Double-layer unmanned aerial vehicle hangar

Abstract

The utility model discloses a double-layer unmanned aerial vehicle hangar, and belongs to the technical field of unmanned aerial vehicle hangars, the double-layer unmanned aerial vehicle hangar comprises a hangar body, the inner wall of the hangar body is fixedly connected with a supporting table, the top of the supporting table is slidably connected with a placing platform, and the bottom of the placing platform is fixedly connected with a connecting plate; the inner wall of the hangar body is fixedly connected with a motor, a rotating shaft of the motor is fixedly connected with a threaded rod, the outer wall of the threaded rod is in threaded connection with a threaded pipe, the threaded pipe is rotationally connected with the connecting plate, and the face, away from the motor, of the hangar body is hinged to a sealing door through a hinge. The double-layer unmanned aerial vehicle hangar is arranged, the vertical space is utilized, and the unmanned aerial vehicles are stacked to save the ground space, so that the number of the placed unmanned aerial vehicles is increased, meanwhile, the two obliquely-symmetrical sealing doors are installed on the double-layer unmanned aerial vehicle hangar, the unmanned aerial vehicles on different layers do not interfere with each other, and therefore the situation that under the emergency situation, the unmanned aerial vehicles cannot be damaged is avoided. The take-off efficiency of the unmanned aerial vehicle is influenced.

Description

Technical Field

[0001] The utility model belongs to the technical field of unmanned aerial vehicle hangars, and specifically relates to a double-layer unmanned aerial vehicle hangar. Background Art

[0002] A drone hangar is a facility or area used to store and maintain drones. A drone hangar is usually equipped with the necessary equipment and infrastructure to support the operation and maintenance of drones.

[0003] However, most of the existing drone hangars on the market have one hangar for each drone, which may face the problem of insufficient space during use, so the utilization efficiency of the hangar is low. Although some hangars can accommodate multiple drones during use, the corresponding hangars usually have only one entrance and exit. During use, if an emergency occurs, the single entrance and exit will affect the efficiency of drone entry and exit, which may cause damage to the drone.

[0004] In order to solve the above problems, a double-layer UAV hangar is proposed in this application. Utility Model Content

[0005] In view of the problems in the related technology, the utility model proposes a double-layer UAV hangar to overcome the above-mentioned technical problems existing in the existing related technology.

[0006] In order to achieve the above purpose, the utility model adopts the following technical solutions:

[0007] A double-layer drone hangar comprises a hangar body, wherein the inner wall of the hangar body is fixedly connected to a support platform, the top of the support platform is slidably connected to a placement platform, the bottom of the placement platform is fixedly connected to a connecting plate, the inner wall of the hangar body is fixedly connected to a motor, a threaded rod is fixedly connected to the rotating shaft of the motor, the outer wall of the threaded rod is threadedly connected to a threaded tube, the threaded tube is rotatably connected to the connecting plate, a closed door is hingedly connected to a side of the hangar body away from the motor through a hinge, both ends of the closed door are rotatably connected to a first rotating block, the outer wall of the hangar body is rotatably connected to a second rotating block, the second rotating block is fixedly connected to a connecting block, a telescopic rod is fixedly connected to one side of the connecting block, the telescopic end of the telescopic rod is fixedly connected to the first rotating block, and a notch is provided on the hangar body.

[0008] Preferably, the second rotating block passes through the side wall of the hangar body, a limiting groove is provided on a side of the second rotating block away from the connecting block, a connecting groove is provided on the side wall of the support platform, the side wall of the placement platform is fixedly connected to the limiting block, the limiting block passes through the connecting groove provided on the support platform, and the outer wall of the limiting block is fitted with the limiting groove provided on the second rotating block.

[0009] By providing the limit groove, the connection groove and the limit block, the closed door can be fixed, thereby preventing the closed door from opening and closing when not in use, thereby preventing the opening and closing of the closed door from affecting the drone inside the device.

[0010] Preferably, a fixing plate is fixedly connected to the bottom of the placing platform, a side of the fixing plate away from the closed door is fixedly connected to a limiting rod, and the limiting rod is slidably connected to the supporting platform.

