Intelligent unmanned aerial vehicle hangar with 90-degree unfolding and moving-out platform

Abstract

The invention discloses an intelligent unmanned aerial vehicle hangar with a 90-degree unfolding and moving-out platform, and belongs to the technical field of unmanned aerial vehicle hangars.The intelligent unmanned aerial vehicle hangar comprises a first mechanism integration shell, the inner side of the first mechanism integration shell is connected with a double-shaft motor, the output end of the double-shaft motor is connected with a rotating rod, one end of the rotating rod is connected with a first bevel gear, and the other end of the rotating rod is connected with a second bevel gear; an electric push rod is connected to the inner side of the second mechanism integration shell, a connecting block is connected to one end of the electric push rod, an unmanned aerial vehicle platform is connected to the connecting block, first sliding rails are connected to the two sides of the unmanned aerial vehicle platform, and second sliding rails are arranged on the two sides of the second mechanism integration shell. The rapid unfolding platform provides a stable take-off and landing foundation for the unmanned aerial vehicle; and after the task is completed, the platform and the unmanned aerial vehicle can be quickly recovered into the hangar, so that the space is saved, the operation efficiency is improved, and the system is particularly suitable for emergency rescue, quick monitoring and other scenes with high time requirements.

Description

Technical Field

[0001] The present invention relates to the field of drone hangars, and in particular to an intelligent drone hangar with a 90-degree unfolding and removable platform. Background Art

[0002] With the widespread application of drone technology, the parking and protection of drones has become an important issue. The traditional drone hangar structure is relatively simple, lacking an efficient platform deployment and storage mechanism, and cannot meet the needs of convenient take-off and landing and all-round protection of drones. In some complex environments, the docking operation of drones is not flexible enough, and the hangar is difficult to provide stable support and timely protection for drones, and is easily interfered with by external factors. In response to these problems, the present invention aims to provide an electric drone hangar with a 90-degree deployment and removable platform through an innovative mechanical structure design, so as to optimize the parking and use experience of drones. Summary of the Invention

[0003] The object of the present invention is to provide an intelligent drone hangar with a 90-degree unfolding and moving-out platform. To achieve the above-mentioned object, the present invention provides the following technical solutions: comprising a mechanism integrated housing 1, a dual-axis motor connected to the inner side of the mechanism integrated housing 1, an output end of the dual-axis motor connected to a rotating rod, one end of the rotating rod connected to a first bevel gear, a second bevel gear provided on one side of the first bevel gear, a threaded slide connected to the middle position of the second bevel gear, a connecting rod connected to the outer side of the threaded slide, one side of the connecting rod connected to a mechanism integrated housing 2, an electric push rod connected to the inner side of the mechanism integrated housing 2, one end of the electric push rod connected to a connecting block, a drone platform connected to the connecting block, first slide rails connected to both sides of the drone platform, and second slide rails provided on both sides of the mechanism integrated housing 2;

[0004] As a further preferred embodiment of the present technical solution: a first hydraulic pipe is connected to the middle position of the upper side of the UAV platform, one end of the first hydraulic pipe is connected to a first piston rod, one end of the first piston rod is connected to a bracket, a second hydraulic pipe is passed through the lower end of the first hydraulic pipe, one end of the second hydraulic pipe is connected to a second piston rod, and one end of the second piston rod is connected to a protective plate;

[0005] As a further preferred embodiment of the present technical solution: the dual-axis motor is fixedly arranged on the inner side of the first integrated housing of the mechanism, the end of the rotating rod away from the dual-axis motor is fixedly connected to the middle position of the first bevel gear, and the first bevel gear and the second bevel gear are meshed;

[0006] As a further preference of this technical solution: One end of the rotating rod away from the dual-axis motor is rotatably connected to a connection shell provided inside the first integrated mechanism housing, the upper end of the threaded slide is rotatably connected to a connection shell provided inside the first integrated mechanism housing, and the lower end of the threaded slide is rotatably connected to an extension plate provided inside the first integrated mechanism housing;

[0007] As a further preference of this technical solution: One end of the connecting rod is rotatably connected to one side of the threaded slide, and the other end of the connecting rod is rotatably connected to one side of the second integrated mechanism housing. There are two groups of connecting rods and they are symmetrically arranged;

[0008] As a further preference of this technical solution: There are two groups of the second slide rails and they are symmetrically arranged on both sides of the second integrated mechanism housing. The first slide rail is slidably connected to the second slide rail. There are two groups of the second slide rails and they are symmetrically arranged on both sides of the drone platform;

