Double-slope-shaped top cover structure for unmanned aerial vehicle parking apron

Abstract

The utility model provides a double-slope-shaped top cover structure for an unmanned aerial vehicle parking apron, and relates to the technical field of unmanned aerial vehicle supporting facilities. A parking apron supporting plate is installed in the parking apron body, the unmanned aerial vehicle is located at the top of the parking apron supporting plate, and a multi-section push rod is installed in the parking apron body and connected with the parking apron supporting plate. The top of the parking apron body is symmetrically connected with two protective cover plates, the protective cover plates are located at the top of the unmanned aerial vehicle, and pulleys are installed at the tops of the two ends of the parking apron body. When the unmanned aerial vehicle lands to the top of the parking apron supporting plate, the multi-section push rod drives the parking apron supporting plate to fall back downwards and reset, the parking apron supporting plate is separated from the inner sides of the two protective cover plates, the driving motor drives the rope winding wheel to rotate reversely, the protective cover plates rotate and reset gradually under the influence of gravity, and the two protective cover plates are in a closed state; the top of the unmanned aerial vehicle is sealed and waterproof through the protective cover plate, the unmanned aerial vehicle is effectively prevented from being exposed to the sun and rain, and the service life of the unmanned aerial vehicle is prolonged.

Description

Technical Field

[0001] The utility model relates to the technical field of supporting facilities for unmanned aerial vehicles, and in particular to a double-slope top cover structure for an unmanned aerial vehicle landing pad. Background Art

[0002] With the development of drone technology, the role of drones has become more and more extensive. They can be used for military exploration, terrain mapping, urban security patrols, power grid inspections, etc. At present, one of the bottlenecks restricting the application of drones is battery life. Providing relay services for drones to land and charge is one of the effective means to solve the application obstacles of drones caused by mileage, so drone landing pads have appeared.

[0003] Most existing drone landing pads are designed to be open-air, lacking effective sealing protection for drones. This can easily accelerate the aging of the drone's own plastic components and shorten their service life. In addition, when extremely bad weather occurs outside, it can easily cause damage to the open-air drones, resulting in poor application effects. Utility Model Content

[0004] The present invention relates to a double-slope roof structure for a drone landing pad, which solves the problem that existing drone landing pads are mostly open-air in design, lack effective sealing protection for drones, easily accelerate the aging of plastic parts of the drones themselves, shorten the service life, and easily cause damage to the open-air drones when extremely bad weather occurs outside, resulting in poor application effect.

[0005] In a first aspect of the present disclosure, a double-slope roof structure for an unmanned aerial vehicle apron is provided, specifically comprising: an apron main body; a apron pallet is installed inside the apron main body, the unmanned aerial vehicle is located on the top of the apron pallet, and a multi-section push rod is installed inside the apron main body, and the multi-section push rod is connected to the apron pallet; two protective cover plates are symmetrically connected to the top of the apron main body, the protective cover plates are located on the top of the unmanned aerial vehicle, and pulleys are installed on the top of both ends of the apron main body; rope winding wheels are installed on both outer sides of the apron main body, and steel wire ropes are wound around the outside of the rope winding wheels, and the steel wire ropes are connected to the protective cover plates; a synchronous belt is connected to one end of the rope winding wheel, and the synchronous belt is connected to the two rope winding wheels; a drive motor is fixedly installed on the outside of the apron main body by bolts, and the drive shaft of the drive motor is connected to the rope winding wheel.

[0006] Furthermore, the protective cover is rotatably connected to the apron body, and the rotation angle of the protective cover is 0 to 55 degrees. The two protective covers are in contact with each other in the combined state, and the protective cover is buckled on the top of the apron body.

[0007] Furthermore, external connecting frames are provided on both outer sides of the apron body, and a rope winding wheel is rotatably connected to the external connecting frames. A pulling hole is provided on the top side of the protective cover plate, one end of the steel wire rope is connected to the pulling hole, and the other end of the steel wire rope is connected to the rope winding wheel.

