Unmanned aerial vehicle wing machining device

Abstract

The utility model discloses an unmanned aerial vehicle wing machining device, and relates to the technical field of unmanned aerial vehicle wing machining devices, the unmanned aerial vehicle wing machining device comprises a carrier plate, the top of the carrier plate is fixedly connected with a machining box, and the machining box is arranged through a second threaded rod, a placing table, a fixing plate, an electric telescopic rod, a third motor, a rotating column, a moving block, a sliding block, a first electrode block, a second electrode block and a fourth motor. According to the unmanned aerial vehicle wing machining device, wings are turned over mechanically, so that the situation that the wings need to be turned over manually, and the operation is too tedious is avoided; the unmanned aerial vehicle wing processing device is provided with a charging barrel, a first motor, a first gear, a stirring shaft, a first bearing, a first connecting rod, a scraper blade, a second connecting rod, a second gear, a first transmission shaft, a second transmission shaft, a second bearing, a fixed column, a first transmission gear, a second transmission gear and a fixed gear. And the situation that the coating possibly precipitates after standing for a long time is avoided.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle wing processing devices, in particular to a unmanned aerial vehicle wing processing device. Background Art

[0002] Unmanned aerial vehicle, abbreviated as "UAV" in English, is an unmanned aircraft controlled by radio remote control equipment and self-contained program control device, or operated completely or intermittently autonomously by an on-board computer.

[0003] At present, drones have been widely used, and drones mainly rely on their wings to generate lift to take off. In order to ensure the long-term use of the wings, the wings need to be sprayed to prevent them from being damaged by moisture and rust, etc. This requires the use of a spraying device.

[0004] At present, the UAV wing processing devices in the prior art are usually simple in structure and single in function, and cannot spray the wings comprehensively. After spraying one side of the wing is completed, the wing needs to be flipped manually, which is too cumbersome. In addition, the paint may precipitate after being left standing for a long time. Due to the precipitation of the paint, the uniformity of the spraying will be affected. There is a problem that the paint may precipitate after being left standing for a long time. Utility Model Content

[0005] 1. Technical issues to be solved

[0006] In view of the deficiencies in the prior art, the utility model provides a UAV wing processing device, which solves the problems raised in the above-mentioned background technology.

[0007] (II) Technical solution

[0008] To achieve the above purpose, the utility model is implemented through the following technical solutions: comprising a carrier plate, the top of the carrier plate is fixedly connected with a processing box, the inner wall of the processing box is movably connected with a glass door, the inner wall of the processing box is fixedly connected with a placing table, the top of the carrier plate is fixedly connected with a barrel, the top of the barrel is fixedly connected with a first motor, the inner wall of the barrel is fixedly connected with a second tube, one end of the second tube is fixedly connected with a material pump, the outer side of the material pump is fixedly connected with the processing box, one end of the material pump is fixedly connected with the first tube, and one end of the first tube is fixedly connected with a nozzle;

[0009] The inner wall of the processing box is fixedly connected with a fourth motor, the output shaft of the fourth motor is fixedly connected with a second threaded rod, the outer side of the second threaded rod is threadedly connected with a moving block, the inner wall of the moving block is fixedly connected with a third motor, the output shaft of the third motor is fixedly connected with a rotating column, the inner wall of the rotating column is fixedly connected with an electric telescopic rod, and one end of the electric telescopic rod is fixedly connected with a fixing plate;

[0010] The output shaft of the first motor is fixedly connected to a fixed gear, the outer side of the fixed gear is meshedly connected to the second transmission gear, the bottom of the second transmission gear is fixedly connected to the first transmission shaft, the outer side of the first transmission shaft is fixedly connected to the first connecting rod, the inner wall of the first connecting rod is fixedly connected to the first bearing, the inner wall of the first bearing is fixedly connected to the stirring shaft, one end of the stirring shaft is fixedly connected to the first gear, the outer side of the first gear is meshedly connected to the second gear, and the top of the second gear is fixedly connected to the barrel.

[0011] Optionally, the outer side of the fixed gear is meshedly connected with a first transmission gear, the bottom of the first transmission gear is fixedly connected with a second transmission shaft, the outer side of the second transmission shaft is connected with a second connecting rod, and one end of the second connecting rod is fixedly connected with a scraper.

[0012] Optionally, a fixing column is fixedly connected to the top of the first transmission gear, a second bearing is fixedly connected to the outer side of the fixing column, and a barrel is fixedly connected to the outer side of the second bearing.

