Unmanned aerial vehicle overhauling device

Abstract

The utility model discloses an unmanned aerial vehicle overhauling device, belongs to the technical field of unmanned aerial vehicle maintenance, and aims to solve the problem that the overhauling process is not convenient enough due to the fact that an unmanned aerial vehicle needs to be frequently rotated to adjust the orientation in the overhauling process when an overhauling table is used in the prior art. Comprising an overhauling table, a lamp panel, a bearing table and a containing box, the bearing table is fixedly installed on the upper surface of the overhauling table, the bearing table is hollow, an inner rotating plate is rotatably installed in the bearing table in an embedded mode, the inner rotating plate and the bearing table are distributed concentrically, a supporting rod is fixed to the side wall of the overhauling table, and the lamp panel is installed on the upper surface of the supporting rod; a turnover plate is rotationally connected to the overhauling table, the opening and closing angle is 90 degrees, and the containing box is fixed to the surface of the turnover plate. According to the unmanned aerial vehicle overhauling device, cabin limiting can be conducted on an unmanned aerial vehicle, the clamping blocks are elastically supported through the first springs, the clamping blocks are attached to the outer wall of the bottom end of the cabin to clamp the cabin, the unmanned aerial vehicle can be fixed, and operation is convenient.

Description

Technical Field

[0001] The utility model belongs to the technical field of unmanned aerial vehicle maintenance, and in particular relates to an unmanned aerial vehicle maintenance device. Background Art

[0002] A drone is an aircraft that can fly and perform tasks without human control. It is usually operated by remote control or preset autonomous flight programs, and can be used in various fields such as military reconnaissance, aerial photography, disaster relief, and agricultural operations. Drone maintenance and overhaul is a very important procedure that ensures the safety and performance of drones. Maintenance and overhaul include daily inspections: regular daily inspections of drones, including the integrity and functional status of components such as appearance, structure, propellers, batteries, and sensors; component replacement: regular replacement of key components of drones, such as batteries, propellers, sensors, etc., to ensure their normal operation; software updates: drone software needs to be updated regularly to ensure that its system can operate normally and adapt to new flight environments; troubleshooting: when a drone fails, it needs to be troubleshooted in a timely manner and the problem needs to be fixed. When a drone needs to be troubleshooted or components replaced, the drone needs to be disassembled as a whole, usually on a maintenance table. The maintenance table requires frequent rotation of the drone to adjust its direction during the maintenance process, making the maintenance process inconvenient, and there are many blind spots for observation and disassembly and assembly of parts. Therefore, the inventor proposes a drone maintenance device. Utility Model Content

[0003] (1) Technical issues to be solved

[0004] In view of the shortcomings of the prior art, the purpose of the present invention is to provide a drone maintenance device, which aims to solve the problem that the prior art uses a maintenance table that requires frequent rotation of the drone to adjust the direction during the maintenance process, making the maintenance process inconvenient.

[0005] (2) Technical solution

[0006] In order to solve the above technical problems, the utility model provides such a UAV maintenance device, including an inspection platform, a light board, a bearing platform and a placement box, the upper surface of the inspection platform is fixedly installed with the bearing platform, the interior of the bearing platform is hollow, and an inner rotating plate is embedded and rotatably installed, the inner rotating plate is coaxially distributed with the bearing platform, a support rod is fixed on the side wall of the inspection platform, and a light board is installed on the upper surface of the support rod; a flip plate is rotatably connected on the inspection platform, and the opening and closing angle is 90 degrees, and the placement box is fixed on the surface of the flip plate; a guide slot is horizontally opened on the upper surface of the inner rotating plate, and two groups of relatively elastically installed clamping blocks are arranged inside the guide slot, a fixed tube is fixedly installed on the outer wall of the bearing platform, and a limited plug plate is inserted into the interior of the fixed tube. Thanks to the setting of the inner rotating plate and the bearing platform, the cabin of the UAV can be limited, and the clamping block is elastically supported by the first spring, and the clamping block is attached to the outer wall of the bottom end of the cabin to clamp it, so that the UAV can be fixed, and the operation is convenient.

[0007] Preferably, a support slide bar is horizontally fixed inside the guide slide groove, a slide hole is penetrated through the clamping block, and the clamping block and the support slide bar are slidably installed.

[0008] Preferably, a first spring is fixedly connected inside the clamping block. The first spring is horizontally arranged, and one end of the first spring away from the clamping block is fixedly connected to the inner wall of the guide slot.

[0009] Preferably, tooth blocks are protruding from the outer circumferential surface of the inner rotating plate, and multiple groups of the tooth blocks are distributed around the outer circumferential surface of the rotating plate.