[0009] As a further preference of this technical solution: The first hydraulic pipe is fixedly arranged at the middle position on the upper side of the drone platform. The first piston rod fits and slides inside the first hydraulic pipe. The upper end of the first piston rod is fixedly connected to the middle position on the lower side of the bracket;

[0010] As a further preference of this technical solution: The shape of the second hydraulic pipe is L-shaped. The second piston rod fits and slides inside the second hydraulic pipe. There are four groups of protective plates and they are evenly distributed on the outside of the bracket;

[0011] As a further preference of this technical solution: The electric push rod is fixedly arranged inside the second integrated mechanism housing, and the connection block is fixedly arranged on the lower side of the drone platform;

[0012] As a further preference of this technical solution: One end of the second integrated mechanism housing is rotatably connected to the inside of the first integrated mechanism housing, and the drone platform is slidably arranged inside the first integrated mechanism housing.

[0013] Compared with the prior art, the beneficial effects of the present invention are:

[0014] 1. In the present invention, by driving the rotating rod with a dual-axis motor, the meshing transmission between the first bevel gear and the second bevel gear is realized, and then the threaded slide is driven to rotate, so that the connecting rod drives the second integrated mechanism housing to deflect. The forward and reverse rotation control of the dual-axis motor can easily realize the 90-degree deployment and storage of the drone platform. The whole process has a high degree of automation and is simple and fast to operate. When the drone needs to be used, the platform can be quickly deployed to provide a stable takeoff and landing foundation for the drone; after the task is completed, the platform and the drone can be quickly recovered into the hangar, saving space and improving the operation efficiency, especially suitable for scenarios with high time requirements such as emergency rescue and rapid monitoring;

[0015] 2. In this invention, when the drone is parked on the bracket, its own gravity triggers the hydraulic system to operate. The first piston rod slides down the first hydraulic pipe, squeezing hydraulic oil into the second hydraulic pipe, pushing the second piston rod upward, causing the four sets of protective plates to rise evenly, forming a tight protection around the drone. This protective mechanism effectively prevents the drone from accidental damage such as collisions and scratches during parking. The combination of the bracket and the hydraulic system also provides stable support for the drone. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 This is a schematic diagram of the structure of an intelligent drone hangar with a 90-degree deployment and removal platform of the present invention. Figure 1 ;

[0017] Figure 2 This is a schematic diagram of the structure of an intelligent drone hangar with a 90-degree deployment and removal platform of the present invention. Figure 2 ;

[0018] Figure 3 This is a schematic diagram of the structure of an intelligent drone hangar with a 90-degree deployment and removal platform of the present invention. Figure 3 ;

[0019] Figure 4 for Figure 3 A is an enlarged view.

[0020] In the figure: 1. Mechanism integrated housing 1; 2. Dual-axis motor; 3. Rotating rod; 4. First bevel gear; 5. Second bevel gear; 6. Threaded slide; 7. Threaded rod; 8. Mechanism integrated housing 2; 9. Electric push rod; 10. Connecting block; 11. UAV platform; 12. First slide rail; 13. Second slide rail; 14. First hydraulic pipe; 15. First piston rod; 16. Bracket; 17. Second hydraulic pipe; 18. Second piston rod; 19. Protective plate; 20. Connecting rod. DETAILED DESCRIPTION

[0021] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0022] Example

[0023] See also Figures 1-4As shown in the figure, the present invention provides a technical solution for an intelligent UAV hangar with a 90-degree unfolding and a moving-out platform: It includes an integrated mechanism housing one 1. A double-shaft motor 2 is connected to the inner side of the integrated mechanism housing one 1. The output end of the double-shaft motor 2 is connected to a rotating rod 3. One end of the rotating rod 3 is connected to a first bevel gear 4. A second bevel gear 5 is provided on one side of the first bevel gear 4. A threaded slide 6 is connected to the middle position of the second bevel gear 5. A connecting rod 20 is connected to the outer side of the threaded slide 6. One side of the connecting rod 20 is connected to an integrated mechanism housing two 8. An electric push rod 9 is connected to the inner side of the integrated mechanism housing two 8. One end of the electric push rod 9 is connected to a connecting block 10. A UAV platform 11 is connected to the connecting block 10. First slide rails 12 are connected to both sides of the UAV platform 11. Second slide rails 13 are provided on both sides of the integrated mechanism housing two 8.

