An unmanned aerial vehicle washing device

Abstract

The utility model relates to low altitude cleaning technical field especially unmanned aerial vehicle cleaning device, including unmanned aerial vehicle body and the suspension assembly that hangs in the lower side of unmanned aerial vehicle body, the lower side of unmanned aerial vehicle body is provided with the adjusting assembly for changing the position of suspension assembly, the lower side of suspension assembly is provided with cleaning assembly and is used for fixing the fixing assembly of cleaning assembly the utility model realizes the flexible adjustment of water gun position through adjusting assembly. In the cleaning operation process, can through the replacement or removal suspension assembly, conveniently adjust water gun working position to adapt to a variety of application scenarios, effectively promote work efficiency.

Description

Technical Field

[0001] This utility model relates to the field of low-altitude cleaning technology, and in particular to a drone cleaning device. Background Technology

[0002] With the increasing number of high-rise buildings, the cleaning of glass curtain walls has become a more prominent challenge. Traditional manual cleaning is not only inefficient but also poses safety hazards due to working at heights. In recent years, drone technology has begun to be applied to the field of high-altitude cleaning. By being equipped with high-pressure water guns, drones can automate the cleaning of the exterior walls of high-rise buildings, significantly improving operational efficiency and safety.

[0003] Most existing high-pressure water guns use a fixed connection design with drones, which prevents flexible adjustment of the water gun angle. However, modern buildings often have irregular shapes and structures. If the water gun position cannot be adjusted accordingly, it will be difficult to thoroughly clean these special areas, thus reducing overall cleaning efficiency. Utility Model Content

[0004] The purpose of this invention is to address the aforementioned shortcomings in the existing technology by proposing a drone cleaning device.

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

[0006] Design a drone cleaning device, including a drone body and a suspension assembly suspended on the lower side of the drone body. The lower side of the drone body is provided with an adjustment component for changing the position of the suspension assembly. The lower side of the suspension assembly is provided with a cleaning component and a fixing component for fixing the cleaning component.

[0007] Furthermore, the adjustment assembly includes two upright plates fixedly connected to the lower side of the UAV body. A screw and a guide rod are respectively provided between the two ends of the two upright plates. The screw is rotatably connected between the two upright plates, and the guide rod is fixedly connected between the two upright plates.

[0008] Furthermore, the suspension assembly includes a connecting plate, both ends of which are formed with sleeves, one of which is threadedly connected to the screw, and the other sleeve is slidably connected to the guide rod.

[0009] Furthermore, the cleaning assembly includes a rod, with a nozzle and a water pipe respectively provided at both ends of the rod, and the rod, water pipe and nozzle are connected by a water circuit.

[0010] Furthermore, the fixing component includes a connecting ring fixedly connected to one end of the rod, the outer side of the connecting ring is formed with a receiving groove, and the lower end of the connecting plate is formed with two stop plates, the connecting ring being slidably connected between the two stop plates through the receiving groove.

[0011] Furthermore, a U-shaped seat is fixedly connected to one side of the stop plate, and a connecting rod is rotatably connected between the two ends of the U-shaped seat. A compression spring is fixedly connected between one end of the connecting rod and the stop plate, and a slot is formed at the other end of the connecting rod. A slot hole is formed on the receiving slot, and a positioning rod is slidably connected in the slot hole. The positioning rod passes through the stop plate, and a rotating shaft is fixedly connected to one end of the positioning rod. The rotating shaft is slidably connected to the slot.

[0012] Furthermore, the balancing component includes a hook fixedly connected to the tail of the drone body, one end of the hook is provided with a spring insert rod, a counterweight is suspended on the hook, and the spring insert rod abuts against the counterweight.

