Tool for changing empennage of unmanned aerial vehicle

Abstract

The utility model discloses an unmanned aerial vehicle empennage changing tool which comprises a working table and a machine head bracket installed on the front side of the working table, a wing bracket is arranged on the right side of the machine head bracket to lift an unmanned aerial vehicle wing, and a bottom plate is arranged on the rear side of the wing bracket. A tail pressing plate is arranged on the upper side of the bottom plate to fix the position of an empennage of the unmanned aerial vehicle, buffering pads are fixedly connected to the outer wall of the upper end of the bottom plate and the outer wall of the lower end of the tail pressing plate to be attached to the shape of a wing, and by installing a storage hopper, a storage groove a and a storage groove b, detached small parts such as screws and nuts can be placed in the storage groove a; when the unmanned aerial vehicle is disassembled, tools and large parts required by disassembly can be placed in the storage groove b to be stored, so that the tools, unmanned aerial vehicle accessories and parts are orderly placed at designated positions, the time for finding and arranging the tools is shortened, and meanwhile, the loss and damage caused by disordered stacking of the tools can be effectively reduced.

Description

Technical Field

[0001] The utility model belongs to the technical field related to unmanned aerial vehicle tooling, and in particular relates to a tail wing changing tooling for an unmanned aerial vehicle. Background Art

[0002] UAV tail wing modification tools refer to tools and equipment used to replace or adjust the tail wing of a drone. These tools usually include tools such as wrenches, screwdrivers, nuts and bolts of various sizes, as well as brackets and clamps to support and fix the tail wing of the drone. When changing the tail wing of a drone, the operator needs to use these tools to remove the original tail wing components and install new tail wing components. However, when disassembling the tail wing, there are multiple holes for fixing the tools on the workbench, resulting in a lack of suitable storage locations for small parts such as bolts and nuts of the disassembled tail wing, which makes it easy for them to fall through the holes when placed on the workbench and fall to the ground and get lost. Utility Model Content

[0003] The utility model aims to provide a tool for changing the tail wing of an unmanned aerial vehicle, so as to solve the problem in the above-mentioned background technology that small parts such as bolts and nuts for removing the tail wing lack a suitable storage place, which causes them to fall out of holes when placed on a workbench and fall to the ground and be lost.

[0004] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a tail wing modification tool for a UAV, comprising a workbench and a nose bracket installed on the front side of the workbench;

[0005] A wing bracket is arranged on the right side of the nose bracket to support the wings of the UAV;

[0006] A bottom plate is provided on the rear side of the wing bracket;

[0007] A tail pressure plate is arranged on the upper side of the bottom plate to fix the position of the tail wing of the UAV, and a buffer pad is fixedly connected to the upper outer wall of the bottom plate and the lower outer wall of the tail pressure plate to fit the shape of the wing;

[0008] A storage bucket is provided on the upper outer wall of the workbench, and a storage slot a is provided inside the front end outer wall of the storage bucket near the lower side to store parts and small accessories of the drone, and a storage slot b is provided on the front end outer wall of the storage bucket and located on the upper side of the storage slot a to store disassembly tools and larger parts of the drone.

[0009] Preferably, a partition a is fixedly connected to the interior of the storage slot a, and a partition b is fixedly connected to the interior of the storage slot b.

[0010] Preferably, a limit plate is fixedly connected to the right outer wall of the storage bucket, and a magnetic plate is fixedly connected to the right outer wall of the storage bucket for magnetic adsorption and fixation with the workbench.

[0011] Preferably, a plurality of jackets are equidistantly and fixedly connected to the outer wall of the upper end of the storage bucket, and sponge blocks are fixedly connected to the interiors of the plurality of jackets.

[0012] Preferably, a guide slit is provided inside the outer wall of the upper end of the sponge block, and a through opening is provided inside the sponge block to limit the position of the tail wing replacement line.

[0013] Preferably, a sliding rod is fixedly connected to the outer wall of the lower end of the machine head bracket, and a sliding sleeve is provided between the outer wall of the lower end of the sliding rod and the workbench.

[0014] Preferably, the outer wall of the lower end of the wing bracket is transmission-connected with a movable rod b, and the outer wall of the left end of the movable rod b is transmission-connected with a movable rod a.

