Unmanned aerial vehicle hangar landing platform

Abstract

The utility model discloses an unmanned aerial vehicle hangar landing platform, which belongs to the field of unmanned aerial vehicle landing auxiliary equipment and comprises a base, a main plate is arranged above the base, a lifting mechanism is arranged between the base and the main plate, auxiliary plates are arranged on the periphery of the main plate, and the auxiliary plates are detachably connected with the main plate through mounting mechanisms. The mounting mechanism comprises a rectangular block fixed to one side face of the auxiliary plate, second rectangular grooves are formed in the periphery of the main plate, and the rectangular block is inserted into the second rectangular grooves. According to the unmanned aerial vehicle hangar landing platform, through the arrangement of the mounting mechanism, the effect that the unmanned aerial vehicle hangar landing platform is convenient to assemble and disassemble is achieved, the auxiliary plate is inserted into the second rectangular groove of the main plate through the rectangular block and matched with the limiting rod to be inserted into the limiting hole, and friction force is increased through magnetic attraction of the first magnet and the second magnet and a rubber pad; the auxiliary board and the main board are stably connected, and meanwhile, the auxiliary board can be conveniently detached from the main board when needed through the detachable connection mode.

Description

Technical Field

[0001] This utility model relates to the field of drone landing assistance equipment technology, and in particular to a drone hangar landing platform. Background Technology

[0002] With the rapid development of drone technology and its widespread application in many fields, drone hangar landing platforms, as key facilities to ensure the safe and efficient landing of drones, are receiving increasing attention for their performance and characteristics.

[0003] Traditional drone hangars and landing platforms are mostly one-piece fixed structures with fixed size and shape. Such structures bring great inconvenience to practical applications. For example, in some projects that require frequent changes of work sites, such as film and television shooting teams using drones for aerial photography, the shooting location may be moved from urban high-rise buildings to remote mountainous areas. Traditional large fixed landing platforms are difficult to move and reinstall due to their large size and weight. This limits the flexible deployment of drones in different sites and reduces work efficiency. Utility Model Content

[0004] The purpose of this invention is to solve the problem that most existing technologies are one-piece fixed structures with fixed size and shape, which brings great inconvenience to practical application scenarios. Therefore, this invention proposes a drone hangar landing platform.

[0005] To achieve the above objectives, the present invention adopts the following technical solution:

[0006] A drone hangar landing platform includes a base, a main board on top of the base, a lifting mechanism between the base and the main board, and sub-plates on all four sides of the main board. The sub-plates are detachably connected to the main board via an installation mechanism. The installation mechanism includes a rectangular block fixed to one side of the sub-plate. Rectangular slots are formed on all four sides of the main board, and the rectangular block is inserted into the rectangular slots.

[0007] Preferably, the mounting mechanism further includes a limiting hole formed in the motherboard, the limiting hole being connected to the second rectangular groove, a limiting rod being fixed on one side of the rectangular block near the second rectangular groove, the limiting rod being inserted into the limiting hole, and a rubber pad being fixed in the limiting hole.

[0008] Preferably, the mounting mechanism further includes a magnet one fixed to the end of the limiting rod away from the rectangular block, and a magnet two fixed in the limiting hole, wherein the magnet one and the magnet two are magnetically attracted to each other.

[0009] Preferably, the mounting mechanism further includes a rectangular groove one formed on the side of the sub-plate away from the rectangular block, wherein the rectangular groove one and the rectangular groove two are the same in size and shape.

[0010] Preferably, the lifting mechanism includes a support base fixed on the base, and a lead screw is rotatably connected between the support bases via bearings. A threaded block is threadedly connected to the outer surface of the lead screw.

[0011] Preferably, the lifting mechanism further includes a crossbar fixed on the threaded block, and a diagonal bar is rotatably connected to the crossbar, with the end of the diagonal bar away from the crossbar rotatably connected to the main board.

[0012] Preferably, the lifting mechanism further includes a second inclined bar rotatably connected to the base. A rectangular bar is fixed at the bottom of the main board, and a sliding groove is provided in the rectangular bar. A sliding rod is rotatably connected to the end of the second inclined bar away from the base, and the sliding rod slides in the sliding groove.

[0013] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0014] 1. The installation mechanism facilitates the assembly and disassembly of the drone hangar landing platform. The sub-plate is inserted into the rectangular slot of the main plate via a rectangular block, and a limiting rod is inserted into the limiting hole. The magnetic attraction between magnets one and two, along with the increased friction from the rubber pad, ensures a stable connection between the sub-plate and the main plate. This detachable connection method allows the sub-plate to be easily removed from the main plate when needed, significantly reducing the overall size of the landing platform. This makes it easy to carry and transport, enabling rapid assembly and redeployment in different locations, effectively improving work efficiency and enhancing the flexibility of the landing platform.