[0011] By providing a fixing plate and a limiting rod, the placement platform is stabilized, thereby preventing the shaking of the placement platform from affecting the release of the storage box of the drone, thereby avoiding affecting the use of the device.

[0012] Preferably, a through opening is provided at the bottom of the hangar body, and a protective plate is fixedly connected to the top of the hangar body.

[0013] Through-holes and protective plates are provided to achieve ventilation and protection inside the connection block, thereby preventing the hangar body from being overheated or overly humid. At the same time, the protective plates are used to protect the through-holes to prevent rainwater from entering through the through-holes, thereby avoiding damage to the drone.

[0014] Preferably, an outer wall of the hangar body is slidably connected with a sliding plate, and a handle is provided on the sliding plate.

[0015] By setting up a sliding plate, the windows set on the hangar body can be protected, thereby avoiding affecting the use of the hangar body and further avoiding damage to the drone inside the hangar body.

[0016] Preferably, a support column is fixedly connected to the bottom of the hangar body.

[0017] By setting up support columns, the hangar body can be supported, thereby avoiding damage caused by overheating inside the hangar body and further avoiding damage to the drone.

[0018] Preferably, a sealing gasket is fixedly connected to the closed door, and one side of the sealing gasket is in contact with one side of the hangar body.

[0019] By providing a sealing gasket, the closed door can be sealed, thereby preventing damage to the components inside the hangar body.

[0020] In summary, the technical effects and advantages of the utility model are as follows:

[0021] By setting up a double-decker drone hangar and utilizing vertical space, drones can be stacked to save ground space, thereby increasing the number of drones that can be placed. At the same time, two obliquely symmetrical closed doors are installed on the double-decker drone hangar so that drones on different floors do not interfere with each other, thereby avoiding affecting the take-off efficiency of drones in emergency situations.

[0022] The closed door is fixed by the cooperation of the limit groove, the connecting groove and the limit block, and the second rotating block is fixed by the limit block being clamped into the inside of the limit groove. When the second rotating block is in the fixing device, the telescopic rod will not be able to be stretched, thereby preventing the closed door from opening and closing when not in use, thereby preventing the opening and closing of the closed door from affecting the drone inside the device. BRIEF DESCRIPTION OF THE DRAWINGS

[0023] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0024] Figure 2 This is a schematic diagram of the structure of the support platform and its related parts of the utility model;

[0025] Figure 3 This is a schematic diagram of the structure of the placement platform and its related parts of the utility model;

[0026] Figure 4 This is a schematic diagram of the structure of the limit block and related parts of the utility model.

[0027] In the figure:

[0028] 1. Hangar body; 2. Connection block; 3. Support platform; 4. Telescopic rod; 5. Closed door; 6. First rotating block; 7. Notch; 8. Motor; 9. Second rotating block; 10. Placement platform; 11. Threaded pipe; 12. Threaded rod; 13. Connection plate; 14. Connection groove; 15. Sealing pad; 16. Support column; 17. Limit groove; 18. Limit block; 19. Limit rod; 20. Fixed plate; 21. Through port; 22. Protective plate; 23. Sliding plate. DETAILED DESCRIPTION

[0029] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all of the embodiments.

[0030] Reference Figure 1-3A double-layer UAV hangar comprises a hangar body 1, the inner wall of the hangar body 1 is fixedly connected with a support platform 3, the top of the support platform 3 is slidably connected with a placement platform 10, the support platform 3 is used to support the placement platform 10, the placement platform 10 is composed of a support component and a fixing component, the support component can realize the landing of the UAV, the fixing component is used to stabilize the UAV, the bottom of the placement platform 10 is fixedly connected with a connecting plate 13, the inner wall of the hangar body 1 is fixedly connected with a motor 8, a threaded rod 12 is fixedly connected to the rotating shaft of the motor 8, the motor 8 is used to realize the rotation of the threaded rod 12, the outer wall of the threaded rod 12 is threadedly connected with a threaded tube 11, the rotation of the threaded rod 12 makes the threaded tube 11 rotate and move, the threaded tube 11 is rotatably connected to the connection plate 13, the movement of the threaded tube 11 makes the connection plate 13 move, through the cooperation of the motor 8, the threaded rod 12, the threaded tube 11, and the connection plate 13, the placement platform 1 0 can be moved, so that the drone can be moved. A closed door 5 is hinged on one side of the hangar body 1 away from the motor 8 through a hinge. The closed door 5 is used to close the entrance and exit opened on the hangar body 1. Two closed doors 5 are arranged on the hangar body 1. The two closed doors 5 are distributed obliquely symmetrically on the hangar body 1. The two ends of the closed door 5 are rotatably connected with a first rotating block 6. The outer wall of the hangar body 1 is rotatably connected with a second rotating block 9. A connecting block 2 is fixedly connected to the second rotating block 9. A telescopic rod 4 is fixedly connected to one side of the connecting block 2. The telescopic end of the telescopic rod 4 is fixedly connected to the first rotating block 6. The closed door 5 can be flipped through the cooperation of the second rotating block 9, the connecting block 2, the telescopic rod 4 and the first rotating block 6. After flipping, the closed door 5 will return to its original position under the pull of the telescopic rod 4, so as to ensure the closure of the interior of the hangar body 1. A notch 7 is provided on the hangar body 1, and the notch 7 can facilitate the flipping of the closed door 5.

