Unmanned aerial vehicle floor stand

Abstract

The utility model provides an unmanned aerial vehicle floor stand, and relates to the related field of unmanned aerial vehicles. The unmanned aerial vehicle floor stand comprises a stand body, a connecting mechanism, protection mechanisms, a clamping mechanism and a supporting mechanism, the protection mechanisms are located at the two ends of the stand body, each protection mechanism comprises a protection plate and a hinge, the protection plates are used for protecting an unmanned aerial vehicle, the hinges are located on the surfaces of the protection plates, and the hinges are used for adjusting the use angles of the protection plates. According to the unmanned aerial vehicle floor stand, the front end and the rear end of an unmanned aerial vehicle can be effectively protected through the protection plate, the use angle of the protection plate can be adjusted through the hinges according to the appearance of the unmanned aerial vehicle, the protection efficiency of the protection plate on the unmanned aerial vehicle can be greatly improved, and the service life of the unmanned aerial vehicle is prolonged; and through the clamping mechanism, an adjustable clamping block is rapidly connected and fixed to the unmanned aerial vehicle, so that the protection mechanism can be attached to the unmanned aerial vehicle for adjustment and protection treatment, and use is convenient.

Description

Technical Field

[0001] This application relates to the technical field of drones, and specifically to a drone landing bracket. Background Art

[0002] Unmanned aerial vehicle, abbreviated as "drone", is an unpiloted aircraft controlled by radio remote control equipment and self - contained program control devices, or operated completely or intermittently autonomously by an on - vehicle computer. Compared with piloted aircraft, drones are often more suitable for tasks that are too "stupid, dirty or dangerous". When a drone performs a high - altitude landing operation, a landing bracket is usually used for assistance to prevent the drone from being bumped when landing.

[0003] In the Chinese patent with the patent number CN218751490U, a drone landing bracket is disclosed. This landing bracket has a base made of rubber material. When the drone lands, the entire bracket contacts the ground first, which can eliminate part of the impact vibration generated by touching the ground and reduce the vibration damage of the acting force on the component structure of the drone.

[0004] However, the rubber bracket can only provide a certain degree of buffering. When the landing speed of the drone is too fast, the rubber bracket is difficult to assist the drone in landing support, and the drone will slide forward under the action of inertia, resulting in the front end hitting the ground and being damaged. Utility Model Content

[0005] (1) Technical Problems to be Solved

[0006] In view of the deficiencies of the prior art, this application provides a drone landing bracket, which solves the problems mentioned in the above background art.

[0007] (2) Technical Solutions

[0008] To achieve the above objectives, this application is realized through the following technical solutions: A drone landing bracket includes a bracket body, a connection mechanism, a protection mechanism, a clamping mechanism, and a support mechanism. The protection mechanism is located at both ends of the bracket body. The protection mechanism includes a protection plate for protecting the drone and a hinge. The hinge is located on the surface of the protection plate, and the hinge is used to adjust the use angle of the protection plate.

[0009] By adopting the above - mentioned technical solutions, the protection plate can effectively protect the front end and the rear end of the drone. The hinge can adjust the use angle of the protection plate according to the shape of the drone, so that the protection plate can greatly improve the protection efficiency of the drone and extend the service life of the drone.

[0010] Preferably, the protection mechanism further includes a first chute located at both ends of the inner wall of the bracket body. A moving block is slidably connected inside the first chute. An adjusting block is movably installed on the surface of the moving block. One side of the adjusting block is fixedly installed with a protection plate.

[0011] By adopting the above technical solution, the position of the adjusting block can be stretched through the first chute, so that the protection plate can be attached to the drone for use.

[0012] Preferably, the support mechanism includes a plurality of protection rods. The plurality of protection rods are movably connected to the bracket body. One end of the plurality of protection rods is movably connected to a support plate. A movable shaft is movably installed at the connection of the bracket body, the protection rods and the support plate.

[0013] By adopting the above technical solution, through the support mechanism, when the drone lands, the impact force received can be reduced through the support plate, so that the drone can maintain stability faster.

[0014] Preferably, the connection mechanism includes a telescopic rod. Both ends of the telescopic rod are fixedly connected to the bracket body. Installation holes are formed on the surface of the telescopic rod. A first fixing bolt is threadedly connected inside the installation holes.

[0015] By adopting the above technical solution, the connection mechanism can connect the bracket bodies on both sides. During actual use, the use position of the bracket body can be stretched according to the length of the drone, so as to be connected and fixed with the drone.