[0008] Furthermore, the pulley is rotatably connected to the top of the outer connecting frame, and the pulley is in rolling contact with the wire rope.

[0009] Furthermore, a transmission pulley is provided at the end of the rope winding wheel, and the transmission pulley is connected to another transmission pulley through a synchronous belt.

[0010] Furthermore, the apron support plate is slidably connected to the apron body, and the apron support plate is in sliding contact with the inner sides of the two protective cover plates.

[0011] Furthermore, four inner connecting frames are arranged inside the main body of the apron, the main body of the multi-section push rod is fixedly connected to the inner connecting frames, and the top end of the multi-section push rod is connected to the bottom of the apron support plate.

[0012] The utility model provides a double sloped roof structure for a drone landing pad, which has the following beneficial effects:

[0013] When the utility model is in use, when the drone needs to be launched, the driving motor drives the rope winding wheel to rotate forwardly, and the rope winding wheel drives another rope winding wheel to rotate synchronously through the synchronous belt, so that the wire rope is evenly wound on the rope winding wheel, and the left and right protective covers are rotated and opened under the pulling of the wire rope, so that the protective covers are in a vertical state, and the multi-section push rod drives the apron support plate to be lifted upward, and the apron support plate contacts the inner sides of the two protective cover plates. After the apron support plate drives the drone to rise to a predetermined position, the drone can wait for take-off, and the operation is simple and convenient.

[0014] In addition, when the UAV lands on the top of the apron pallet, the multi-section push rod drives the apron pallet to fall back and reset, and the apron pallet separates from the inner side of the two protective covers. The drive motor drives the rope winding wheel to rotate in the opposite direction, and the protective covers gradually rotate and reset under the influence of gravity, so that the two protective covers are in a closed state. The protective covers have a sealing and waterproof effect on the top of the UAV, effectively preventing the UAV from being eroded by the sun and rain, and extending the service life of the UAV.

[0015] Other advantages, objectives and features of the present invention will be reflected in part through the following description, and in part will be understood by those skilled in the art through research and practice of the present invention. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] In order to more clearly illustrate the technical solution of the embodiment of the utility model, the drawings of the embodiment will be briefly introduced below.

[0017] The drawings described below only relate to some embodiments of the present invention, but are not intended to limit the present invention.

[0018] In the attached picture:

[0019] Figure 1A schematic diagram of the shaft side structure of the protective cover plate of the present application in a closed state is shown;

[0020] Figure 2 It shows a schematic diagram of the shaft side structure when the protective cover plate of the present application is in the open and closed state;

[0021] Figure 3 It shows a schematic diagram of the axle side structure of the apron support plate of the present application when it is lifted upward;

[0022] Figure 4 The overall bottom shaft side structure schematic diagram of the present application is shown;

[0023] Figure 5 A schematic diagram of the connection structure between the apron body and the rope winding wheel of the present application is shown.

[0024] Reference numerals list

[0025] 1. Apron body; 101. Inner connecting frame; 102. Outer connecting frame; 2. Apron pallet; 3. Multi-section push rod; 4. Protective cover; 401. Pull hole; 5. Pulley; 6. Rope reel; 601. Drive pulley; 7. Wire rope; 8. Synchronous belt; 9. Drive motor. DETAILED DESCRIPTION

[0026] In order to make the purpose, technical solution and advantages of the embodiment of the utility model clearer, the technical solution of the embodiment of the utility model will be clearly and completely described below in conjunction with the drawings of the embodiment of the utility model. Obviously, the described embodiment is a part of the embodiment of the utility model, not all of the embodiments. Based on the described embodiment of the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0027] Example 1: Please refer to Figures 1 to 5 :

