Spraying device for aviation part machining

Abstract

The utility model discloses a spraying device for aviation part processing, which comprises a box body, the upper surface of the box body is fixedly provided with a gear motor, the upper surface of the box body is fixedly provided with a shell, the inner top wall of the box body is fixedly embedded with a bearing, the inner ring of the bearing is fixedly connected with a rotating rod, and the rotating rod is fixedly connected with a rotating shaft. The top end of the rotating rod is fixedly connected with the output end of a gear motor. According to the aviation part spraying device, the gear motor drives the rotating rod and the rotating plate to rotate slowly and is matched with the two electric push rods and the two fixing plates, aviation parts can be fixed, clamped and rotated, then the aviation parts can be evenly sprayed, the pump body, the discharging pipe and the spraying head are arranged, and the spraying efficiency is improved. According to the spraying device for the aviation parts, spraying paint in the storage box can be rapidly extracted to conduct spraying treatment on the aviation parts, through cooperation of the two guide plates, the three through openings and the collecting hopper, the paint splashed during spraying can be collected, and loss of the spraying paint is reduced.

Description

Technical Field

[0001] The present application relates to the technical field of aviation parts, and in particular to a spraying device for processing aviation parts. Background Art

[0002] Aviation parts refer to independently replaceable components used on aircraft that do not affect the overall structure and performance of the aircraft. The quality, performance and reliability of aviation parts are key to ensuring the safe flight of aircraft.

[0003] However, at present, when spraying aviation parts, workers usually use handheld spray guns to spray them, which has poor flexibility, not only increasing the loss of spray material, but also endangering the health of workers. Therefore, we propose a spraying device for aviation parts processing to solve the above problems. Utility Model Content

[0004] The purpose of the present utility model is to provide a spraying device for machining aviation parts, so as to solve the problems raised in the above-mentioned background technology.

[0005] The embodiments of this application adopt the following technical solutions:

[0006] A spraying device for processing aviation parts includes a box body, a reduction motor is fixedly installed on the upper surface of the box body, a shell is fixedly installed on the upper surface of the box body, a bearing is fixedly inlaid on the inner top wall of the box body, the inner ring of the bearing is fixedly connected to a rotating rod, the top end of the rotating rod is fixedly connected to the output end of the reduction motor, the bottom end of the rotating rod is fixedly connected to a rotating plate, the bottom surface of the rotating plate is fixedly connected to two mounting plates, the side surfaces of the two mounting plates close to each other are fixedly installed with electric push rods, the telescopic ends of the two electric push rods are fixedly installed with fixed plates, and the side surfaces of the two mounting plates close to each other are fixedly connected with the A protective shell is fixedly installed on each side, a storage box is fixedly connected to the upper surface of the box body, a pump body is fixedly installed on the upper surface of the box body, the input end of the pump body passes through the storage box and extends to the interior of the storage box, the output end of the pump body is fixedly connected to a discharge pipe, the end of the discharge pipe away from the pump body passes through the box body and extends to the interior of the box body, the end of the discharge pipe away from the pump body is fixedly connected to a nozzle, the inner side wall of the box body is fixedly connected to two material guide plates, the inner bottom wall of the box body is provided with three openings, the bottom surface of the box body is provided with two slide grooves, and the interiors of the two slide grooves are slidably connected to a collecting bucket.

[0007] Preferably, two reinforcement blocks are fixedly mounted on the inner side wall of the box body, and the right sides of the two reinforcement blocks are fixedly mounted on the left side of the nozzle.

[0008] Preferably, a sealed door is hinged on the front of the box through a hinge, and an observation window is provided on the front of the sealed door.

[0009] Preferably, the upper surface of the storage box is fixedly connected to a feed hopper, and the bottom surface of the box body is fixedly connected to two groups of supporting legs.

[0010] Preferably, a square opening is provided on the back side of the shell, and a protective net is provided inside the square opening.

[0011] Preferably, a control panel is fixedly mounted on the front of the sealing door, and the reduction motor, electric push rod and pump body are all electrically connected to the control panel via wires.

[0012] At least one of the above technical solutions adopted in the embodiments of the present application can achieve the following beneficial effects:

[0013] The spraying device for processing aviation parts drives the rotating rod and the rotating plate to rotate slowly through the provided reduction motor, and cooperates with the two electric push rods and the two fixed plates to fix and clamp the aviation parts and rotate them, and then can evenly spray the aviation parts. The provided pump body, discharge pipe and nozzle can be used to quickly extract the spray paint in the storage box for spraying the aviation parts. The provided two guide plates, three openings and collection bucket cooperate to collect the paint splashed during spraying, thereby reducing the loss of spray paint. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] The drawings described herein are used to provide a further understanding of the present application and constitute a part of the present application. The illustrative embodiments of the present application and their descriptions are used to explain the present application and do not constitute an improper limitation on the present application. In the drawings:

[0015] Figure 1 : A front view structural diagram of the spraying device for machining aviation parts of the utility model;

[0016] Figure 2 This is a front cross-sectional view of the spraying device for machining aviation parts according to the present invention;

[0017] Figure 3 This is a front cross-sectional view of a protective shell in a spray coating device for machining aviation parts according to the present invention;

[0018] Figure 4 : A rear structural schematic diagram of the utility model of a spraying device for machining aviation parts.

