Airplane part surface paint coating device

Abstract

The utility model discloses an aircraft part surface paint coating device which comprises a frame body, a sliding opening is formed in the upper surface of the frame body, a sliding block is connected to the inner wall of the sliding opening in a sliding mode, a bearing seat is fixedly connected to the upper surface of the frame body, and a fixing plate is fixedly connected to the right side face of the frame body. The upper surface of the fixing plate is fixedly connected with a motor. According to the device, the motor, the threaded rod, the threaded cylinder, the bearing seat, a sliding opening, a sliding block, a spray head, a connecting pipe and a sliding cylinder are arranged, through cooperation of the spray head and the connecting pipe, the spray head conveniently sprays aircraft parts, then according to cooperation of the motor, the threaded rod and the threaded cylinder, the threaded cylinder conveniently moves on the surface of the threaded rod, and meanwhile the sliding block is driven to slide in the sliding opening; and at the moment, through cooperation of a sliding block and a spray head, uniform spraying of the aircraft parts is facilitated, through cooperation of an electric push rod and a lifting plate, the aircraft parts are conveniently driven to get close to the spray head, and the spraying effect is improved.

Description

Technical Field

[0001] The utility model relates to the field of coating, in particular to a device for coating paint on the surface of aircraft parts. Background Art

[0002] Coating is an important link in the modern product manufacturing process. The quality of rust-proof and corrosion-proof coating is one of the important aspects of the overall quality of the product. The quality of product appearance not only reflects the product's protective and decorative performance, but is also an important factor in the value of the product. Coating refers to the process of covering the surface of the object to be coated with a certain thickness of material by applying coatings and paints. Coating generally includes primer, mid-coat and topcoat. The main purpose of coating is to protect the surface of the object to be coated, beautify the appearance and improve the performance. Coating is widely used in various fields, such as automobiles, aviation, electronics, construction and furniture industries. Among them, automotive coating is one of the most widely used coating fields. Automotive coating needs to meet multiple requirements such as mechanical strength, weather resistance and wear resistance, and the requirements for coatings are extremely strict.

[0003] At present, when processing aircraft parts, a coating device is needed to spray its surface. The current coating device has a simple structure and the spraying position is generally fixed, which will affect the uniformity of the spraying and make the appearance of the parts inconsistent. For this reason, we propose a surface paint coating device for aircraft parts to solve the above problems. Utility Model Content

[0004] The utility model aims to provide a device for coating the surface of aircraft parts with paint, so as to solve the problems raised in the above-mentioned background technology.

[0005] In order to achieve the above purpose, the utility model provides the following technical solutions:

[0006] The cam is connected with the bearing seat of the frame body, and the upper end of the cam is connected with the bearing seat of the frame body, the upper end of the cam is connected with the bearing seat of the frame body, the upper end of the cam is connected with the bearing seat of the frame body, the upper end of the cam is connected with the bearing seat of the frame body, the upper end of the cam is connected with the bearing seat of the frame body, the upper end of the cam is connected with the bearing seat of the frame body, the upper end of the cam is connected with the bearing seat of the frame body, the upper end of the cam is connected with the bearing seat of the frame body, the upper end of the cam is connected with the bearing seat of the frame body, the upper end of the cam is connected with the bearing seat of the frame body, the upper end of the cam is connected with the bearing seat of the frame body, the upper end of the cam is connected with the bearing seat of the frame body, the upper end of the cam is connected with the bearing seat of the frame body

[0007] In a further embodiment, the back of the frame is fixedly connected to a box body, the inner wall of the box body is fixedly connected to a heating wire, the back of the box body is fixedly embedded with a group of fans, and the front of the box body is fixedly embedded with a group of ventilation pipes.

[0008] In a further embodiment, both left and right side surfaces of the frame are fixedly connected with mounting plates, and the upper surface of each mounting plate is provided with two mounting holes.

[0009] In a further embodiment, a connecting plate is fixedly connected to the right side surface of the frame, and a storage battery is fixedly connected to the upper surface of the connecting plate.

[0010] In a further embodiment, a support plate is fixedly connected to the right side surface of the frame, and a side surface of the support plate away from the frame is fixedly connected to the bottom surface of the fixing plate.

[0011] In a further embodiment, a warning sign is fixedly connected to the right side of the frame, and a storage box is fixedly connected to the upper surface of the frame.

