Aircraft processing coating apparatus

Abstract

The utility model discloses an aircraft processing is with coating equipment, including baseplate and first vertical board, the outer wall of first vertical board is fixed with first cross board, and is fixed with vertical rod between first cross board and baseplate, the outer wall of vertical rod is equipped with a pair of second cross board, the one end of second cross board away from vertical rod is fixed with casing, the upper and inner part of casing is installed with adjusting mechanism and coating mechanism respectively, the utility model relates to aircraft processing technical field, can place the aircraft part that needs to carry out coating to baseplate, starts first motor, makes first motor drive cross bar to rotate, and the roller is rotated, and the roller is payed out to the line, and then cooperation vertical rod and second cross board can drive casing to move down, make casing cover the aircraft part on baseplate, like this when paint spraying is sprayed to the aircraft part surface and scatters to all around, will be blocked by casing to the aircraft part, thereby more favorable to the follow -up cleaning work's progress.

Description

Technical Field

[0001] This utility model relates to the field of aircraft processing technology, specifically to a coating equipment for aircraft processing. Background Technology

[0002] An aircraft is a device that flies within or outside the atmosphere (space). Aircraft are classified into three categories: aircraft, spacecraft, and rockets and missiles. Those that fly within the atmosphere are called aircraft, such as balloons (some), airships, and airplanes. They take off and fly using the static buoyancy of the air or aerodynamic forces generated by relative air motion. During the manufacturing and processing of aircraft, their surfaces need to be painted, thus requiring painting equipment. However, existing equipment for painting aircraft lacks a barrier structure, causing paint sprayed onto the aircraft surface to disperse and hinder subsequent cleaning. Utility Model Content

[0003] To address the shortcomings of existing technologies, this utility model provides a painting equipment for aircraft processing, which solves the problem that when existing equipment paints aircraft, the paint sprayed onto the aircraft surface will spread in all directions due to the lack of a blocking structure, which is not conducive to subsequent cleaning work.

[0004] To achieve the above objectives, this utility model provides the following technical solution: a painting device for aircraft processing, comprising a base and a first vertical plate. A pair of first vertical plates are fixedly connected to the top of the base. A first horizontal plate is fixedly connected to the outer wall of the first vertical plate. A vertical rod is fixedly connected between the first horizontal plate and the base. A pair of second horizontal plates are disposed on the outer wall of the vertical rod. The inner wall of the through hole of the second horizontal plate is clearance-fitted with the outer wall of the vertical rod. A housing is fixedly connected to the end of the second horizontal plate away from the vertical rod. An adjustment mechanism and a painting mechanism are respectively installed on the top and inside of the housing.

[0005] Preferably, the adjustment mechanism includes a top plate fixedly connected to a pair of first vertical plates, a pair of second vertical plates fixedly connected to the bottom end of the top plate, a crossbar rotatably connected inside the second vertical plate, and a pair of rollers fixedly connected to the outer wall of the crossbar. A rope is wound around the outer wall of the rollers, and the end of the rope away from the roller is connected to the housing.

[0006] Preferably, a first motor is fixedly connected to the bottom end of the top plate, and the output shaft of the first motor is connected to the crossbar through a coupling.

[0007] Preferably, the coating mechanism includes a pair of third vertical plates fixedly connected to the inner wall of the top of the housing, and a first pipe is rotatably connected inside the third vertical plate. The top and bottom ends of the first pipe are respectively connected to a second pipe and a plurality of spray heads. The second pipe penetrates the housing. A vertical rod is rotatably connected inside the housing through a bearing. The top of the vertical rod is connected to a second motor through a coupling, and the base of the second motor is fixedly connected to the housing.

[0008] Preferably, a first bevel gear is fixedly connected to the bottom end of the vertical rod, a second bevel gear is threadedly connected to the outer circumference of the first bevel gear, and the second bevel gear is fixedly connected to the first pipe. Beneficial effects

[0009] This utility model provides a painting equipment for aircraft processing, which has the following beneficial effects:

[0010] The aircraft parts that need to be painted can be placed on the base. Start the first motor to drive the crossbar to rotate. The crossbar drives the roller to rotate and the roller releases the line. With the help of the vertical bar and the second horizontal plate, the shell can be moved downward to cover the aircraft parts on the base. In this way, when the paint is sprayed onto the surface of the aircraft parts and spreads in all directions, it will be blocked by the shell, which will make it easier for subsequent cleaning work. Attached Figure Description

[0011] Figure 1 This is a schematic diagram of the structure of this utility model.