[0028] The utility model proposes a double-slope roof structure for a drone apron, comprising: a helipad body 1; a helipad support plate 2 is installed inside the helipad body 1, the drone is located on the top of the helipad support plate 2, a multi-section push rod 3 is installed inside the helipad body 1, and the multi-section push rod 3 is connected to the helipad support plate 2; two protective cover plates 4 are symmetrically connected to the top of the helipad body 1, the protective cover plates 4 are located on the top of the drone, and pulleys 5 are installed on the top of both ends of the helipad body 1; rope reels 6 are installed on both outer sides of the helipad body 1, and a steel wire rope 7 is wound around the outside of the rope reel 6, and the steel wire rope 7 is connected to the protective cover plate 4; one end of the rope reel 6 is connected to a synchronous belt 8, and the synchronous belt 8 is connected to the two rope reels 6 is connected; a driving motor 9 is fixedly installed on the outside of the apron main body 1 by bolts, and the driving shaft of the driving motor 9 is connected to the rope winding wheel 6; the protective cover plate 4 is rotatably connected to the apron main body 1, and the rotation angle of the protective cover plate 4 is 0-55 degrees. The two protective cover plates 4 are in contact with each other in the combined state, and the protective cover plates 4 are buckled on the top of the apron main body 1; external connecting frames 102 are provided on both outer sides of the apron main body 1, and the rope winding wheel 6 is rotatably connected in the external connecting frames 102, and a pulling hole 401 is provided on the top side of the protective cover plate 4, one end of the wire rope 7 is connected in the pulling hole 401, and the other end of the wire rope 7 is connected to the rope winding wheel 6; the pulley 5 is rotatably connected in the top of the external connecting frame 102, and the pulley 5 is in rolling contact with the wire rope 7.

[0029] In the disclosed embodiment, a transmission pulley 601 is provided at the end of the rope winding wheel 6, and the transmission pulley 601 is connected to another transmission pulley 601 through a synchronous belt 8. The apron pallet 2 is slidably connected to the apron body 1, and the apron pallet 2 is in sliding contact with the inner sides of the two protective cover plates 4. Four inner connecting frames 101 are provided inside the apron body 1, and the main body of the multi-section push rod 3 is fixedly connected to the inner connecting frame 101, and the top of the multi-section push rod 3 is connected to the bottom of the apron pallet 2; using the above technical solution, when it is necessary to launch the drone, the driving motor 9 drives the rope winding wheel 6 to rotate forward, and the rope winding wheel 6 drives another rope winding wheel 6 to rotate synchronously through the synchronous belt 8, and the wire rope 7 is evenly wound on the rope winding wheel 6, and the left and right protective covers are pulled by the wire rope 7. The protective cover plate 4 rotates and opens, so that the protective cover plate 4 is in a vertical state, and the multi-section push rod 3 drives the apron pallet 2 to lift upward, and the apron pallet 2 contacts the inner sides of the two protective cover plates 4. The apron pallet 2 drives the UAV to rise to the predetermined position and then waits for take-off. The operation is simple and easy. When the UAV lands on the top of the apron pallet 2, the multi-section push rod 3 drives the apron pallet 2 to fall back and reset, and the apron pallet 2 is separated from the inner sides of the two protective cover plates 4. The driving motor 9 drives the rope wheel 6 to rotate in the opposite direction. The protective cover plate 4 is gradually rotated and reset under the influence of gravity, so that the two protective cover plates 4 are in a closed state. Relying on the protective cover plate 4, the top of the UAV is sealed and waterproofed, which effectively prevents the UAV from being eroded by the sun and rain, and prolongs the service life of the UAV.

[0030] The working principle of this embodiment is as follows: when the UAV lands on the top of the apron pallet 2, the multi-section push rod 3 drives the apron pallet 2 to fall back and reset, the apron pallet 2 is separated from the inner sides of the two protective covers 4, and the driving motor 9 drives the rope reel 6 to rotate in the opposite direction. The protective covers 4 are gradually rotated and reset under the influence of gravity, so that the two protective covers 4 are in a closed state, and the protective covers 4 are relied on to achieve a sealing and waterproof effect on the top of the UAV; when the UAV needs to be released, the driving motor 9 drives the rope reel 6 to rotate forward, and the rope reel 6 drives another rope reel 6 to rotate synchronously through the synchronous belt 8, and the wire rope 7 is evenly wound on the rope reel 6. Under the pull of the wire rope 7, the left and right protective covers 4 are rotated and opened, so that the protective covers 4 are in a vertical state, and the multi-section push rod 3 drives the apron pallet 2 to lift upward, and the apron pallet 2 contacts the inner sides of the two protective covers 4. After the apron pallet 2 drives the UAV to rise to a predetermined position, it can wait for take-off.