[0015] Preferably, the outer wall of the lower end of the movable rod a is transmission-connected with a rotating column to adjust the lateral tilt angle of the movable rod a, and a threaded sleeve is fixedly connected between the outer wall of the lower end of the base plate and the workbench.

[0016] Preferably, a threaded rod is provided between the lower outer wall of the tail pressure plate and the threaded sleeve to adjust the height of the tail pressure plate, and an adjusting screw is transmission-connected to the upper outer wall of the tail pressure plate to adjust the up and down movement of the threaded rod inside the threaded sleeve.

[0017] Preferably, a plurality of legs are fixedly connected to the outer wall of the lower end of the workbench, and a plurality of fixing holes are opened on the outer wall of the upper end of the workbench.

[0018] Compared with the prior art, the utility model provides a UAV tail wing modification tooling, which has the following beneficial effects:

[0019] By installing the storage bucket, storage slot a and storage slot b, when disassembling the tail wing of the UAV, the position of the storage bucket can be moved to a range that is convenient for the staff to move. In the process of disassembling the tail wing, the disassembled screws, nuts and small parts can be placed in the storage slot a, and the tools required for disassembly and larger parts can be placed in the storage slot b for storage, so that the tools, UAV accessories and parts are placed in designated locations in an orderly manner, reducing the time for finding and organizing tools, and at the same time can effectively reduce the loss and damage caused by the messy stacking of tools, and can isolate sharp or fragile tools and bolts to reduce the occurrence of accidental injuries. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 The utility model is a schematic diagram of the structure of a UAV tail wing changing tooling.

[0021] Figure 2 This is a structural schematic diagram of a UAV tail wing modification tooling of the utility model when viewed from the left.

[0022] Figure 3 It is a schematic diagram of the partial structure of the storage bucket area in a top view of the present invention.

[0023] Figure 4 It is a schematic diagram of the local structure of the jacket area viewed from above of the utility model.

[0024] Figure 5 It is a schematic diagram of the local structure of the storage bucket area of ​​the utility model.

[0025] In the figure: 1. workbench; 2. head bracket; 3. tail pressure plate; 4. movable rod a; 5. movable rod b; 6. wing bracket; 7. fixing hole; 8. support foot; 9. storage bucket; 10. sliding sleeve; 11. sliding rod; 12. buffer pad; 13. adjusting screw; 14. threaded rod; 15. bottom plate; 16. threaded sleeve; 17. rotating column; 18. limit plate; 19. partition a; 20. storage slot a; 21. partition b; 22. storage slot b; 23. through port; 24. guide seam; 25. sponge block; 26. jacket; 27. magnetic plate. DETAILED DESCRIPTION

[0026] 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.

[0027] The utility model provides Figure 1-3 The tail wing modification tooling of a UAV shown in the figure comprises a workbench 1 and a nose bracket 2 installed on the front side of the workbench 1;

[0028] A wing bracket 6 is provided on the right side of the nose bracket 2 to support the wings of the UAV;

[0029] A bottom plate 15 is provided on the rear side of the wing bracket 6;

[0030] A tail pressure plate 3 is provided on the upper side of the bottom plate 15 to fix the position of the UAV tail wing. The upper outer wall of the bottom plate 15 and the lower outer wall of the tail pressure plate 3 are fixedly connected with a buffer pad 12 to fit the shape of the wing. When changing the tail wing of the UAV, the UAV is lifted according to the position, the head of the UAV is placed on the head bracket 2, and after the wing bracket 6 is adjusted, it is moved to the lower side of the UAV wing for lifting, and the tail wing is lifted on the bottom plate 15 buffer pad 12, and then the tail pressure plate 3 is fixed downward and fixed between the bottom plate 15 to clamp the tail wing, and then the tail wing of the UAV can be disassembled by tools for replacement;

[0031] A storage bucket 9 is provided on the outer wall of the upper end of the workbench 1, and a storage groove a20 is opened near the lower side of the front end outer wall of the storage bucket 9 to store parts and small accessories of the drone. A storage groove b22 is opened on the front end outer wall of the storage bucket 9 and located on the upper side of the storage groove a20 to store disassembly tools and larger parts of the drone. When disassembling the tail wing of the drone, the disassembled screws, bolts and small parts can be put into the storage groove a20 of the storage bucket 9 for temporary storage, and the disassembly tools can be taken out from the storage groove b22 or the disassembly tools and larger usable components disassembled from the tail wing can be stored.