[0012] Figure 2 This is a partially enlarged schematic diagram of the present invention.

[0013] Figure 3 This is a partially enlarged schematic diagram of the present invention.

[0014] Figure 4 This is a partially enlarged schematic diagram of the present invention.

[0015] In the diagram: 1. Base; 2. First vertical plate; 3. First horizontal plate; 4. Vertical rod; 5. Second horizontal plate; 6. Housing; 7. Second vertical plate; 8. Horizontal rod; 9. Roller; 10. Rope; 11. First motor; 12. Third vertical plate; 13. First pipe; 14. Second pipe; 15. Spray head; 16. Second motor; 17. Second vertical rod; 18. First bevel gear; 19. Second bevel gear; 20. Top plate. Detailed Implementation

[0016] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0017] Please see Figure 1-4 This utility model provides a technical solution: a painting equipment for aircraft processing, including a base 1 and a first vertical plate 2. A pair of first vertical plates 2 are fixedly connected to the top of the base 1. A first horizontal plate 3 is fixedly connected to the outer wall of the first vertical plate 2. A vertical rod 4 is fixedly connected between the first horizontal plate 3 and the base 1. A pair of second horizontal plates 5 are arranged on the outer wall of the vertical rod 4. The inner wall of the through hole of the second horizontal plate 5 is clearance-fitted with the outer wall of the vertical rod 4. A housing 6 is fixedly connected to the end of the second horizontal plate 5 away from the vertical rod 4. An adjustment mechanism and a painting mechanism are respectively installed on the top and inside of the housing 6.

[0018] A through hole can be machined inside the second horizontal plate 5, and a vertical rod 4 can be set at this through hole. In this way, the shell 6 can be limited by the vertical rod 4 and the second horizontal plate 5. At the same time, the shell 6 can be made of transparent material to facilitate observation of the internal situation.

[0019] In this embodiment, the adjustment mechanism is further configured such that the top plate 20 is fixedly connected to a pair of first vertical plates 2, a pair of second vertical plates 7 are fixedly connected to the bottom end of the top plate 20, a crossbar 8 is rotatably connected inside the second vertical plate 7, and a pair of rollers 9 are fixedly connected to the outer wall of the crossbar 8. A rope 10 is wound around the outer wall of the rollers 9, and the end of the rope 10 away from the rollers 9 is connected to the housing 6.

[0020] When the crossbar 8 drives the roller 9 to rotate, the roller 9 can drive the housing 6 to move through the rope 10, thereby adjusting the height of the housing 6.

[0021] In this embodiment, the bottom end of the top plate 20 is fixedly connected to a first motor 11, and the output shaft of the first motor 11 is connected to the crossbar 8 through a coupling.

[0022] In this embodiment, the coating mechanism includes a pair of third vertical plates 12 fixedly connected to the inner wall of the top of the housing 6, and a first pipe 13 is rotatably connected inside the third vertical plate 12. The top and bottom ends of the first pipe 13 are respectively connected to a second pipe 14 and a plurality of spray heads 15. The second pipe 14 penetrates the housing 6. A second vertical rod 17 is rotatably connected inside the housing 6 through a bearing. The top of the second vertical rod 17 is connected to a second motor 16 through a coupling, and the base of the second motor 16 is fixedly connected to the housing 6.

[0023] The first pipe 13 is closed at both ends, while the second pipe 14 is extendable to meet the rotation requirements of the first pipe 13. At the same time, the second pipe 14 is connected to an external coating material supply machine.

[0024] In this embodiment, the bottom end of the second vertical rod 17 is fixedly connected to a first bevel gear 18, the outer circumference of the first bevel gear 18 is threadedly connected to a second bevel gear 19, and the second bevel gear 19 is fixedly connected to the first pipe 13.

[0025] The second motor 16 can be started, causing the second vertical rod 17 to rotate regularly. The second vertical rod 17 then drives the second bevel gear 19 to rotate through the first bevel gear 18, which in turn drives the first pipe 13 to rotate. This allows the spraying angle of the spray head 15 on the first pipe 13 to be adjusted, thereby increasing the spraying range.