[0016] Preferably, the clamping mechanism includes a second chute opened on the surface of the bracket body. A screw rod is arranged inside the second chute. A plurality of clamping blocks for fixing with the drone are slidably connected to the surface of the screw rod.

[0017] By adopting the above technical solution, through the clamping mechanism, the adjustable clamping blocks are quickly connected and fixed with the drone, so that the protection mechanism can be adjusted and protected in accordance with the drone, which is convenient for use.

[0018] Preferably, positioning holes are formed on the surface of the clamping block. A second fixing bolt is threadedly connected inside the positioning holes.

[0019] By adopting the above technical solution, the clamping block can be attached and fixed to the drone through the second fixing bolt.

[0020] (III) Beneficial effects

[0021] This application provides a landing bracket for a drone. The beneficial effects are as follows:

[0022] 1. The landing bracket of the drone can effectively protect the front and rear ends of the drone through the protective plate. The hinge can adjust the use angle of the protective plate according to the shape of the drone, enabling the protective plate to greatly improve the protection efficiency of the drone and extend its service life.

[0023] 2. The landing bracket of the drone is provided with a clamping mechanism. The adjustable clamping block is used to quickly connect and fix the drone, enabling the protective mechanism to adjust the protection treatment in accordance with the drone, which is convenient for use. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] Figure 1 It is a three-dimensional structural schematic diagram of the present application;

[0025] Figure 2 It is the first three-dimensional structural schematic diagram of the bracket body of the present application;

[0026] Figure 3 It is the second three-dimensional structural schematic diagram of the bracket body of the present application;

[0027] Figure 4 For the present application Figure 3 The enlarged three-dimensional structural schematic diagram of the part A in the figure.

[0028] In the figure: 1. Bracket body; 2. Connection mechanism; 20. Telescopic rod; 21. First fixing bolt; 3. Protective mechanism; 30. First sliding groove; 31. Moving block; 32. Adjusting block; 33. Protective plate; 34. Hinge; 4. Clamping mechanism; 40. Second sliding groove; 41. Screw rod; 42. Clamping block; 43. Second fixing bolt; 5. Support mechanism; 50. Protective rod; 51. Moving shaft; 52. Support plate. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0029] The present application will be further described in detail below with reference to the drawings and embodiments.

[0030] Refer to Figure 1 、 Figure 2 、 Figure 3 and Figure 4 According to the embodiments of the present application, a landing bracket for a drone is provided, including a bracket body 1, a connection mechanism 2, a protective mechanism 3, a clamping mechanism 4, and a support mechanism 5. The protective mechanism 3 is located at both ends of the bracket body 1, the connection mechanism 2 is located on one side of the bracket body 1, the clamping mechanism 4 is located at the top of the bracket body 1. The protective mechanism 3 includes a protective plate 33 for protecting the drone and a hinge 34. The hinge 34 is located on the surface of the protective plate 33 and is used to adjust the use angle of the protective plate 33.

[0031] Refer to Figure 1 、 Figure 2 and Figure 3, in one aspect of this embodiment, the protection mechanism 3 further includes a first chute 30 located at both ends of the inner wall of the bracket body 1. A moving block 31 is slidably connected inside the first chute 30. An adjusting block 32 is movably installed on the surface of the moving block 31, and one side of the adjusting block 32 is fixedly installed with a protection plate 33.

[0032] The support mechanism 5 includes a plurality of protection rods 50. The plurality of protection rods 50 are movably connected to the bracket body 1. One end of the plurality of protection rods 50 is movably connected to a support plate 52. A movable shaft 51 is movably installed at the connection of the bracket body 1, the protection rods 50, and the support plate 52.

[0033] After the device is installed on the drone and the drone makes a landing, the support plate 52 will touch the ground first under the extension of the protection rods 50. The impact force on the drone can be greatly reduced through the support plate 52 and the protection rods 50. However, when the inertia of the drone increases, the protection plate 33 extending forward can effectively protect it. The protection plate 33 can adjust its length according to the size of the drone through the moving block 31, and can also change its use angle under the adjustment of the hinge 34, so that it can effectively fit the drone for protection, ensuring that the damage to the drone is reduced.