[0032] like Figure 3 As shown, a partition a19 is fixedly connected to the interior of the storage groove a20, and a partition b21 is fixedly connected to the interior of the storage groove b22.

[0033] When placing bolts, nuts and small parts inside the storage slot a20, they can be separated by partition a19 to avoid confusion that affects taking. The disassembly tools and the disassembled tail wing parts can be isolated by partition b21 to avoid the disassembly tools colliding and scratching the tail wing parts.

[0034] like Figure 5 As shown, the right end outer wall of the storage bucket 9 is fixedly connected to the limiting plate 18, and the right end outer wall of the storage bucket 9 is fixedly connected to the magnetic plate 27 for magnetic adsorption and fixation with the workbench 1.

[0035] When the storage bucket 9 is installed, the limit plate 18 and the upper end of the workbench 1 can be abutted against each other, and magnetic adsorption can be performed between the magnetic plate 27 and the workbench 1 to fix the storage bucket 9 on the workbench 1, and the position of the storage bucket 9 can be easily taken and replaced by magnetic means.

[0036] like Figure 4 As shown, a plurality of jackets 26 are equidistantly fixedly connected to the outer wall of the upper end of the storage bucket 9, a sponge block 25 is fixedly connected to the interior of each of the plurality of jackets 26, a guide seam 24 is provided inside the outer wall of the upper end of the sponge block 25, and a through opening 23 is provided inside the sponge block 25 to limit the position of the tail replacement line.

[0037] When replacing the tail wing, it may be necessary to replace the internal circuit. The circuit to be used can be inserted into the through-port 23 through the guide seam 24 and clamped by the sponge block 25 to limit the position of the circuit and avoid the situation where multiple circuits are entangled with each other. At the same time, when taking out the circuit, it can be directly pulled out for easy taking and use.

[0038] like Figure 2 As shown, the lower end outer wall of the head bracket 2 is fixedly connected with a slide rod 11, a sliding sleeve 10 is arranged between the lower end outer wall of the slide rod 11 and the workbench 1, the lower end outer wall of the wing bracket 6 is transmission connected with a movable rod b5, the left end outer wall of the movable rod b5 is transmission connected with a movable rod a4, the lower end outer wall of the movable rod a4 is transmission connected with a rotating column 17 to adjust the lateral inclination angle of the movable rod a4, and a threaded sleeve 16 is fixedly connected between the lower end outer wall of the base plate 15 and the workbench 1.

[0039] The height of the nose bracket 2 can be adjusted by sliding the sliding rod 11 up and down inside the sliding sleeve 10 to adapt to the length of different UAV noses. When the wing bracket 6 lifts the UAV wing, the position of the wing bracket 6 under the UAV wing can be adjusted by adjusting the upper and lower angle positions of the movable rod a4 and the movable rod b5, and by adjusting the rotation angle of the rotating column 17, thereby completing the stable lifting of the wing.

[0040] like Figure 2 As shown, a threaded rod 14 is arranged between the lower outer wall of the tail pressure plate 3 and the threaded sleeve 16 to adjust the height of the tail pressure plate 3, and an adjusting screw 13 is transmission-connected to the upper outer wall of the tail pressure plate 3 to adjust the up and down movement of the threaded rod 14 inside the threaded sleeve 16.

[0041] The tail pressure plate 3 can be driven to move downward by rotating the adjusting screw 13 clockwise, so that the threaded rod 14 installed on the threaded object moves downward inside the threaded sleeve 16, thereby stably clamping the tail wing of the UAV.

[0042] like Figure 1 and Figure 2 As shown, a plurality of legs 8 are fixedly connected to the outer wall of the lower end of the workbench 1 , and a plurality of fixing holes 7 are opened on the outer wall of the upper end of the workbench 1 .

[0043] The height of the workbench 1 is increased by the support legs 8, so that the staff can do hard work more conveniently, and a plurality of fixing holes 7 can be provided to adjust the positions of the sliding sleeve 10, the rotating column 17 and the threaded sleeve 16 as needed to adapt to the lifting operation of drones of different sizes.

