Unmanned aerial vehicle maintenance and detection support

Abstract

The utility model discloses an unmanned aerial vehicle maintenance and detection support, and particularly relates to the technical field of unmanned aerial vehicle maintenance, the unmanned aerial vehicle maintenance and detection support comprises a supporting mechanism, the supporting mechanism comprises a rotating disc, two screw rod lifting devices are symmetrically arranged at the top of the rotating disc, and connecting rods are arranged at the sliding ends of the two screw rod lifting devices; the unmanned aerial vehicle device comprises two connecting rods, the two ends of each connecting rod are each provided with a clamping mechanism, each clamping mechanism comprises a base, and the top of each base is provided with a first clamping block and a second clamping block which can slide relatively. In the process of inspecting, disassembling and assembling the unmanned aerial vehicle device, the height and the placing direction of the unmanned aerial vehicle device are adjusted through the supporting mechanism, the space layout is optimized, personnel operation is facilitated, meanwhile, personnel walking is reduced, the working efficiency and safety are improved, and the fatigue feeling of workers in the unmanned aerial vehicle maintaining process is effectively relieved.

Description

Technical Field

[0001] This utility model relates to the field of drone maintenance technology, specifically to a drone maintenance and testing bracket. Background Technology

[0002] A drone is an unmanned aircraft controlled by radio remote control equipment and its own program control device. Currently, drones are used in various fields. Small drones are generally used for civilian entertainment. Common small drones are aerial photography drones. Medium-sized drones are usually used in agriculture, logistics and distribution, police security, forest fire prevention and other fields. Large drones are usually used for military security.

[0003] After a period of flight operations, existing agricultural drones typically undergo overall maintenance and inspection. This maintenance usually includes external cleaning, internal inspection, mechanical component maintenance, propeller safety checks, motor testing and cleaning, and sensor calibration. These inspections need to be conducted at a maintenance location, and the drone needs to be supported during the maintenance process to allow staff to easily view and operate it. However, existing drone maintenance support structures still have shortcomings in use. The drone support structure usually only provides support for the drone, and staff have to walk around the support structure and the drone, adjusting their body posture to observe and disassemble the drone structure. The drone cannot be in a state where staff can freely adjust it while on the support structure. Utility Model Content

[0004] The purpose of this invention is to provide a drone maintenance and inspection bracket to address the aforementioned shortcomings in the technology.

[0005] To achieve the above objectives, this utility model provides the following technical solution:

[0006] A drone maintenance and inspection bracket includes a support mechanism. The support mechanism includes a turntable. Two lead screw lifting devices are symmetrically arranged on the top of the turntable. Each of the two lead screw lifting devices has a connecting rod at its sliding end. Each of the two connecting rods has a clamping mechanism at both ends. The clamping mechanism includes a base. The top of the base has two relatively slidable first clamping blocks and second clamping blocks.

[0007] Preferably, the top of the base is provided with a mounting groove, a screw is provided in the mounting groove, and the bottom of the first clamping block and the second clamping block are both provided with sliders, the sliders are threadedly connected to the screw, and the end of the screw is connected to a motor.

[0008] Preferably, the top of the base is provided with a sliding groove, and the bottom of both the first clamping block and the second clamping block are provided with sliding plates that cooperate with the sliding groove.

[0009] Preferably, the top of the turntable is also provided with a guide rail, the surface of the guide rail is provided with a guide groove, a guide block is provided in the guide groove, and one end of the guide block is connected to the connecting rod.

[0010] Preferably, a drone device is placed on top of the clamping mechanism, and the inner walls of the first clamping block and the second clamping block are both soft structures.

[0011] Preferably, the outer wall of the turntable is symmetrically provided with two platforms, and the platforms are arc-shaped structures.

[0012] Preferably, the inner wall of the platform is also provided with a traction device. The traction device includes a fixed seat, a shaft seat is provided at the bottom of the fixed seat, a main traction rod is provided on one side of the shaft seat, a rotatable auxiliary traction rod is connected to one end of the main traction rod, a traction cable is connected to one end of the auxiliary traction rod, and a traction hook is fixed to the end of the traction cable.

[0013] The technical effects and advantages provided by this utility model in the above technical solution are as follows:

[0014] The support mechanism allows for the lifting, lowering, and rotation of the drone device. During the inspection and disassembly of the drone device, the support mechanism can adjust the height and orientation of the drone device, optimize the spatial layout, facilitate personnel operation, reduce personnel movement, improve work efficiency and safety, and effectively alleviate the fatigue of staff during drone maintenance. Attached Figure Description

[0015] To more clearly illustrate the technical solutions in the embodiments of this application or the prior art, the drawings used in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments recorded in this utility model. For those skilled in the art, other drawings can be obtained based on these drawings.