[0019] In the figure: 1. Box body; 2. Reducer motor; 3. Bearing; 4. Rotating rod; 5. Rotating plate; 6. Mounting plate; 7. Electric push rod; 8. Fixed plate; 9. Protective shell; 10. Shell; 11. Square opening; 12. Protective net; 13. Storage box; 14. Feed hopper; 15. Pump body; 16. Discharge pipe; 17. Nozzle; 18. Reinforcement block; 19. Guide plate; 20. Through port; 21. Chute; 22. Collecting hopper; 23. Control panel; 24. Sealing door; 25. Observation window; 26. Support leg. DETAILED DESCRIPTION

[0020] To make the purpose, technical solutions, and advantages of this application more clear, the technical solutions of this application will be clearly and completely described below in conjunction with the specific embodiments of this application and the corresponding drawings. Obviously, the embodiments described are only part of the embodiments of this application, not all of them. Based on the embodiments in this application, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of this application.

[0021] The following describes in detail the technical solutions provided by various embodiments of the present application in conjunction with the accompanying drawings.

[0022] See also Figure 1-4 , the utility model provides a technical solution for a spraying device for processing aviation parts:

[0023] A spraying device for processing aviation parts includes a box body 1, a reduction motor 2 is fixedly installed on the upper surface of the box body 1, a shell 10 is fixedly installed on the upper surface of the box body 1, a bearing 3 is fixedly inlaid on the inner top wall of the box body 1, the inner ring of the bearing 3 is fixedly connected to a rotating rod 4, the top of the rotating rod 4 is fixedly connected to the output end of the reduction motor 2, the bottom end of the rotating rod 4 is fixedly connected to a rotating plate 5, the bottom surface of the rotating plate 5 is fixedly connected to two mounting plates 6, the side surfaces of the two mounting plates 6 close to each other are fixedly installed with electric push rods 7, the telescopic ends of the two electric push rods 7 are fixedly installed with fixed plates 8, the side surfaces of the two mounting plates 6 close to each other are fixedly installed with protective shells 9, a material storage box 13 is fixedly connected to the upper surface of the box body 1, a pump body 15 is fixedly installed on the upper surface of the box body 1, the input end of the pump body 15 passes through the material storage box 13 and extends to the interior of the material storage box 13, and the output end of the pump body 15 passes through the material storage box 13 and extends to the interior of the material storage box 13. The end is fixedly connected with a discharge pipe 16, and the end of the discharge pipe 16 away from the pump body 15 passes through the box body 1 and extends to the interior of the box body 1, and the end of the discharge pipe 16 away from the pump body 15 is fixedly connected with a nozzle 17. The inner side wall of the box body 1 is fixedly connected with two guide plates 19, and the inner bottom wall of the box body 1 is provided with three through-holes 20. The bottom surface of the box body 1 is provided with two slide grooves 21, and the inside of the two slide grooves 21 is slidably connected with a collecting bucket 22; specifically, the aviation parts can be fixedly clamped and rotated by the reduction motor 2, the bearing 3, the rotating rod 4, the rotating plate 5, the two electric push rods 7 and the two fixed plates 8. The pump body 15, the discharge pipe 16 and the nozzle 17 can be used to quickly extract the spray paint in the storage box 13 to spray the aviation parts. The paint splashed during spraying can be collected by the two guide plates 19, the three through-holes 20 and the collecting bucket 22;

[0024] In this embodiment, two reinforcing blocks 18 are fixedly installed on the inner side wall of the box body 1, and the right sides of the two reinforcing blocks 18 are fixedly installed to the left side of the spray head 17; the front of the box body 1 is hinged with a sealing door 24 by a hinge, and the front of the sealing door 24 is provided with an observation window 25; the upper surface of the storage box 13 is fixedly connected to the feed hopper 14, and the bottom surface of the box body 1 is fixedly connected to two groups of supporting legs 26; specifically, the two reinforcing blocks 18 can make the spray head 17 more stable, the sealing door 24 can be used to seal the box body 1, the spraying condition in the box body 1 can be observed through the observation window 25, the feed hopper 14 can be used to add spray paint into the storage box 13, and the two groups of supporting legs 26 can support the device;

[0025] In this embodiment, a square opening 11 is provided on the back of the shell 10, and a protective net 12 is provided inside the square opening 11; a control panel 23 is fixedly installed on the front of the sealing door 24, and the reduction motor 2, the electric push rod 7 and the pump body 15 are all electrically connected to the control panel 23 through wires; specifically, the square opening 11 and the protective net 12 can be used for ventilation and protection, and the start-up of the device can be conveniently controlled through the control panel 23.