[0026] It is worth noting that the electrical structures and other components involved in this application can be selected according to the user's needs, as long as they meet the requirements of this application. At the same time, the corresponding control circuits and other components are all existing technologies, which can be fully implemented by those skilled in the art, so they will not be described in detail here.

[0027] Those skilled in the art can connect the components in this case sequentially. The specific connection and operation sequence should refer to the working principle described below. The detailed connection methods are well-known technologies in the field. The working principle and process are mainly described below.

[0028] Example: When this device is needed, the external power supply and control circuit of each electrical structure can be connected. Then, the second pipe 14 is connected to the external painting material supply machine. The aircraft parts to be painted are then placed on the base 1. The first motor 11 is started, which drives the crossbar 8 to rotate. The crossbar 8 drives the roller 9 to rotate. The roller 9 releases the line 10. With the help of the vertical bar 4 and the second horizontal plate 5, the shell 6 can be moved downward so that the shell 6 covers the aircraft parts on the base 1. In this way, when the paint is sprayed onto the surface of the aircraft parts and spreads in all directions, it will be blocked by the shell 6, which makes it easier for subsequent cleaning work.

[0029] When the external coating supply machine injects material into the second pipe 14, the paint flows into the first pipe 13 through the second pipe 14, and is then sprayed out through the spray head 15 to coat the aircraft parts below. At the same time, the second motor 16 is started, causing the second motor 16 to drive the second vertical rod 17 to rotate regularly. The second vertical rod 17 then drives the second bevel gear 19 to rotate through the first bevel gear 18, which in turn drives the first pipe 13 to rotate. This allows the spray angle of the spray head 15 on the first pipe 13 to be adjusted, thereby increasing the coating range.

[0030] It should be noted that, in this document, relational terms such as "first" and "second" are used merely to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such a process, method, article, or apparatus. Without further limitations, the phrase "comprising an element defined as..." does not exclude the presence of other identical elements in the process, method, article, or apparatus that includes said element.

[0031] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A painting device for aircraft processing, comprising a base (1) and a first vertical plate (2), wherein a pair of first vertical plates (2) are fixedly connected to the top of the base (1), characterized in that: A first horizontal plate (3) is fixed to the outer wall of the first vertical plate (2), and a vertical rod (4) is fixed between the first horizontal plate (3) and the base (1). A pair of second horizontal plates (5) are arranged on the outer wall of the vertical rod (4), and the inner wall of the through hole of the second horizontal plate (5) is clearance-fitted with the outer wall of the vertical rod (4). A housing (6) is fixed to the end of the second horizontal plate (5) away from the vertical rod (4). An adjustment mechanism and a coating mechanism are respectively installed on the top and inside of the housing (6).

2. The coating equipment for aircraft processing according to claim 1, characterized in that, The adjustment mechanism includes a top plate (20) fixedly connected to a pair of first vertical plates (2), a pair of second vertical plates (7) fixedly connected to the bottom end of the top plate (20), a crossbar (8) rotatably connected inside the second vertical plate (7), and a pair of rollers (9) fixedly connected to the outer wall of the crossbar (8), a rope (10) wound around the outer wall of the rollers (9), and the end of the rope (10) away from the rollers (9) is connected to the housing (6).

3. The coating equipment for aircraft processing according to claim 2, characterized in that, The bottom end of the top plate (20) is fixedly connected to the first motor (11), and the output shaft of the first motor (11) is connected to the crossbar (8) through a coupling.

4. The coating equipment for aircraft processing according to claim 3, characterized in that, The coating mechanism includes a pair of third vertical plates (12) fixed to the inner wall of the top of the housing (6), and a first pipe (13) is rotatably connected inside the third vertical plate (12). The top and bottom ends of the first pipe (13) are respectively connected to a second pipe (14) and a number of spray heads (15). The second pipe (14) penetrates the housing (6). A second vertical rod (17) is rotatably connected inside the housing (6) through a bearing. The top of the second vertical rod (17) is connected to a second motor (16) through a coupling. The base of the second motor (16) is fixed to the housing (6).

5. The coating equipment for aircraft processing according to claim 4, characterized in that, The bottom end of the second vertical rod (17) is fixedly connected to a first bevel gear (18), the outer circumference of the first bevel gear (18) is threadedly connected to a second bevel gear (19), and the second bevel gear (19) is fixedly connected to the first pipe (13).

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