[0010] Preferably, the limit plug plate corresponds to the gap between the tooth block, and the limit plug plate passes through the fixing tube and extends into the inner side of the bearing platform to be plugged with the tooth block.

[0011] Preferably, a portion of the limiting plug plate located inside the fixed tube is provided with a limiting block, and the limiting block is vertically distributed and fixedly connected to the limiting plug plate.

[0012] Preferably, a second spring is fixedly connected to the upper surface of the limiting block, the second spring is sleeved on the outer wall of the limiting plug plate, and the end away from the limiting block is fixedly connected to the inner wall of the fixed pipe.

[0013] (3) Beneficial effects

[0014] Compared with the prior art, the beneficial effects of the utility model are:

[0015] Thanks to the arrangement of the inner rotating plate and the bearing platform, the utility model can limit the cabin of the UAV. The first spring elastically supports the clamping block, and the clamping block fits against the bottom outer wall of the cabin to clamp it, so that the UAV can be fixed. The operation is convenient. During the maintenance process, the limit plug plate is pulled, and the limit plug plate drives the limit block to move toward the direction of the second spring. The second spring is compressed by the force, and the end of the limit plug plate is separated from the tooth block. Then the inner rotating plate loses the limit and can rotate inside the bearing platform, driving the UAV above to rotate and perform scheduling and direction adjustment. The UAV can be viewed from different angles and the parts can be disassembled. The operation is convenient and can be widely promoted. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present application. For those skilled in the art, other drawings can be obtained based on these drawings without paying any creative work.

[0017] Figure 1 It is a schematic diagram of the structure of the utility model;

[0018] Figure 2 It is a structural schematic diagram of the flip board in the folded state;

[0019] Figure 3 It is a structural schematic diagram of the separation state of the bearing platform and the clamping block;

[0020] Figure 4 It is a schematic diagram of the structure of the inner rotating plate and the bearing platform.

[0021] The markings in the attached drawings are: 1. Maintenance table; 2. Placement box; 3. Load-bearing platform; 4. Support rod; 5. Light board; 6. Flip plate; 7. Inner rotating plate; 8. Clamping block; 9. First spring; 11. Slide hole; 12. Support slide rod; 13. Guide slide groove; 14. Limit plug plate; 15. Fixed tube; 16. Limit block; 17. Second spring; 18. Tooth block. DETAILED DESCRIPTION

[0022] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in 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.

[0023] This specific implementation is a UAV maintenance device, and its structural diagram is as follows Figure 1 , Figure 2 As shown, it includes an inspection platform 1, a light board 5, a bearing platform 3 and a placement box 2. The bearing platform 3 is fixedly installed on the upper surface of the inspection platform 1. The interior of the bearing platform 3 is hollow and has an inner rotating plate 7 rotatably installed therein. The inner rotating plate 7 is cocentrically distributed with the bearing platform 3. A support rod 4 is fixed on the side wall of the inspection platform 1, and a light board 5 is installed on the upper surface of the support rod 4; a flip plate 6 is rotatably connected to the inspection platform 1, and the opening and closing angle is ninety degrees, and the placement box 2 is fixed on the surface of the flip plate 6; a guide groove 13 is horizontally opened on the upper surface of the inner rotating plate 7, and two groups of relatively elastically installed clamping blocks 8 are arranged inside the guide groove 13; a fixing tube 15 is fixedly installed on the outer wall of the bearing platform 3, and a limited position plug 14 is inserted into the interior of the fixing tube 15 for sliding.

[0024] Reference Figure 3 , Figure 4 , a support slide bar 12 is horizontally fixed inside the guide slide groove 13, and a slide hole 11 is opened through the clamping block 8, and the clamping block 8 and the support slide bar 12 are slidably installed. A first spring 9 is fixedly connected inside the clamping block 8, and the first spring 9 is horizontally arranged, and the end away from the clamping block 8 is fixedly connected to the inner wall of the guide slide groove 13. A tooth block 18 is protruding on the outer circumferential surface of the inner rotating plate 7, and multiple groups of tooth blocks 18 are distributed around the outer circumferential surface of the rotating plate. The gap between the limit plug 14 and the tooth block 18 corresponds to the limit plug 14, and the limit plug 14 passes through the fixed tube 15 and extends into the inner side of the bearing platform 3 to cooperate with the tooth block 18. The part of the limit plug 14 located inside the fixed tube 15 is provided with a limit block 16, and the limit block 16 and the limit plug 14 are vertically distributed and fixedly connected to each other. The upper surface of the limiting block 16 is fixedly connected with a second spring 17 . The second spring 17 is sleeved on the outer wall of the limiting plug plate 14 , and the end away from the limiting block 16 is fixedly connected to the inner wall of the fixing tube 15 .