[0031] Reference Figure 2 and Figure 4 The second rotating block 9 passes through the side wall of the hangar body 1, and a limiting groove 17 is provided on the side of the second rotating block 9 away from the connecting block 2. A connecting groove 14 is provided on the side wall of the support platform 3, and the side wall of the placement platform 10 is fixedly connected to the limiting block 18. The limiting block 18 passes through the connecting groove 14 provided on the support platform 3, and the outer wall of the limiting block 18 is fitted with the limiting groove 17 provided on the second rotating block 9. The limiting groove 17, the connecting groove 14 and the limiting block 18 are used in coordination to fix the closed door 5. The limiting block 18 is snapped into the inside of the limiting groove 17, so that the second rotating block 9 is fixed. When the second rotating block 9 is in the fixing device, the telescopic rod 4 will not be able to stretch, thereby preventing the closed door 5 from opening and closing when not in use, thereby preventing the opening and closing of the closed door 5 from affecting the drone inside the device.

[0032] Reference Figure 4A fixing plate 20 is fixedly connected to the bottom of the placement platform 10, and a side of the fixing plate 20 away from the closed door 5 is fixedly connected to a limit rod 19, and the limit rod 19 is slidably connected to the support platform 3. The limit rod 19 is used to stabilize the placement platform 10 to prevent the placement platform 10 from shaking during the movement, thereby preventing the shaking of the placement platform 10 from affecting the release of the storage box of the drone, thereby avoiding affecting the use of the device.

[0033] Reference Figure 1 A through opening 21 is provided at the bottom of the hangar body 1, and a protective plate 22 is fixedly connected to the top of the hangar body 1. The through opening 21 realizes ventilation and protection of the interior of the connecting block 2. The through opening 21 allows the interior of the hangar body 1 to interact with the external air, thereby preventing the interior of the hangar body 1 from being too high or too humid. At the same time, the protective plate 22 is used to protect the through opening 21 to prevent rainwater from entering through the through opening 21, thereby avoiding damage to the drone.

[0034] Reference Figure 1 The outer wall of the hangar body 1 is slidably connected with a sliding plate 23, on which a handle is provided. The sliding plate 23 is used to protect the windows provided on the hangar body 1 to prevent the windows provided on the hangar body 1 from being damaged without protection, thereby avoiding affecting the use of the hangar body 1 and further avoiding damage to the drone inside the hangar body 1.

[0035] Reference Figure 1 The bottom of the hangar body 1 is fixedly connected with a support column 16, which is used to support the hangar body 1. The hangar body 1 is separated from the ground by the support column 16 to avoid affecting the heat dissipation inside the hangar body 1, thereby avoiding damage caused by overheating inside the hangar body 1, and further avoiding damage to the drone.

[0036] Reference Figure 3 A sealing gasket 15 is fixedly connected to the closed door 5, and one side of the sealing gasket 15 is in contact with one side of the hangar body 1. The sealing gasket 15 is used to seal the closed door 5 to prevent rainwater from flowing into the interior of the hangar body 1 through the contact surface between the closed door 5 and the hangar body 1, thereby preventing parts inside the hangar body 1 from being damaged.