[0034] Refer to Figure 1 , Figure 3 and Figure 4 , in one aspect of this embodiment, the connection mechanism 2 includes a telescopic rod 20. Both ends of the telescopic rod 20 are fixedly connected to the bracket body 1. Installation holes are formed on the surface of the telescopic rod 20, and a first fixing bolt 21 is threadedly connected inside the installation holes.

[0035] The clamping mechanism 4 includes a second chute 40 formed on the surface of the bracket body 1. A screw rod 41 is arranged inside the second chute 40. The surface of the screw rod 41 is slidably connected with a plurality of clamping blocks 42 for fixing to the drone.

[0036] Positioning holes are formed on the surface of the clamping block 42, and a second fixing bolt 43 is threadedly connected inside the positioning holes.

[0037] Before installing the bracket on the drone, adjust the installation position of the clamping block 42 in the second chute 40 according to the size of the drone, so that the clamping block 42 can fit the bottom of the drone and complete the connection with the drone under the fixation of the second fixing bolt 43. At the same time, stretch the length of the telescopic rod 20 so that both sides of the bracket body 1 can move to the bottom of the drone for connection and fixation.

[0038] All the electrical equipment in this solution is powered by an external power supply.

[0039] Working principle: Before installing the bracket on the drone, according to the size of the drone, adjust the installation position of the clamping block 42 in the second chute 40 so that the clamping block 42 can fit the bottom of the drone, and complete the connection with the drone under the fixation of the second fixing bolt 43. At the same time, stretch the length of the telescopic rod 20 so that the bracket bodies 1 on both sides can move to the bottom of the drone for connection and fixation. When the device is installed on the drone and the drone lands, the support plate 52 will touch the ground first under the extension of the protection rod 50. The impact force on the drone can be greatly reduced through the support plate 52 and the protection rod 50. However, when the inertia of the drone increases, the protection plate 33 extending forward can effectively protect it. The protection plate 33 can adjust its length through the moving block 31 according to the size of the drone, and can also change the use angle under the adjustment of the hinge 34, so that it can effectively fit the drone for protection and ensure that the damage to the drone is reduced.

[0040] It should be noted that in this article, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the term "comprising", "including" or any other variation thereof is intended to cover non-exclusive inclusion, so that a process, method, article or device comprising a series of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such process, method, article or device.

[0041] Although the embodiments of the present application have been shown and described, it will be understood by those of ordinary skill in the art that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present application. The scope of the present application is defined by the appended claims and their equivalents.

Claims

1. A drone landing bracket, comprising a bracket body (1), a connecting mechanism (2), a protective mechanism (3), a clamping mechanism (4) and a supporting mechanism (5), wherein the protective mechanism (3) is located at both ends of the bracket body (1), and is characterized in that: The protection mechanism (3) comprises a protection plate (33) for protecting the drone and a hinge (34); the hinge (34) is located on the surface of the protection plate (33); and the hinge (34) is used to adjust the use angle of the protection plate (33).

2. The UAV landing bracket according to claim 1, characterized in that: The protection mechanism (3) further comprises a first slide groove (30), the first slide groove (30) being located at both ends of the inner wall of the bracket body (1), a moving block (31) being slidably connected inside the first slide groove (30), an adjusting block (32) being movably mounted on the surface of the moving block (31), and one side of the adjusting block (32) being fixedly mounted to the protection plate (33).

3. The UAV landing bracket according to claim 1, characterized in that: The support mechanism (5) comprises a plurality of protection rods (50), the plurality of protection rods (50) being movably connected to the support body (1), one end of the plurality of protection rods (50) being movably connected to a support plate (52), and a movable shaft (51) being movably installed at the connection between the support body (1), the protection rods (50) and the support plate (52).

4. The UAV landing bracket according to claim 1, characterized in that: The connecting mechanism (2) comprises a telescopic rod (20), both ends of which are fixedly connected to the bracket body (1), a mounting hole is provided on the surface of the telescopic rod (20), and a first fixing bolt (21) is threadedly connected to the interior of the mounting hole.

5. The UAV landing bracket according to claim 1, characterized in that: The clamping mechanism (4) comprises a second slide groove (40), the second slide groove (40) is provided on the surface of the bracket body (1), a screw rod (41) is arranged inside the second slide groove (40), and a plurality of clamping blocks (42) for fixing to the drone are slidably connected to the surface of the screw rod (41).

6. The UAV landing bracket according to claim 5, characterized in that: A positioning hole is provided on the surface of the clamping block (42), and a second fixing bolt (43) is threadedly connected inside the positioning hole.

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