[0012] Compared with the prior art, the beneficial effects of the utility model are:

[0013] The device is provided with a motor, a threaded rod, a threaded barrel, a bearing seat, a sliding mouth, a slider, a nozzle, a connecting pipe and a sliding barrel. The nozzle and the connecting pipe cooperate to facilitate the nozzle to spray the aircraft parts. Then, according to the cooperation of the motor, the threaded rod and the threaded barrel, the threaded barrel moves on the surface of the threaded rod and drives the slider to slide inside the sliding mouth. At this time, the cooperation of the slider and the nozzle facilitates the uniform spraying of the aircraft parts. The cooperation of the electric push rod and the lifting plate facilitates the aircraft parts to be driven close to the nozzle, which is conducive to improving the spraying effect. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 It is a schematic diagram of the overall three-dimensional structure of the paint coating device on the surface of aircraft parts;

[0015] Figure 2 It is a three-dimensional structural schematic diagram of the side view of the frame of the aircraft parts surface paint coating device;

[0016] Figure 3 It is a three-dimensional structural schematic diagram of a top view of a frame of a paint coating device for the surface of aircraft parts;

[0017] Figure 4 It is a cross-sectional view of the top view of the box of the aircraft parts surface paint coating device.

[0018] In the figure: 1. Mounting hole; 2. Electric push rod; 3. Lifting plate; 4. Frame; 5. Mounting plate; 6. Connecting plate; 7. Battery; 8. Warning sign; 9. Support plate; 10. Fixing plate; 11. Motor; 12. Slide; 13. Threaded rod; 14. Nozzle; 15. Slider; 16. Bearing seat; 17. Connecting pipe; 18. Slide cylinder; 19. Ventilation pipe; 20. Threaded cylinder; 21. Storage box; 22. Box; 23. Heating wire; 24. Fan. DETAILED DESCRIPTION

[0019] 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.

[0020] See also Figure 1-4 In the utility model, a device for coating the surface of aircraft parts with paint comprises a frame 4, a sliding opening 12 is provided on the upper surface of the frame 4, a slider 15 is slidably connected to the inner wall of the sliding opening 12, a bearing seat 16 is fixedly connected to the upper surface of the frame 4, a fixing plate 10 is fixedly connected to the right side of the frame 4, a motor 11 is fixedly connected to the upper surface of the fixing plate 10, a threaded rod 13 is fixedly connected to the output end of the motor 11, a left end of the threaded rod 13 is fixedly connected to the inner ring of the bearing seat 16, a threaded cylinder 20 is threadedly connected to the outer surface of the threaded rod 13, and the outer surface of the threaded cylinder 20 is fixedly connected to the upper surface of the slider 15, a nozzle 14 is fixedly connected to the bottom surface of the slider 15, a sliding cylinder 18 is fixedly inlaid on the left side of the frame 4, a connecting pipe 17 is slidably connected to the inner wall of the sliding cylinder 18, and the right end of the connecting pipe 17 is fixedly connected to the left side of the nozzle 14, and two electric push rods 2 are fixedly connected to the inner bottom wall of the frame 4, and a lifting plate 3 is fixedly connected to the top ends of the two electric push rods 2.

[0021] The back of the frame 4 is fixedly connected to a box 22, the inner wall of the box 22 is fixedly connected to a heating wire 23, the back of the box 22 is fixedly inlaid with a group of fans 24, and the front of the box 22 is fixedly inlaid with a group of ventilation pipes 19. By using the cooperation of the heating wires 23 and the fans 24, the ventilation pipes 19 can blow and shape the aircraft parts. The left and right sides of the frame 4 are fixedly connected to mounting plates 5, and the upper surface of each mounting plate 5 is provided with two mounting holes 1. The mounting plate 5, the mounting holes 1 and the external screws are used to facilitate the installation of the device in the use position. The right side of the frame 4 is fixedly connected to a connecting plate 6, and the upper surface of the connecting plate 6 is fixedly connected to a battery 7, which is convenient for providing power through the battery 7.

[0022] A support plate 9 is fixedly connected to the right side of the frame 4, and a side of the support plate 9 away from the frame 4 is fixedly connected to the bottom surface of the fixed plate 10. The support plate 9 is used to increase the stability of the fixed plate 10. A warning sign 8 is fixedly connected to the right side of the frame 4, and a storage box 21 is fixedly connected to the upper surface of the frame 4. The storage box 21 is used to store tools.