[0013] Optionally, one end of the rotating column is fixedly connected to a slider, the outer side of the slider is slidably connected to a moving block, the inner wall of the moving block is fixedly connected to a second electrode block, and the inner wall of the slider is fixedly connected to a first electrode block.

[0014] Optionally, a second motor is fixedly connected to the inner wall of the processing box, an output shaft of the second motor is fixedly connected to a first threaded rod, an outer side of the first threaded rod is threadedly connected to a nozzle, a limiting rod is slidably connected to the inner wall of the nozzle, and one end of the limiting rod is fixedly connected to the processing box.

[0015] Optionally, there are two first gears, and the first gears are distributed on both sides of the second gear.

[0016] (III) Beneficial effects

[0017] The utility model provides a UAV wing processing device, which has the following beneficial effects:

[0018] 1. The UAV wing processing device is provided with a second threaded rod, a placement table, a fixed plate, an electric telescopic rod, a third motor, a rotating column, a moving block, a slider, a first electrode block, a second electrode block, and a fourth motor. The UAV wing processing device has the function of mechanically flipping the wing, avoiding the need for manual flipping of the wing, which is too cumbersome.

[0019] 2. The UAV wing processing device is arranged through a barrel, a first motor, a first gear, a stirring shaft, a first bearing, a first connecting rod, a scraper, a second connecting rod, a second gear, a first transmission shaft, a second transmission shaft, a second bearing, a fixed column, a first transmission gear, a second transmission gear, and a fixed gear. A UAV wing processing device has the function of preventing the precipitation of the paint and avoiding the possible precipitation of the paint after standing still for a long time. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 This is a schematic diagram of the positive shaft side structure of the utility model;

[0021] Figure 2 This is a schematic diagram of the front view structure of the utility model;

[0022] Figure 3 This is a schematic diagram of the front cross-sectional structure of the utility model;

[0023] Figure 4 This is a schematic diagram of the cross-sectional structure of the rotating column of the utility model;

[0024] Figure 5 For this utility model Figure 3 Schematic diagram of the enlarged structure at A of the species;

[0025] Figure 6 For this utility model Figure 3 Schematic diagram of the enlarged structure of B;

[0026] Figure 7 It is a schematic diagram of the cross-sectional structure of the first transmission shaft of the utility model.

[0027] In the figure: 1, processing box; 2, glass door; 3, first tube; 4, barrel; 5, first motor; 6, carrier plate; 7, material pump; 8, second tube; 9, second motor; 10, limiting rod; 11, nozzle; 12, first threaded rod; 13, first gear; 14, stirring shaft; 15, first bearing; 16, first connecting rod; 17, scraper; 18, second connecting rod; 19, second threaded rod; 20, placing table; 21, fixed plate; 22, electric telescopic rod; 23, third motor; 24, second gear; 25, first transmission shaft; 26, second transmission shaft; 27, rotating column; 28, moving block; 29, slider; 30, first electrode block; 31, second bearing; 32, fixed column; 33, first transmission gear; 34, second transmission gear; 35, fixed gear; 36, second electrode block; 37, fourth motor. DETAILED DESCRIPTION

[0028] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, rather than all of the embodiments.

[0029] Example 1

[0030] See also Figures 1 to 7 The utility model provides a technical solution: a UAV wing processing device, comprising a carrier plate 6, a processing box 1 is fixedly connected to the top of the carrier plate 6, a glass door 2 is movably connected to the inner wall of the processing box 1, a placing table 20 is fixedly connected to the inner wall of the processing box 1, a barrel 4 is fixedly connected to the top of the carrier plate 6, a first motor 5 is fixedly connected to the top of the barrel 4, a second tube 8 is fixedly connected to the inner wall of the barrel 4, a material pump 7 is fixedly connected to one end of the second tube 8, the processing box 1 is fixedly connected to the outer side of the material pump 7, a second motor 9 is fixedly connected to the inner wall of the processing box 1, a first threaded rod 12 is fixedly connected to the output shaft of the second motor 9, a nozzle 11 is threadedly connected to the outer side of the first threaded rod 12, a limiting rod 10 is slidably connected to the inner wall of the nozzle 11, one end of the limiting rod 10 is fixedly connected to the processing box 1, one end of the material pump 7 is fixedly connected to the first tube 3, and one end of the first tube 3 is fixedly connected to the nozzle 11;