[0037] Working principle:

[0038] When the drone needs to land, the motor 8 is started to rotate the threaded rod 12, and the rotation of the threaded rod 12 drives the threaded tube 11 to rotate. The threaded tube 11 moves during the rotation and moves the connecting plate 13. The movement of the connecting plate 13 drives the placement platform 10 to move. After the placement platform 10 moves to a certain distance, it pushes the closed door 5. The closed door 5 begins to flip under the push of the placement platform 10. The flipping of the closed door 5 causes the first rotating block 6 and the connecting block 2 to rotate, and the telescopic rod 4 begins to stretch. When the placement platform 10 moves to a certain position, the drone lands on the placement platform 10. At this time, the motor 8 drives the placement platform 10 back to its original position. The reset of the placement platform 10 causes the closed door 5 to return to its original position. The reset of the closed door 5 causes the first rotating block 6, the telescopic rod 4, the second rotating block 9 and the connecting block 2 to reset. At this time, the limit block 18 is clamped into the limit groove 17 provided in the second rotating block 9, thereby fixing the second rotating block 9. The fixation of the second rotating block 9 prevents the closed door 5 from flipping again, thereby preventing the closed door 5 from being opened when it is not needed, thereby avoiding affecting the use of the device.

[0039] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. A double-layer UAV hangar, comprising a hangar body (1), characterized in that: The inner wall of the hangar body (1) is fixedly connected to a support platform (3), the top of the support platform (3) is slidably connected to a placement platform (10), the bottom of the placement platform (10) is fixedly connected to a connecting plate (13), the inner wall of the hangar body (1) is fixedly connected to a motor (8), a threaded rod (12) is fixedly connected to the rotating shaft of the motor (8), the outer wall of the threaded rod (12) is threadedly connected to a threaded pipe (11), the threaded pipe (11) is rotatably connected to the connecting plate (13), and the hangar body (1) is fixedly connected to a motor (8), the motor (8) is fixedly connected to a threaded rod (12), the outer wall of the threaded rod (12) is threadedly connected to a threaded pipe (11), and the threaded pipe (11) is rotatably connected to the connecting plate (13). A closed door (5) is hingedly connected to a side of the hangar body (1) away from the motor (8) via a hinge, and the two ends of the closed door (5) are rotatably connected to a first rotating block (6), and the outer wall of the hangar body (1) is rotatably connected to a second rotating block (9), and a connecting block (2) is fixedly connected to the second rotating block (9), and a telescopic rod (4) is fixedly connected to one side of the connecting block (2), and the telescopic end of the telescopic rod (4) is fixedly connected to the first rotating block (6), and a notch (7) is provided on the hangar body (1).

2. A double-layer UAV hangar according to claim 1, characterized in that: The second rotating block (9) passes through the side wall of the hangar body (1); a limiting groove (17) is provided on a side of the second rotating block (9) away from the connecting block (2); a connecting groove (14) is provided on the side wall of the supporting platform (3); a limiting block (18) is fixedly connected to the side wall of the placement platform (10); the limiting block (18) passes through the connecting groove (14) provided on the supporting platform (3); and an outer wall of the limiting block (18) is fitted with the limiting groove (17) provided on the second rotating block (9).

3. A double-layer UAV hangar according to claim 1, characterized in that: A fixing plate (20) is fixedly connected to the bottom of the placement platform (10), and a side of the fixing plate (20) away from the closed door (5) is fixedly connected to a limiting rod (19), and the limiting rod (19) is slidably connected to the support platform (3).

4. A double-layer UAV hangar according to claim 1, characterized in that: A through opening (21) is provided at the bottom of the hangar body (1), and a protective plate (22) is fixedly connected to the top of the hangar body (1).

5. The double-layer UAV hangar according to claim 1 is characterized in that: The outer wall of the hangar body (1) is slidably connected with a sliding plate (23), and a handle is provided on the sliding plate (23).

6. A double-layer UAV hangar according to claim 1, characterized in that: A support column (16) is fixedly connected to the bottom of the hangar body (1).

7. The double-layer UAV hangar according to claim 1 is characterized in that: A sealing gasket (15) is fixedly connected to the closed door (5), and one side of the sealing gasket (15) is in contact with one side of the hangar body (1).

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