[0044] The implementation principle of this embodiment is: when replacing the tail of the drone, the head of the drone can be placed on the head bracket 2, and the wing bracket 6 can be adjusted to a position and then moved to the lower side of the drone wing for lifting, and the tail can be lifted on the bottom plate 15 buffer pad 12, and then the tail pressure plate 3 is fixed downward and between the bottom plate 15 to clamp the tail, and then the drone tail can be removed by tools for replacement, and when disassembling the drone tail, the removed screws, bolts, and small parts can be placed in the storage slot a20 in the storage bucket 9 for temporary storage, and the disassembly tools can be taken out from the storage slot b22 or the disassembly tools and larger usable components removed from the tail can be stored.

[0045] Finally, it should be noted that the above is only a preferred embodiment of the present invention and is not intended to limit the present invention. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art can still modify the technical solutions described in the aforementioned embodiments or 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 invention should be included in the protection scope of the present invention.

Claims

1. A tail wing modification tool for an unmanned aerial vehicle, comprising a workbench (1) and a nose bracket (2) mounted on the front side of the workbench (1); A wing bracket (6) is arranged on the right side of the nose bracket (2) to support the wings of the UAV; A bottom plate (15) is provided on the rear side of the wing bracket (6); A tail pressure plate (3) is arranged on the upper side of the base plate (15) to fix the position of the tail wing of the UAV, and a buffer pad (12) is fixedly connected to the upper outer wall of the base plate (15) and the lower outer wall of the tail pressure plate (3) to fit the shape of the wing; Features: The upper outer wall of the workbench (1) is provided with a storage bucket (9), the front end outer wall of the storage bucket (9) is provided with a storage groove a (20) near the lower side for storing parts and small accessories of the drone, and the front end outer wall of the storage bucket (9) is provided with a storage groove b (22) located above the storage groove a (20) for storing disassembly tools and parts of the drone.

2. The UAV tail wing modification tooling according to claim 1 is characterized by: The storage tank a (20) is fixedly connected to a partition a (19) inside, and the storage tank b (22) is fixedly connected to a partition b (21) inside.

3. The UAV tail wing modification tooling according to claim 1 is characterized by: The right end outer wall of the storage bucket (9) is fixedly connected to a limiting plate (18), and the right end outer wall of the storage bucket (9) is fixedly connected to a magnetic plate (27) for magnetic adsorption and fixation with the workbench (1).

4. The UAV tail wing modification tooling according to claim 1 is characterized by: The outer wall of the upper end of the storage bucket (9) is equidistantly and fixedly connected with a plurality of jackets (26), and the interiors of the plurality of jackets (26) are all fixedly connected with sponge blocks (25).

5. The UAV tail wing modification tooling according to claim 4 is characterized by: A guide slit (24) is provided inside the outer wall of the upper end of the sponge block (25), and a through opening (23) is provided inside the sponge block (25) to limit the position of the tail wing replacement line.

6. The UAV tail wing modification tooling according to claim 1 is characterized by: The lower outer wall of the machine head bracket (2) is fixedly connected to a slide rod (11), and a slide sleeve (10) is provided between the lower outer wall of the slide rod (11) and the workbench (1).

7. The UAV tail wing modification tooling according to claim 1 is characterized by: The lower end outer wall of the wing bracket (6) is transmission-connected with a movable rod b (5), and the left end outer wall of the movable rod b (5) is transmission-connected with a movable rod a (4).

8. The UAV tail wing modification tooling according to claim 7 is characterized by: The lower end outer wall of the movable rod a (4) is drivingly connected to a rotating column (17) to adjust the lateral tilt angle of the movable rod a (4), and a threaded sleeve (16) is fixedly connected between the lower end outer wall of the base plate (15) and the workbench (1).

9. The UAV tail wing modification tooling according to claim 7, characterized in that: A threaded rod (14) is arranged between the lower outer wall of the tail pressure plate (3) and the threaded sleeve (16) to adjust the height of the tail pressure plate (3), and an adjusting screw (13) is transmission-connected to the upper outer wall of the tail pressure plate (3) to adjust the upward and downward movement of the threaded rod (14) inside the threaded sleeve (16).

10. The UAV tail wing modification tooling according to claim 1, characterized in that: A plurality of supporting legs (8) are fixedly connected to the outer wall at the lower end of the workbench (1), and a plurality of fixing holes (7) are provided on the outer wall at the upper end of the workbench (1).

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