[0031] The inner wall of the processing box 1 is fixedly connected with a fourth motor 37, the output shaft of the fourth motor 37 is fixedly connected with a second threaded rod 19, the outer side of the second threaded rod 19 is threadedly connected with a moving block 28, the inner wall of the moving block 28 is fixedly connected with a third motor 23, the output shaft of the third motor 23 is fixedly connected with a rotating column 27, one end of the rotating column 27 is fixedly connected with a slider 29, the outer side of the slider 29 is slidably connected with the moving block 28, the inner wall of the moving block 28 is fixedly connected with a second electrode block 36, and the inner wall of the slider 29 is fixedly connected with a first The electrode block 30, the inner wall of the rotating column 27 is fixedly connected with the electric telescopic rod 22, one end of the electric telescopic rod 22 is fixedly connected with the fixed plate 21, through the second threaded rod 19, the placement table 20, the fixed plate 21, the electric telescopic rod 22, the third motor 23, the rotating column 27, the moving block 28, the slider 29, the first electrode block 30, the second electrode block 36, and the fourth motor 37, a UAV wing processing device is capable of mechanically flipping the wing, avoiding the need for manual flipping of the wing, which is too cumbersome.

[0032] When in use, the wing is placed on the placement table 20, the electric telescopic rod 22 is started, the electric telescopic rod 22 clamps the wing through the fixed plate 21, and then the fourth motor 37 is started. The fourth motor 37 drives the second threaded rod 19 to move the moving block 28 upward. After the moving block 28 moves to a suitable position, the fourth motor 37 stops working, the material pump 7 is started, and the material pump 7 extracts the paint from the barrel 4 through the second tube 8, and then supplies it to the nozzle 11 from the first tube 3. The second motor 9 is started, and the second motor 9 drives the first threaded rod 12 to move the nozzle 11 so that the paint is sprayed from the nozzle 11 to spray the wing. When one side of the wing is sprayed, the material pump 7 stops working, and the third motor 23 is started. The third motor 23 drives the rotating column 27. When the first electrode block 30 in the slider 29 contacts the second electrode block 36, the third motor 23 no longer works, so the wing is turned over, and the material pump 7 and the second motor 9 are started again to spray the wing.

[0033] Example 2

[0034] See also Figures 1 to 7 The utility model provides a technical solution: a UAV wing processing device, including a carrier plate 6, a processing box 1 is fixedly connected to the top of the carrier plate 6, a glass door 2 is movably connected to the inner wall of the processing box 1, a placing table 20 is fixedly connected to the inner wall of the processing box 1, a barrel 4 is fixedly connected to the top of the carrier plate 6, a first motor 5 is fixedly connected to the top of the barrel 4, a second tube 8 is fixedly connected to the inner wall of the barrel 4, one end of the second tube 8 is fixedly connected to a material pump 7, the outer side of the material pump 7 is fixedly connected to the processing box 1, one end of the material pump 7 is fixedly connected to the first tube 3, and one end of the first tube 3 is fixedly connected to a nozzle 11;

[0035] The output shaft of the first motor 5 is fixedly connected to a fixed gear 35, the outer side of the fixed gear 35 is meshedly connected to the first transmission gear 33, the bottom of the first transmission gear 33 is fixedly connected to the second transmission shaft 26, the outer side of the second transmission shaft 26 is connected to the second connecting rod 18, one end of the second connecting rod 18 is fixedly connected to the scraper 17, the top of the first transmission gear 33 is fixedly connected to a fixed column 32, the outer side of the fixed column 32 is fixedly connected to the second bearing 31, the outer side of the second bearing 31 is fixedly connected to the barrel 4, the outer side of the fixed gear 35 is meshedly connected to the second transmission gear 34, the bottom of the second transmission gear 34 is fixedly connected to the first transmission shaft 25, the outer side of the first transmission shaft 25 is fixedly connected to the first connecting rod 16, the inner wall of the first connecting rod 16 is fixedly connected to the first bearing 15, and the first bearing 1 5 is fixedly connected to the inner wall of the stirring shaft 14, one end of the stirring shaft 14 is fixedly connected to the first gear 13, there are two first gears 13, the first gears 13 are distributed on both sides of the second gear 24, the outer side of the first gear 13 is meshedly connected to the second gear 24, the top of the second gear 24 is fixedly connected to the barrel 4, through the barrel 4, the first motor 5, the first gear 13, the stirring shaft 14, the first bearing 15, the first connecting rod 16, the scraper 17, the second connecting rod 18, the second gear 24, the first transmission shaft 25, the second transmission shaft 26, the second bearing 31, the fixed column 32, the first transmission gear 33, the second transmission gear 34, and the fixed gear 35, a UAV wing processing device has the function of preventing the precipitation of the paint and avoiding the possible precipitation of the paint after standing for a long time.