[0015] 2. The lifting mechanism allows for flexible adjustment of the drone hangar landing platform height. This enables the landing platform to be adjusted according to different usage needs, drone types, and site conditions, providing a more suitable landing environment for the drone and ensuring the safety and stability of the drone landing. At the same time, adjusting the height further enhances portability. Attached Figure Description

[0016] Figure 1 This is a three-dimensional structural diagram of a drone hangar landing platform proposed in this utility model;

[0017] Figure 2 This is a side view of the overall structure of a drone hangar landing platform proposed in this utility model;

[0018] Figure 3 This is a bottom view of the overall structure of a drone hangar landing platform proposed in this utility model;

[0019] Figure 4 This is a schematic diagram showing the separation of the main board and sub-board structure of a drone hangar landing platform proposed in this utility model.

[0020] Figure 5 This utility model Figure 4 Enlarged schematic diagram of the structure at point A in the middle;

[0021] Figure 6 This is a schematic diagram of the internal structure of the mainboard of a drone hangar landing platform proposed in this utility model.

[0022] In the diagram: 1. Base; 2. Main board; 3. Sub-board; 40. Support base; 41. Lead screw; 42. Threaded block; 43. Crossbar; 44. Diagonal strip one; 45. Diagonal strip two; 46. Rectangular strip; 47. Slide groove; 48. Slide rod; 50. Rectangular groove one; 51. Rectangular groove two; 52. Rectangular block; 53. Limiting hole; 54. Limiting rod; 55. Rubber pad; 56. Magnet one; 57. Magnet two. Detailed Implementation

[0023] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present utility model. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of the present utility model without creative effort are within the protection scope of the present utility model.

[0024] Example 1

[0025] Reference Figures 1-6 A drone hangar landing platform includes a base 1, a main board 2 on top of the base 1, a lifting mechanism between the base 1 and the main board 2, and sub-plates 3 on all four sides of the main board 2. The sub-plates 3 are detachably connected to the main board 2 through an installation mechanism. The installation mechanism includes a rectangular block 52 fixed to one side of the sub-plate 3. Rectangular slots 51 are opened on all four sides of the main board 2, and the rectangular block 52 is inserted into the rectangular slots 51.

[0026] Furthermore, the installation mechanism also includes a limiting hole 53 opened in the main board 2. The limiting hole 53 is connected to the second rectangular groove 51. A limiting rod 54 is fixed on one side of the rectangular block 52 near the second rectangular groove 51. The limiting rod 54 is inserted into the limiting hole 53. A rubber pad 55 is fixed in the limiting hole 53.

[0027] Furthermore, the installation mechanism also includes a magnet 56 fixed to one end of the limiting rod 54 away from the rectangular block 52, and a magnet 57 fixed in the limiting hole 53, with the magnet 56 and the magnet 57 magnetically attracted to each other.

[0028] Furthermore, the mounting mechanism also includes a rectangular groove 50 on the side of the sub-plate 3 away from the rectangular block 52, and the rectangular groove 50 and the rectangular groove 51 are the same in size and shape.

[0029] When assembling the drone hangar landing platform, the rectangular block 52 on the sub-board 3 is aligned with the rectangular slot 51 around the main board 2, and the rectangular block 52 is inserted into the rectangular slot 51. This process achieves the initial positioning and connection between the sub-board 3 and the main board 2, laying the foundation for a more stable connection later. At the same time as the rectangular block 52 is inserted into the rectangular slot 51, the limiting rod 54 fixed on the side of the rectangular block 52 will be aligned with and inserted into the limiting hole 53 in the main board 2 that communicates with the rectangular slot 51. The rubber pad 55 fixed in the limiting hole 53 will be in close contact with the limiting rod 54. The elasticity and friction of the rubber pad 55 will further limit the movement of the limiting rod 54 in the limiting hole 53, thereby enhancing the stability of the connection between the sub-board 3 and the main board 2.

[0030] The magnet 56 fixed at the end of the limiting rod 54 away from the rectangular block 52 will approach the magnet 57 fixed in the limiting hole 53 after the limiting rod 54 is inserted into the limiting hole 53. Since the magnet 56 and the magnet 57 are magnetically attracted, the magnetic force generated will further firmly attract the limiting rod 54 into the limiting hole 53, thereby further enhancing the connection stability between the sub-board 3 and the main board 2.

[0031] By creating a rectangular slot 50 on the side of the sub-plate 3 away from the rectangular block 52, the same components as those in the rectangular slot 51 are installed in the rectangular slot 50. The rectangular slot 50 is the same size and shape as the rectangular slot 51 on the main plate 2. This means that when it is necessary to further expand the landing platform area, other sub-plates 3 can be inserted into the rectangular slot 50 of the sub-plate 3. Through the same installation method, the multi-module assembly of the landing platform can be realized to meet the landing platform area requirements of different scenarios. When it is necessary to disassemble the landing platform for carrying or redeployment, it is only necessary to overcome the magnetic force of magnet 56 and magnet 57, and the friction between rubber pad 55 and limit rod 54, pull the limit rod 54 out of the limit hole 53, and at the same time pull the rectangular block 52 out of the rectangular slot 51. The sub-plate 3 can then be removed from the main plate 2, which greatly reduces the volume of the landing platform and makes it convenient to carry and transport.