[0024] In this embodiment, specifically: A first hydraulic pipe 14 is connected to the middle position on the upper side of the UAV platform 11. One end of the first hydraulic pipe 14 is connected to a first piston rod 15. One end of the first piston rod 15 is connected to a bracket 16. The lower end of the first hydraulic pipe 14 is connected through a second hydraulic pipe 17. One end of the second hydraulic pipe 17 is connected to a second piston rod 18. One end of the second piston rod 18 is connected to a protection plate 19.

[0025] In this embodiment, specifically: The double-shaft motor 2 is fixedly arranged on the inner side of the integrated mechanism housing one 1. The end of the rotating rod 3 away from the double-shaft motor 2 is fixedly connected to the middle position of the first bevel gear 4. The first bevel gear 4 and the second bevel gear 5 are meshed.

[0026] In this embodiment, specifically: The end of the rotating rod 3 away from the double-shaft motor 2 is rotatably connected to a connection shell provided on the inner side of the integrated mechanism housing one 1. The upper end of the threaded slide 6 is rotatably connected to a connection shell provided on the inner side of the integrated mechanism housing one 1. The lower end of the threaded slide 6 is rotatably connected to an extension plate provided on the inner side of the integrated mechanism housing one 1.

[0027] In this embodiment, specifically: One end of the connecting rod 20 is rotatably connected to one side of the threaded slide 6. The other end of the connecting rod 20 is rotatably connected to one side of the integrated mechanism housing two 8. There are two groups of connecting rods 20 and they are symmetrically arranged.

[0028] In this embodiment, specifically: There are two groups of second slide rails 13 and they are symmetrically arranged on both sides of the integrated mechanism housing two 8. The first slide rails 12 are slidably connected to the second slide rails 13. There are two groups of second slide rails 13 and they are symmetrically arranged on both sides of the UAV platform 11.

[0029] In this embodiment, specifically: The first hydraulic pipe 14 is fixedly arranged on the middle position on the upper side of the UAV platform 11. The first piston rod 15 fits and slides inside the first hydraulic pipe 14. The upper end of the first piston rod 15 is fixedly connected to the middle position on the lower side of the bracket 16.

[0030] In this embodiment, specifically: the shape of the second hydraulic pipe 17 is L-shaped, the second piston rod 18 fits and slides inside the second hydraulic pipe 17, and there are four groups of protective plates 19 evenly distributed on the outside of the bracket 16.

[0031] In this embodiment, specifically: the electric push rod 9 is fixedly arranged inside the second mechanism integration housing 8, and the connecting block 10 is fixedly arranged on the lower side of the drone platform 11.

[0032] In this embodiment, specifically: one end of the second mechanism integration housing 8 is rotatably connected inside the first mechanism integration housing 1, and the drone platform 11 is slidably arranged inside the first mechanism integration housing 1.

[0033] Working principle or structural principle: First, by starting the double-shaft motor 2, the rotating rod 3 is driven to rotate, and at the same time, the first bevel gear 4 is driven to rotate, and at the same time, the second bevel gear 5 is driven to rotate, and at the same time, the threaded slide 6 is driven to rotate, so that the threaded rod 7 can be driven to rotate, and at the same time, the connecting rod 20 is driven to move downward, and at the same time, the second mechanism integration housing 8 is pushed to deflect downward. When the second mechanism integration housing 8 deflects to the horizontal position, stop the double-shaft motor 2. By starting the electric push rod 9, the connecting block 10 is pushed to move, and the drone platform 11 is pushed through the connecting block 10, driving the first slide rail 12 to slide on the second slide rail 13, so that the drone platform 11 can be opened. When the drone is parked on the bracket 16, due to the self-gravity of the drone, the bracket 16 is pressed downward, driving the first piston rod 15 to slide downward inside the first hydraulic pipe 14, squeezing the hydraulic oil inside the first hydraulic pipe 14, so that the hydraulic oil is squeezed into the second hydraulic pipe 17, and squeezing the second piston rod 18 to move upward, and at the same time driving the protective plate 19 to move upward to protect the surroundings of the drone. When the drone flies away from the bracket 16, the protective plate 19 and the bracket 16 return to their original positions, start the electric push rod 9, pull the connecting block 10 and the drone platform 11 to contract back to their original positions. At this time, by starting the double-shaft motor 2 to drive the rotating rod 3 to rotate in the reverse direction, and at the same time driving the threaded rod 7 to move upward, pulling the connecting rod 20 to deflect upward, and at the same time pulling the second mechanism integration housing 8 to deflect upward, driving the second mechanism integration housing 8, the drone platform 11 and the first piston rod 15 to be received inside the first mechanism integration housing 1.