[0036] When in use, start the first motor 5, the first motor 5 drives the fixed gear 35, the fixed gear 35 drives the first transmission gear 33 and the second transmission gear 34, the second transmission gear 34 drives the first transmission shaft 25, the first transmission shaft 25 drives the stirring shaft 14 through the first connecting rod 16, the stirring shaft 14 rotates through the engagement of the first gear 13 and the second gear 24, the coating is stirred by the rotation of the stirring shaft 14 to prevent the coating from settling, and the first transmission gear 33 drives the second transmission shaft 26, the second transmission shaft 26 drives the scraper 17 through the second connecting rod 18 to clean the inner wall of the barrel 4 to prevent the coating from adhering to the inner wall of the barrel 4.

[0037] The above description is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes within the technical scope disclosed by the present invention according to the technical scheme and the utility model concept of the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A drone wing processing device, comprising a carrier plate (6), characterized in that: The top of the carrier plate (6) is fixedly connected to a processing box (1), the inner wall of the processing box (1) is movably connected to a glass door (2), the inner wall of the processing box (1) is fixedly connected to a placing table (20), the top of the carrier plate (6) is fixedly connected to a barrel (4), the top of the barrel (4) is fixedly connected to a first motor (5), the inner wall of the barrel (4) is fixedly connected to a second tube (8), one end of the second tube (8) is fixedly connected to a material pump (7), the outer side of the material pump (7) is fixedly connected to the processing box (1), one end of the material pump (7) is fixedly connected to a first tube (3), and one end of the first tube (3) is fixedly connected to a nozzle (11); The inner wall of the processing box (1) is fixedly connected to a fourth motor (37), the output shaft of the fourth motor (37) is fixedly connected to a second threaded rod (19), the outer side of the second threaded rod (19) is threadedly connected to a moving block (28), the inner wall of the moving block (28) is fixedly connected to a third motor (23), the output shaft of the third motor (23) is fixedly connected to a rotating column (27), the inner wall of the rotating column (27) is fixedly connected to an electric telescopic rod (22), and one end of the electric telescopic rod (22) is fixedly connected to a fixing plate (21); The output shaft of the first motor (5) is fixedly connected to a fixed gear (35), the outer side of the fixed gear (35) is meshedly connected to a second transmission gear (34), the bottom of the second transmission gear (34) is fixedly connected to a first transmission shaft (25), the outer side of the first transmission shaft (25) is fixedly connected to a first connecting rod (16), the inner wall of the first connecting rod (16) is fixedly connected to a first bearing (15), the inner wall of the first bearing (15) is fixedly connected to a stirring shaft (14), one end of the stirring shaft (14) is fixedly connected to a first gear (13), the outer side of the first gear (13) is meshedly connected to a second gear (24), and the top of the second gear (24) is fixedly connected to a barrel (4).

2. The UAV wing processing device according to claim 1, characterized in that: The outer side of the fixed gear (35) is meshedly connected with a first transmission gear (33), the bottom of the first transmission gear (33) is fixedly connected with a second transmission shaft (26), the outer side of the second transmission shaft (26) is connected with a second connecting rod (18), and one end of the second connecting rod (18) is fixedly connected with a scraper (17).

3. The UAV wing processing device according to claim 2, characterized in that: A fixing column (32) is fixedly connected to the top of the first transmission gear (33), a second bearing (31) is fixedly connected to the outer side of the fixing column (32), and a barrel (4) is fixedly connected to the outer side of the second bearing (31).

4. The UAV wing processing device according to claim 1, characterized in that: One end of the rotating column (27) is fixedly connected to a slider (29), the outer side of the slider (29) is slidably connected to a moving block (28), the inner wall of the moving block (28) is fixedly connected to a second electrode block (36), and the inner wall of the slider (29) is fixedly connected to a first electrode block (30).

5. The UAV wing processing device according to claim 1, characterized in that: A second motor (9) is fixedly connected to the inner wall of the processing box (1); an output shaft of the second motor (9) is fixedly connected to a first threaded rod (12); an outer side of the first threaded rod (12) is threadedly connected to a nozzle (11); a limiting rod (10) is slidably connected to the inner wall of the nozzle (11); one end of the limiting rod (10) is fixedly connected to the processing box (1).

6. The UAV wing processing device according to claim 1, characterized in that: There are two first gears (13), and the first gears (13) are distributed on both sides of the second gear (24).

Images