[0013] The drone cleaning device proposed in this invention has the following advantages: It allows for flexible adjustment of the water gun position through an adjustable component. During cleaning operations, the water gun's working position can be easily adjusted by replacing or moving the suspension component, thus adapting to various application scenarios and effectively improving work efficiency. Attached Figure Description

[0014] Figure 1 This is a perspective view of the present utility model;

[0015] Figure 2 This is a partial structural schematic diagram of the present invention;

[0016] Figure 3 This is a cross-sectional view of the fixing component structure of this utility model;

[0017] Figure 4 For the present utility model Figure 2 A schematic diagram of the area structure;

[0018] Figure 5 This is a schematic diagram of the balancing component structure of this utility model.

[0019] In the diagram: 1. UAV body; 2. Suspension assembly; 21. Connecting plate; 22. Sleeve; 3. Adjustment assembly; 31. Vertical plate; 32. Screw; 33. Guide rod; 4. Cleaning assembly; 41. Rod; 42. Nozzle; 43. Water pipe; 5. Fixing assembly; 51. Connecting ring; 52. Receiving groove; 53. Stop plate; 54. U-shaped seat; 55. Connecting rod; 56. Compression spring; 57. Slot; 58. Hole; 59. Positioning rod; 50. Rotating shaft; 6. Balancing assembly; 61. Hook; 62. Spring insert rod; 63. Counterweight. Detailed Implementation

[0020] 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.

[0021] Reference Figure 1-5 A drone cleaning device includes a drone body 1 and a suspension assembly 2 suspended on the lower side of the drone body 1. An adjustment assembly 3 for changing the position of the suspension assembly 2 is provided on the lower side of the drone body 1. A cleaning assembly 4 and a fixing assembly 5 for fixing the cleaning assembly 4 are provided on the lower side of the suspension assembly 2.

[0022] It should be noted that the adjustment component 3 includes two upright plates 31 fixedly connected to the lower side of the UAV body 1. A screw 32 and a guide rod 33 are respectively provided between the two ends of the two upright plates 31. The screw 32 is rotatably connected between the two upright plates 31, and the guide rod 33 is fixedly connected between the two upright plates 31.

[0023] In this embodiment, the suspension assembly 2 includes a connecting plate 21, and sleeves 22 are formed at both ends of the connecting plate 21. One sleeve 22 is threadedly connected to the screw 32, and the other sleeve 22 is slidably connected to the guide rod 33. By rotating the screw 32, the connecting plate 21 is moved, thereby conveniently adjusting the position of the connecting plate 21.

[0024] Furthermore, the cleaning assembly 4 includes a rod 41, with a nozzle 42 and a water pipe 43 respectively installed at both ends of the rod 41. The rod 41, water pipe 43, and nozzle 42 are connected by a water circuit. It should be noted that a booster pump is also connected to the lower side of the water pipe 43. The rod 41 is a hollow rod, and the other end of the booster pump is connected to a water tank. The booster pump transports water from the water tank to the water pipe 43, and then through the water pipe 43 to the rod 41, where it is sprayed out by the nozzle 42. This is existing technology and will not be described in detail here.

[0025] The fixing component 5 includes a connecting ring 51 fixedly connected to one end of the rod 41. The outer side of the connecting ring 51 is formed with a receiving groove 52. The lower end of the connecting plate 21 is formed with two stop plates 53. The connecting ring 51 is slidably connected between the two stop plates 53 through the receiving groove 52. The stop plates 53 on both sides cooperate with the receiving groove 52 to position the connecting ring 51 at that location.

[0026] Based on the above embodiment, a U-shaped seat 54 is fixedly connected to one side of the stop plate 53, and a connecting rod 55 is rotatably connected between the two ends of the U-shaped seat 54. A compression spring 56 is fixedly connected between one end of the connecting rod 55 and the stop plate 53, and a slot 57 is formed at the other end of the connecting rod 55. A slot hole 58 is formed on the receiving groove 52, and a positioning rod 59 is slidably connected in the slot hole 58. The positioning rod 59 passes through the stop plate 53, and a rotating shaft 50 is fixedly connected to one end of the positioning rod 59. The rotating shaft 50 is slidably connected to the slot 57. By inserting the positioning rod 59 into the slot hole 58, the connecting ring 51 is fixed to the lower side of the connecting plate 21. When it needs to be removed, simply press the connecting rod 55 to move the positioning rod 59 out of the slot hole 58, thereby removing the connecting ring 51.

