plate (1), a base (12) is fixedly connected to the bottom of each supporting leg (11), and a rubber pad is arranged at the bottom of each base (12).

4. The foldable stowable drone device of claim 1, wherein: the bottom symmetry of mounting disc (1) is connected with work board (13), first rectangular hole (14) have been seted up to the inside of work board (13), second rectangular hole (15) that are linked together with first rectangular hole (14) are seted up to one side of work board (13).

5. The foldable stowable drone device of claim 4, wherein: the inside sliding connection of first rectangular hole (14) has diaphragm (16), one side fixedly connected with silk post (18) of diaphragm (16), silk post (18) run through second rectangular hole (15), the one end threaded connection of silk post (18) has the locking dish, locking dish and working plate (13) contact.

6. The foldable stowable drone device of claim 5, wherein: one end of the transverse plate (16) is provided with a shooting ball (17).