[0026] Working principle: When the spraying device for processing aviation parts is used, the user first opens the sealing door 24 to take the aviation parts between the two fixed plates 8, and starts the two electric push rods 7 to push the two fixed plates 8 closer to each other to fix and clamp the aviation parts. Then close the sealing door 24, and start the reduction motor 2 to drive the rotating rod 4, the rotating plate 5 and the aviation parts to rotate slowly. At the same time, start the pump body 15 to extract the spray paint in the storage box 13 and evenly spray the aviation parts through the discharge pipe 16 and the nozzle 17. During the spraying process, the splashed spray paint flows into the collecting bucket 22 through the two guide plates 19 and the three openings 20.

[0027] It should also be noted that the terms "comprises," "includes," or any other variations thereof are intended to encompass non-exclusive inclusion, such that a process, method, commodity, or apparatus that includes a series of elements includes not only those elements but also other elements not explicitly listed, or includes elements inherent to such process, method, commodity, or apparatus. In the absence of further limitations, an element defined by the phrase "comprises a ..." does not exclude the presence of other identical elements in the process, method, commodity, or apparatus that includes the element.

[0028] The foregoing is merely an embodiment of the present application and is not intended to limit the present application. For those skilled in the art, the present application may have various changes and variations. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present application should all be included within the scope of the claims of the present application.

Claims

1. A spraying device for processing aviation parts, comprising a housing (1), characterized in that: The upper surface of the box (1) is fixedly mounted with a reduction motor (2), the upper surface of the box (1) is fixedly mounted with a shell (10), the inner top wall of the box (1) is fixedly inlaid with a bearing (3), the inner ring of the bearing (3) is fixedly connected with a rotating rod (4), the top end of the rotating rod (4) is fixedly connected to the output end of the reduction motor (2), the bottom end of the rotating rod (4) is fixedly connected with a rotating plate (5), the bottom surface of the rotating plate (5) is fixedly connected with two mounting plates (6), the side of the two mounting plates (6) close to each other is fixedly mounted with an electric push rod (7), the telescopic ends of the two electric push rods (7) are fixedly mounted with a fixed plate (8), the side of the two mounting plates (6) close to each other is fixedly mounted with a protective shell (9), the upper surface of the box (1) is fixedly mounted with a bearing (3), the inner ring of the bearing (3) is fixedly connected with a rotating rod (4), the top end of the rotating rod (4) is fixedly connected with an output end of the reduction motor (2), the bottom end of the rotating rod (4) is fixedly connected with a rotating plate (5), the bottom surface of the rotating plate (5) is fixedly connected with two mounting plates (6), the side of the two mounting plates (6) close to each other is fixedly mounted with an electric push rod (7), the telescopic ends of the two electric push rods (7) are fixedly mounted with a fixed plate (8), the side of the two mounting plates (6) close to each other is fixedly mounted with a protective shell (9), the upper surface of the box (1) is fixedly mounted with a bearing (3), the inner ring of the bearing (3) is fixedly connected with a rotating rod (4), the top end of the rotating rod (4) is fixedly connected with a rotating plate (5), the bottom surface of the rotating plate (5) is fixedly connected with two mounting plates (6), the bottom surface of the rotating plate (5) is fixedly mounted with a protective shell (9), the upper A material storage box (13) is fixedly connected to the box body (1), and a pump body (15) is fixedly installed on the upper surface of the box body (1), the input end of the pump body (15) passes through the material storage box (13) and extends to the interior of the material storage box (13), the output end of the pump body (15) is fixedly connected to a discharge pipe (16), the end of the discharge pipe (16) away from the pump body (15) passes through the box body (1) and extends to the interior of the box body (1), and the end of the discharge pipe (16) away from the pump body (15) is fixedly connected to a nozzle (17), the inner side wall of the box body (1) is fixedly connected to two material guide plates (19), the inner bottom wall of the box body (1) is provided with three openings (20), and the bottom surface of the box body (1) is provided with two slide grooves (21), and the interiors of the two slide grooves (21) are slidably connected to a collecting bucket (22).

2. The spraying device for machining aviation parts according to claim 1, characterized in that: Two reinforcement blocks (18) are fixedly mounted on the inner side wall of the box body (1), and the right sides of the two reinforcement blocks (18) are fixedly mounted on the left side of the nozzle (17).

3. The spray coating device for aviation parts processing according to claim 1, characterized in that: A sealed door (24) is hingedly connected to the front of the box body (1) via a hinge, and an observation window (25) is provided on the front of the sealed door (24).

4. The spray coating device for aviation parts processing according to claim 1, characterized in that: The upper surface of the storage box (13) is fixedly connected to the feed hopper (14), and the bottom surface of the box body (1) is fixedly connected to two groups of support legs (26).

5. The spray coating device for aviation parts processing according to claim 1, characterized in that: A square opening (11) is provided on the back of the housing (10), and a protective net (12) is provided inside the square opening (11).

6. The spray coating device for aviation parts processing according to claim 3, characterized in that: A control panel (23) is fixedly mounted on the front of the sealing door (24), and the reduction motor (2), the electric push rod (7) and the pump body (15) are all electrically connected to the control panel (23) via wires.

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