[0034] Although the embodiments of the present invention have been shown and described, for those of ordinary skill in the art, it can be understood that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principle and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An intelligent drone hangar with a 90-degree deployment and retraction platform, characterized by: It includes an integrated mechanism housing one (1). A dual-axis motor (2) is connected to the inner side of the integrated mechanism housing one (1). The output end of the dual-axis motor (2) is connected to a rotating rod (3). One end of the rotating rod (3) is connected to a first bevel gear (4). A second bevel gear (5) is provided on one side of the first bevel gear (4). A threaded slide (6) is connected to the middle position of the second bevel gear (5). A connecting rod (20) is connected to the outer side of the threaded slide (6). One side of the connecting rod (20) is connected to an integrated mechanism housing two (8). An electric push rod (9) is connected to the inner side of the integrated mechanism housing two (8). One end of the electric push rod (9) is connected to a connecting block (10). A drone platform (11) is connected to the connecting block (10). First slide rails (12) are connected to both sides of the drone platform (11). Second slide rails (13) are provided on both sides of the integrated mechanism housing two (8).

2. The intelligent UAV hangar with a 90-degree unfolding and moving-out platform according to claim 1, wherein: A first hydraulic pipe (14) is connected to the middle position on the upper side of the drone platform (11). One end of the first hydraulic pipe (14) is connected to a first piston rod (15). One end of the first piston rod (15) is connected to a bracket (16). The lower end of the first hydraulic pipe (14) is connected through and to a second hydraulic pipe (17). One end of the second hydraulic pipe (17) is connected to a second piston rod (18). One end of the second piston rod (18) is connected to a protective plate (19).

3. The intelligent drone hangar with a 90-degree deployment and removable platform according to claim 2, characterized in that: The dual-axis motor (2) is fixedly arranged on the inner side of the integrated mechanism housing one (1). The end of the rotating rod (3) away from the dual-axis motor (2) is fixedly connected to the middle position of the first bevel gear (4). The first bevel gear (4) and the second bevel gear (5) are meshed.

4. The intelligent drone hangar with a 90-degree unfolding and moving-out platform according to claim 3, wherein: The end of the rotating rod (3) away from the dual-axis motor (2) is rotatably connected to a connection shell provided on the inner side of the integrated mechanism housing one (1). The upper end of the threaded slide (6) is rotatably connected to the connection shell provided on the inner side of the integrated mechanism housing one (1). The lower end of the threaded slide (6) is rotatably connected to an extension plate provided on the inner side of the integrated mechanism housing one (1).

5. The intelligent drone hangar with a 90-degree deployment and removal platform according to claim 4, characterized in that: One end of the connecting rod (20) is rotatably connected to one side of the threaded slide (6). The other end of the connecting rod (20) is rotatably connected to one side of the integrated mechanism housing two (8). There are two groups of the connecting rods (20) and they are symmetrically arranged.

6. The intelligent drone hangar with a 90-degree deployment and removable platform according to claim 5, characterized in that: There are two groups of the second slide rails (13) and they are symmetrically arranged on both sides of the integrated mechanism housing two (8). The first slide rails (12) are slidably connected to the second slide rails (13). There are two groups of the second slide rails (13) and they are symmetrically arranged on both sides of the drone platform (11).

7. The intelligent drone hangar with a 90-degree deployment and removable platform according to claim 6, characterized in that: The first hydraulic pipe (14) is fixedly arranged on the middle position on the upper side of the drone platform (11). The first piston rod (15) fits and slides inside the first hydraulic pipe (14). The upper end of the first piston rod (15) is fixedly connected to the middle position on the lower side of the bracket (16).

8. The intelligent drone hangar with a 90-degree deployment and removal platform according to claim 7, characterized in that: The shape of the second hydraulic pipe (17) is L-shaped, the second piston rod (18) fits and slides inside the second hydraulic pipe (17), and there are four groups of protective plates (19) evenly distributed on the outer side of the bracket (16).

9. The intelligent drone hangar with a 90-degree deployment and removable platform according to claim 8, characterized in that: The electric push rod (9) is fixedly arranged inside the second mechanism integration housing (8), and the connecting block (10) is fixedly arranged on the lower side of the drone platform (11).

10. The intelligent drone hangar with a 90-degree deployment and removal platform according to claim 9, characterized in that: One end of the second mechanism integration housing (8) is rotatably connected inside the first mechanism integration housing (1), and the drone platform (11) slides inside the first mechanism integration housing (1).

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