[0032] Based on Example 1, Example 2:

[0033] Reference Figures 1-6 ,

[0034] Furthermore, the lifting mechanism includes a support base 40 fixed on the base 1, a lead screw 41 rotating between the support bases 40 via bearings, and a threaded block 42 threadedly connected to the outer surface of the lead screw 41.

[0035] Furthermore, the lifting mechanism also includes a crossbar 43 fixed on the threaded block 42, and a diagonal bar 44 is rotatably connected to the crossbar 43. The end of the diagonal bar 44 away from the crossbar 43 is rotatably connected to the main board 2.

[0036] Furthermore, the lifting mechanism also includes a second inclined bar 45 rotatably connected to the base 1, a rectangular bar 46 fixed at the bottom of the main board 2, a groove 47 opened in the rectangular bar 46, and a sliding rod 48 rotatably connected to the end of the second inclined bar 45 away from the base 1, the sliding rod 48 sliding in the groove 47.

[0037] By driving the lead screw 41 to rotate, either by installing a motor or manually rotating the lead screw 41, the threaded block 42 will move along the axial direction of the lead screw 41 due to the action of the thread. The crossbar 43 fixed on the threaded block 42 will move synchronously with the movement of the threaded block 42. At this time, the inclined bar 44 will rotate around the connection point with the crossbar 43, and at the same time push the main plate 2 to rise and fall vertically. Thus, when the crossbar 43 moves to the right, the inclined bar 44 will lift upward, thereby lifting the main plate 2 and raising the lowering platform. Conversely, when the crossbar 43 moves to the left, the inclined bar 44 will lift upward. The first 44 will pull the main board 2 downward, lowering the landing platform. During the raising and lowering of the main board 2, the second 45 will rotate around the connection point with the base 1, and the slide bar 48 will slide in the slide groove 47, playing a role in assisting support and stabilizing the raising and lowering of the main board 2. Through the cooperation of the first 44, the second 45, the slide bar 48 and the slide groove 47, the main board 2 can be raised and lowered smoothly and accurately. This allows the landing platform to flexibly adjust its height according to different usage needs, drone types and site conditions, providing a more suitable landing environment for the drone. At the same time, by adjusting the height, portability is further improved.

[0038] The above description is only a preferred embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any equivalent substitutions or changes made by those skilled in the art within the technical scope disclosed in the present utility model, based on the technical solution and the inventive concept of the present utility model, should be included within the protection scope of the present utility model.

Claims

1. A drone hangar landing platform, comprising a base (1), characterized in that, A main board (2) is provided above the base (1). A lifting mechanism is provided between the base (1) and the main board (2). Sub-plates (3) are provided around the main board (2). The sub-plates (3) are detachably connected to the main board (2) through an installation mechanism. The installation mechanism includes a rectangular block (52) fixed on one side of the sub-plate (3). A rectangular slot (51) is provided around the main board (2). The rectangular block (52) is inserted into the rectangular slot (51).

2. The unmanned aerial vehicle (UAV) hangar landing platform according to claim 1, characterized in that, The mounting mechanism also includes a limiting hole (53) opened in the main board (2), the limiting hole (53) is connected to the second rectangular groove (51), the side of the rectangular block (52) near the second rectangular groove (51) is fixed with a limiting rod (54), the limiting rod (54) is inserted into the limiting hole (53), and a rubber pad (55) is fixed in the limiting hole (53).

3. The unmanned aerial vehicle (UAV) hangar landing platform according to claim 2, characterized in that, The mounting mechanism also includes a magnet (56) fixed to one end of the limiting rod (54) away from the rectangular block (52), and a magnet (57) fixed in the limiting hole (53), wherein the magnet (56) and the magnet (57) are magnetically attracted to each other.

4. The unmanned aerial vehicle (UAV) hangar landing platform according to claim 1, characterized in that, The mounting mechanism also includes a rectangular groove one (50) opened on the side of the sub-plate (3) away from the rectangular block (52), and the rectangular groove one (50) and the rectangular groove two (51) are the same in size and shape.

5. A drone hangar landing platform according to claim 1, characterized in that, The lifting mechanism includes a support base (40) fixed on the base (1), and a lead screw (41) is rotatably connected between the support bases (40) via bearings. A threaded block (42) is threadedly connected to the outer surface of the lead screw (41).

6. A drone hangar landing platform according to claim 5, characterized in that, The lifting mechanism also includes a crossbar (43) fixed on the threaded block (42), and a diagonal bar (44) is rotatably connected to the crossbar (43). The end of the diagonal bar (44) away from the crossbar (43) is rotatably connected to the main board (2).

7. A drone hangar landing platform according to claim 1, characterized in that, The lifting mechanism also includes a second inclined bar (45) rotatably connected to the base (1). A rectangular bar (46) is fixed at the bottom of the main board (2). A groove (47) is provided in the rectangular bar (46). A sliding rod (48) is rotatably provided at the end of the second inclined bar (45) away from the base (1). The sliding rod (48) slides in the groove (47).

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