[0023] The working principle of the utility model is:

[0024] When the staff uses it, first install the device at the use position through the cooperation of the mounting plate 5, the mounting hole 1 and the external screws, and then connect the connecting pipe 17 with the paint delivery equipment. After the connection is completed, the aircraft parts are placed on the lifting plate 3, and at the same time, the lifting plate 3 is pushed upward by the power provided by the electric push rod 2, and the aircraft parts are brought close to the nozzle 14. At this time, the aircraft parts are sprayed through the cooperation of the connecting pipe 17 and the nozzle 14, and then the threaded rod 13 is driven to rotate inside the bearing seat 16 according to the power provided by the motor 11, and then the slider 15 drives the nozzle 14 to spray evenly through the cooperation of the threaded rod 13 and the threaded cylinder 20, and then the heating wire 23 and the fan 24 are cooperated to make the ventilation pipe 19 blow and shape the aircraft parts.

[0025] It is obvious to those skilled in the art that the present invention is not limited to the details of the exemplary embodiments described above, and that the present invention can be implemented in other specific forms without departing from the spirit or essential features of the present invention. Therefore, the embodiments should be regarded as exemplary and non-restrictive from any point of view, and the scope of the present invention is defined by the appended claims rather than the above description, and it is intended that all changes falling within the meaning and scope of the equivalent elements of the claims be included in the present invention. Any reference numeral in a claim should not be regarded as limiting the claim to which it relates.

[0026] In addition, it should be understood that although the present specification is described according to implementation modes, not every implementation mode contains only one independent technical solution. This description of the specification is only for the sake of clarity. Those skilled in the art should regard the specification as a whole. The technical solutions in each embodiment may also be appropriately combined to form other implementation modes that can be understood by those skilled in the art.

Claims

1. A device for applying paint to the surface of aircraft parts, characterized in that: The invention comprises a frame (4), wherein a sliding opening (12) is provided on the upper surface of the frame (4), a sliding block (15) is slidably connected to the inner wall of the sliding opening (12), a bearing seat (16) is fixedly connected to the upper surface of the frame (4), a fixing plate (10) is fixedly connected to the right side of the frame (4), a motor (11) is fixedly connected to the upper surface of the fixing plate (10), a threaded rod (13) is fixedly connected to the output end of the motor (11), the left end of the threaded rod (13) is fixedly connected to the inner ring of the bearing seat (16), and the outer surface of the threaded rod (13) is threaded. The frame (4) is connected with a threaded cylinder (20), the outer surface of the threaded cylinder (20) is fixedly connected to the upper surface of the slider (15), the bottom surface of the slider (15) is fixedly connected to the nozzle (14), the left side surface of the frame (4) is fixedly inlaid with a slide cylinder (18), the inner wall of the slide cylinder (18) is slidably connected with a connecting pipe (17), the right end of the connecting pipe (17) is fixedly connected to the left side surface of the nozzle (14), the inner bottom wall of the frame (4) is fixedly connected with two electric push rods (2), and the top ends of the two electric push rods (2) are fixedly connected with a lifting plate (3).

2. The device for applying paint to the surface of aircraft parts according to claim 1, characterized in that: The back of the frame (4) is fixedly connected to a box (22), the inner wall of the box (22) is fixedly connected to a heating wire (23), the back of the box (22) is fixedly inlaid with a group of fans (24), and the front of the box (22) is fixedly inlaid with a group of ventilation pipes (19).

3. The device for applying paint to the surface of aircraft parts according to claim 1, characterized in that: The left and right side surfaces of the frame (4) are fixedly connected with mounting plates (5), and the upper surface of each mounting plate (5) is provided with two mounting holes (1).

4. The device for applying paint to the surface of aircraft parts according to claim 1, characterized in that: A connecting plate (6) is fixedly connected to the right side surface of the frame (4), and a storage battery (7) is fixedly connected to the upper surface of the connecting plate (6).

5. The device for applying paint to the surface of aircraft parts according to claim 1, characterized in that: A support plate (9) is fixedly connected to the right side of the frame (4), and a side of the support plate (9) away from the frame (4) is fixedly connected to the bottom surface of the fixing plate (10).

6. The device for applying paint to the surface of aircraft parts according to claim 1, characterized in that: A warning sign (8) is fixedly connected to the right side of the frame (4), and a storage box (21) is fixedly connected to the upper surface of the frame (4).

Images