[0016] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0017] Figure 2 for Figure 1 A status diagram showing the placement of a drone device;

[0018] Figure 3 This is a schematic diagram of the platform and turntable of this utility model;

[0019] Figure 4 This is a schematic diagram of the clamping mechanism, screw lifting device, and drone device of this utility model.

[0020] Figure 5This is a perspective view of the clamping mechanism and lead screw lifting device of this utility model;

[0021] Figure 6 This is a schematic diagram of the clamping mechanism of this utility model;

[0022] Figure 7 This is an exploded view of the clamping mechanism of this utility model;

[0023] Figure 8 This is a perspective view of the platform and traction device of this utility model;

[0024] Figure 9 This is a schematic diagram of the traction device of this utility model;

[0025] Figure 10 This is a state diagram of the traction device of this utility model for tractioning unmanned aerial vehicles.

[0026] Explanation of reference numerals in the attached figures:

[0027] 1. Platform; 2. Unmanned aerial vehicle (UAV) device; 3. Turntable; 4. Screw jacking device;

[0028] 5. Traction device; 51. Main traction rod; 52. Axle seat; 53. Fixed seat; 54. Secondary traction rod; 55. Traction cable; 56. Traction hook;

[0029] 6. Clamping mechanism; 61. Slide groove; 62. First clamping block; 63. Second clamping block; 64. Motor; 65. Base; 66. Mounting groove; 67. Slider; 68. Slide plate; 69. Screw;

[0030] 7. Guide rail; 8. Connecting rod; 9. Guide groove; 10. Guide block. Detailed Implementation

[0031] To enable those skilled in the art to better understand the technical solution of this utility model, the present utility model will be further described in detail below with reference to the accompanying drawings.

[0032] This utility model provides, for example Figure 1 - Figure 3 The UAV maintenance and inspection bracket shown includes a support mechanism, which includes a turntable 3. Two lead screw lifting devices 4 are symmetrically arranged on the top of the turntable 3. Each of the two lead screw lifting devices 4 has a connecting rod 8 at its sliding end. Each of the two connecting rods 8 has a clamping mechanism 6 at both ends. The clamping mechanism 6 includes a base 65. The top of the base 65 has two relatively sliding first clamping blocks 62 and second clamping blocks 63.

[0033] The staff controls the drone device 2 to fly above the clamping mechanism 6 and places the bottom legs of the drone device 2 on the base 65 of the clamping mechanism 6. The legs are clamped by the first clamping block 62 and the second clamping block 63, making the drone device 2 stable. During the maintenance and inspection of the drone device 2, the drone device 2 and the turntable 3 can be rotated by manually pushing the screw lifting device 4, which makes it easy to view different positions of the drone device 2. The connecting rod 8 and the clamping mechanism 6 are raised and lowered synchronously by the screw lifting device 4, which allows the bottom and top of the drone device 2 to be viewed.

[0034] like Figure 6 and Figure 7 As shown, the top of the base 65 is provided with a mounting groove 66, and a screw 69 is provided in the mounting groove 66. The bottom of the first clamping block 62 and the second clamping block 63 are both provided with sliders 67, which are threadedly connected to the screw 69. The end of the screw 69 is connected to a motor 64.

[0035] The drone device 2 is placed on top of the clamping mechanism 6. The inner walls of the first clamping block 62 and the second clamping block 63 are both soft structures. After the bottom feet of the drone device 2 land on the base 65, the motor 64 is started. The output shaft of the motor 64 drives the screw 69 to rotate. The screw 69 is a bidirectional screw. During the rotation of the screw 69, the sliders 67 at the bottom of the first clamping block 62 and the second clamping block 63 move closer to each other on the screw 69. During the process of the first clamping block 62 and the second clamping block 63 moving closer to each other, the bottom feet of the drone device 2 are clamped, so that the drone device 2 is stable and does not move.

[0036] like Figure 6 and Figure 7 As shown, a groove 61 is provided on the top of the base 65, and a sliding plate 68 that cooperates with the groove 61 is provided on the bottom of the first clamping block 62 and the second clamping block 63. During the movement of the first clamping block 62 and the second clamping block 63, the sliding plate 68 moves in a straight line in the groove 61 on the top of the base 65, making the movement of the first clamping block 62 and the second clamping block 63 more stable.