[0027] Furthermore, the balancing component 6 includes a hook 61 fixedly connected to the tail of the drone body 1. A spring rod 62 is inserted through one end of the hook 61, and a counterweight 63 is suspended on the hook 61. The spring rod 62 abuts against the counterweight 63. The counterweight 63 includes several different weights. When the position of the cleaning component 4 moves, the drone body can be balanced by replacing the counterweight 63 to prevent the weight on one side from being too high and causing the drone to crash.

[0028] Working method: When working, fix the two ends of the water pipe 43 to the booster pump and the rod 41 respectively, then fix the nozzle 42 to the rod 41, and then connect the rod 41 to the suspension assembly 2 through the fixing component 5. Then rotate the screw 32 to move the connecting plate 21 to the appropriate position, and suspend a counterweight 63 of appropriate weight at the tail. After the adjustment is completed, the drone body 1 can take off. After flying to the appropriate position, turn on the booster pump to supply water.

[0029] 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 cleaning device, comprising a drone body (1) and a suspension assembly (2) suspended below the drone body (1), characterized in that: The lower side of the drone body (1) is provided with an adjustment component (3) for changing the position of the suspension component (2), the lower side of the suspension component (2) is provided with a cleaning component (4) and a fixing component (5) for fixing the cleaning component (4), and the tail of the drone body (1) is provided with a balancing component (6).

2. The drone cleaning device according to claim 1, characterized in that: The adjustment assembly (3) includes two upright plates (31) fixedly connected to the lower side of the UAV body (1). A screw (32) and a guide rod (33) are respectively provided between the two ends of the two upright plates (31). The screw (32) is rotatably connected between the two upright plates (31), and the guide rod (33) is fixedly connected between the two upright plates (31).

3. The drone cleaning device according to claim 2, characterized in that: The suspension assembly (2) includes a connecting plate (21), both ends of which are formed with sleeves (22), one of the sleeves (22) being threadedly connected to the screw (32), and the other sleeve (22) being slidably connected to the guide rod (33).

4. The drone cleaning device according to claim 3, characterized in that: The cleaning assembly (4) includes a rod (41), with a nozzle (42) and a water pipe (43) respectively provided at both ends of the rod (41), and the rod (41), the water pipe (43) and the nozzle (42) are connected by a water circuit.

5. The drone cleaning device according to claim 4, characterized in that: The fixing component (5) includes a connecting ring (51) fixedly connected to one end of the rod (41). The outer side of the connecting ring (51) is formed with a receiving groove (52). The lower end of the connecting plate (21) is formed with two stop plates (53). The connecting ring (51) is slidably connected between the two stop plates (53) through the receiving groove (52).

6. The drone cleaning device according to claim 5, characterized in that: A U-shaped seat (54) is fixedly connected to one side of the stop plate (53). A connecting rod (55) is rotatably connected between the two ends of the U-shaped seat (54). A compression spring (56) is fixedly connected between one end of the connecting rod (55) and the stop plate (53). A slot (57) is opened at the other end of the connecting rod (55). A slot hole (58) is opened on the receiving groove (52). A positioning rod (59) is slidably connected in the slot hole (58). The positioning rod (59) passes through the stop plate (53). A rotating shaft (50) is fixedly connected to one end of the positioning rod (59). The rotating shaft (50) is slidably connected to the slot (57).

7. The drone cleaning device according to claim 1, characterized in that: The balancing component (6) includes a hook (61) fixedly connected to the tail of the UAV body (1). A spring rod (62) is inserted through one end of the hook (61). A counterweight (63) is suspended on the hook (61). The spring rod (62) abuts against the counterweight (63).

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