[0025] Working principle: When in use, first place the drone on the upper surface of the inner rotating plate 7, remove the supporting feet at the bottom of the drone, fit the bottom of the cabin to the upper surface of the inner rotating plate 7, and use the first spring 9 to elastically support the clamping block 8, so that the clamping block 8 fits the bottom outer wall of the cabin to clamp it. At this time, the drone can be fixed, and then the light board 5 is turned on to illuminate the drone, and the flip plate 6 is opened. At this time, the placement box 2 is exposed, and the drone can be disassembled, and the disassembled parts are placed in the placement box 2 to avoid loss. During the maintenance process, due to different maintenance positions and the need to observe the drone from different angles, the limit switch can be pulled at this time. The plug plate 14 and the limit plug plate 14 drive the limit block 16 to move toward the direction of the second spring 17. The second spring 17 is compressed by the force, and the end of the limit plug plate 14 is separated from the tooth block 18. Then, the inner rotating plate 7 loses the limit and can rotate inside the supporting platform 3, driving the UAV above to rotate, and adjust the direction. After adjusting to the required position, release the pull on the limit plug plate 14, the second spring 17 is reset, and the limit block 16 is pushed back. The limit block 16 drives the limit plug plate 14 to approach the tooth block 18 and is inserted into the gap between the tooth blocks 18, so that the limit of the inner rotating plate 7 is fixed, and then the adjusted UAV is fixed.

[0026] Finally, it should be noted that the above is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Although the present utility model has been described in detail with reference to the aforementioned embodiments, it is still possible for those skilled in the art to modify the technical solutions described in the aforementioned embodiments, or to make equivalent substitutions for some of the technical features therein. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present utility model shall be included in the protection scope of the present utility model.

Claims

1. A drone maintenance device, comprising a maintenance platform (1), a light board (5), a carrying platform (3) and a placement box (2), characterized in that: A bearing platform (3) is fixedly mounted on the upper surface of the inspection platform (1); the interior of the bearing platform (3) is hollow and has an inner rotating plate (7) embedded therein and rotatably mounted therein; the inner rotating plate (7) is cocentrically distributed with the bearing platform (3); a support rod (4) is fixed on the side wall of the inspection platform (1); a light panel (5) is mounted on the upper surface of the support rod (4); The inspection platform (1) is rotatably connected to a flip plate (6) with an opening and closing angle of ninety degrees, and the placement box (2) is fixed on the surface of the flip plate (6); A guide slot (13) is horizontally provided on the upper surface of the inner rotating plate (7), two groups of relatively elastically mounted clamping blocks (8) are provided inside the guide slot (13), a fixed tube (15) is fixedly installed on the outer wall of the supporting platform (3), and a limited position plug plate (14) is slidably inserted into the interior of the fixed tube (15).

2. The unmanned aerial vehicle maintenance device according to claim 1, characterized in that: A support slide bar (12) is horizontally fixed inside the guide slide groove (13), a slide hole (11) is penetrated through the clamping block (8), and the clamping block (8) and the support slide bar (12) are slidably mounted.

3. The unmanned aerial vehicle maintenance device according to claim 2, characterized in that: A first spring (9) is fixedly connected inside the clamping block (8); the first spring (9) is arranged horizontally, and one end of the first spring (9) away from the clamping block (8) is fixedly connected to the inner wall of the guide slot (13).

4. The unmanned aerial vehicle maintenance device according to claim 1, characterized in that: The outer circumferential surface of the inner rotating plate (7) is provided with tooth blocks (18) protruding therefrom, and the tooth blocks (18) are arranged in a plurality of groups distributed around the outer circumferential surface of the rotating plate.

5. The unmanned aerial vehicle maintenance device according to claim 4, characterized in that: The gap between the limiting plug plate (14) and the tooth block (18) corresponds to each other, and the limiting plug plate (14) passes through the fixing tube (15) and extends into the inner side of the bearing platform (3) to be plugged in with the tooth block (18).

6. The unmanned aerial vehicle maintenance device according to claim 1, characterized in that: The portion of the limiting plug plate (14) located inside the fixed tube (15) is provided with a limiting block (16), and the limiting block (16) and the limiting plug plate (14) are vertically distributed and fixedly connected to each other.

7. The unmanned aerial vehicle maintenance device according to claim 6, characterized in that: A second spring (17) is fixedly connected to the upper surface of the limit block (16); the second spring (17) is sleeved on the outer wall of the limit plug plate (14) and is fixedly connected to the inner wall of the fixed tube (15) at the end away from the limit block (16).

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