[0037] like Figure 5 As shown, a guide rail 7 is also provided on the top of the turntable 3. A guide groove 9 is provided on the surface of the guide rail 7. A guide block 10 is provided in the guide groove 9. One end of the guide block 10 is connected to the connecting rod 8. During the process of the screw lifting device 4 driving the connecting rod 8 to move up and down, the connecting rod 8 drives the guide block 10 to move in the guide groove 9. The linear movement of the guide block 10 in the guide groove 9 can improve the stability of the movement of the connecting rod 8.

[0038] like Figure 8 , Figure 9 and Figure 10As shown, two platforms 1 are symmetrically arranged on the outer wall of the turntable 3. The platform 1 has an arc-shaped structure. By standing on the platform 1, the staff can have a better viewing angle to observe the drone device 2.

[0039] The inner wall of platform 1 is also equipped with a traction device 5. The traction device 5 includes a fixed seat 53, a bearing seat 52 at the bottom of the fixed seat 53, a main traction rod 51 on one side of the bearing seat 52, a rotatable auxiliary traction rod 54 connected to one end of the main traction rod 51, a traction cable 55 connected to one end of the auxiliary traction rod 54, and a traction hook 56 fixed to the end of the traction cable 55. During the maintenance of the UAV device 2, the flight status of the UAV device 2 is usually checked. The auxiliary traction rod 54 is manually deployed, and the traction hook 56 is pulled by hand and placed on the wing of the UAV device 2. The UAV device 2 is started by pulling the wing through the traction hook 56. During the takeoff process, the UAV device 2 is pulled and held by the traction hook 56, the traction cable 55, the auxiliary traction rod 54 and the main traction rod 51. The UAV device 2 cannot take off upward. During this process, the staff observes whether there are any problems with the flight status of the UAV device 2.

[0040] The foregoing description only illustrates certain exemplary embodiments of the present invention. Undoubtedly, those skilled in the art can modify the described embodiments in various ways without departing from the spirit and scope of the present invention. Therefore, the above drawings and descriptions are illustrative in nature and should not be construed as limiting the scope of protection of the claims of the present invention.

Claims

1. A maintenance and inspection bracket for unmanned aerial vehicles (UAVs), characterized in that: The support mechanism includes a turntable (3), and two screw lifting devices (4) are symmetrically arranged on the top of the turntable (3). The sliding ends of the two screw lifting devices (4) are provided with connecting rods (8), and the two ends of the two connecting rods (8) are provided with clamping mechanisms (6). The clamping mechanism (6) includes a base (65), and the top of the base (65) is provided with two relatively sliding first clamping blocks (62) and second clamping blocks (63).

2. The UAV maintenance and inspection bracket according to claim 1, characterized in that: The base (65) has a mounting groove (66) on its top, and a screw (69) is provided in the mounting groove (66). The bottom of the first clamping block (62) and the second clamping block (63) are both provided with sliders (67). The sliders (67) are threadedly connected to the screw (69), and the end of the screw (69) is connected to a motor (64).

3. The UAV maintenance and inspection bracket according to claim 2, characterized in that: The base (65) has a groove (61) on its top, and the bottom of the first clamping block (62) and the second clamping block (63) are provided with a sliding plate (68) that cooperates with the groove (61).

4. The UAV maintenance and inspection bracket according to claim 1, characterized in that: The top of the turntable (3) is also provided with a guide rail (7), and a guide groove (9) is provided on the surface of the guide rail (7). A guide block (10) is provided in the guide groove (9), and one end of the guide block (10) is connected to the connecting rod (8).

5. The UAV maintenance and inspection bracket according to claim 1, characterized in that: The top of the clamping mechanism (6) is equipped with a drone device (2), and the inner walls of the first clamping block (62) and the second clamping block (63) are both soft structures.

6. The UAV maintenance and inspection bracket according to claim 1, characterized in that: The turntable (3) has two symmetrically arranged platforms (1) on its outer wall, and the platforms (1) are arc-shaped.

7. The UAV maintenance and inspection bracket according to claim 6, characterized in that: The inner wall of the platform (1) is also provided with a traction device (5). The traction device (5) includes a fixed seat (53). The bottom of the fixed seat (53) is provided with a bearing seat (52). A main traction rod (51) is provided on one side of the bearing seat (52). One end of the main traction rod (51) is connected to a rotatable auxiliary traction rod (54). One end of the auxiliary traction rod (54) is connected to a traction cable (55). The end of the traction cable (55) is fixed with a traction hook (56).

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