[0031] In this article, there are a few points to note:

[0032] 1. The drawings of the embodiments of the present disclosure only involve structures related to the embodiments of the present disclosure, and other structures may refer to general designs.

[0033] 2. In the absence of conflict, the embodiments of the present disclosure and the features therein may be combined with each other to obtain new embodiments.

[0034] The above are only specific embodiments of the present disclosure, but the protection scope of the present disclosure is not limited thereto. Any technician familiar with the technical field can easily think of changes or substitutions within the technical scope disclosed in the present disclosure, which should be included in the protection scope of the present disclosure. Therefore, the protection scope of the present disclosure should be based on the protection scope of the claims.

Claims

1. A double sloped roof structure for a drone landing pad, comprising: A helipad body (1); characterized in that a helipad support plate (2) is installed inside the helipad body (1), a drone is located on the top of the helipad support plate (2), a multi-section push rod (3) is installed inside the helipad body (1), and the multi-section push rod (3) is connected to the helipad support plate (2); two protective cover plates (4) are symmetrically connected to the top of the helipad body (1), the protective cover plates (4) are located on the top of the drone, and pulleys (5) are installed on the top of both ends of the helipad body (1); rope reels (6) are installed on both outer sides of the helipad body (1), and a steel wire rope (7) is wound around the rope reel (6), and the steel wire rope (7) is connected to the protective cover plate (4); one end of the rope reel (6) is connected to a synchronous belt (8), and the synchronous belt (8) is connected to the two rope reels (6); a drive motor (9) is fixedly installed on the outside of the helipad body (1) by bolts, and the drive shaft of the drive motor (9) is connected to the rope reel (6).

2. The double-slope roof structure for a drone landing pad according to claim 1, characterized in that: The protective cover plate (4) is rotatably connected to the apron body (1), the rotation angle of the protective cover plate (4) is 0 to 55 degrees, the two protective cover plates (4) are in contact with each other in a combined state, and the protective cover plates (4) are buckled on the top of the apron body (1).

3. The double-slope roof structure for a drone landing pad according to claim 1, characterized in that: The two outer sides of the apron body (1) are provided with external connecting frames (102), the rope winding wheel (6) is rotatably connected to the outer connecting frame (102), the top side of the protective cover plate (4) is provided with a pulling hole (401), one end of the steel wire rope (7) is connected to the pulling hole (401), and the other end of the steel wire rope (7) is connected to the rope winding wheel (6).

4. The double-slope roof structure for a drone landing pad according to claim 3, characterized in that: The pulley (5) is rotatably connected to the top of the outer connecting frame (102), and the pulley (5) is in rolling contact with the steel wire rope (7).

5. The double sloped roof structure for a drone landing pad according to claim 1, characterized in that: A transmission pulley (601) is provided at the end of the rope winding wheel (6), and the transmission pulley (601) is connected to another transmission pulley (601) through a synchronous belt (8).

6. The double slope roof structure for a drone landing pad according to claim 1, characterized in that: The apron support plate (2) is slidably connected inside the apron body (1), and the apron support plate (2) is in slidable contact with the inner sides of the two protective cover plates (4).

7. The double slope roof structure for a drone landing pad according to claim 1, characterized in that: Four inner connecting frames (101) are arranged inside the apron body (1), the body of the multi-section push rod (3) is fixedly connected to the inner connecting frame (101), and the top of the multi-section push rod (3) is connected to the bottom of the apron support plate (2).

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