Spraying machine device and method for airplane empennage

Abstract

The invention discloses a spraying machine device and method for an airplane empennage, and relates to the field of airplane empennage spraying. The spraying machine device comprises a spraying bin, a door plate is installed on the side wall of the spraying bin, a linear module is installed on the inner top wall of the spraying bin, and a first motor is installed on the outer wall of the spraying bin; and the execution end of the first motor penetrates through the outer wall of the spraying bin and is connected with a placement plate, the placement plate is rotationally connected with the spraying bin, a U-shaped frame is installed at the execution end of the linear module, a plurality of electric telescopic rods are symmetrically embedded in the bottom of the U-shaped frame, and the execution ends of the electric telescopic rods are rectangular plates correspondingly. By arranging the adjusting mechanism, the situation that a large amount of coating is splashed to other parts of the airplane empennage due to the fact that large impact force is generated between the coating sprayed out of the spray head and the top of the airplane empennage is avoided, the phenomenon that the coating on the other parts is not uniform is avoided, and then the spraying effect is improved.

Description

Technical Field

[0001] The invention relates to the field of aircraft tail fin spraying, in particular to a spraying machine device and a method for aircraft tail fins. Background Art

[0002] The tail of an aircraft is a device installed at the tail of the aircraft to enhance the stability of flight. Most tails include a horizontal tail and a vertical tail, and a few use a V-shaped tail. The tail can be used to control the pitch, yaw and tilt of the aircraft to change its flight attitude. The tail is an important part of the flight control system.

[0003] When an existing sprayer is spraying an aircraft tail, the position of the spray head cannot be changed when the spray head is adjusted from the side to the top of the aircraft tail, which results in a large impact force when the paint is sprayed from the top to the top of the aircraft tail at a close distance, causing the paint to splash to other parts of the aircraft tail, thereby causing uneven spraying of other parts. To this end, we provide a sprayer device and method for an aircraft tail to solve the above problem. Summary of the invention

[0004] The purpose of the present invention is to provide a spraying machine device and method for an aircraft tail in order to solve the problem that the position of the nozzle cannot be changed, which leads to the paint spraying from the top to the top of the aircraft tail at a close distance, which easily generates a large impact force, thereby causing the paint to splash to other parts of the aircraft tail, thereby causing uneven spraying of other parts.

[0005] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: a spraying machine device for an aircraft tail, comprising: a spraying chamber, a door panel is installed on the side wall of the spraying chamber, a linear module is installed on the inner top wall of the spraying chamber, a first motor is installed on the outer wall of the spraying chamber, an execution end of the first motor passes through the outer wall of the spraying chamber and is connected to a placement plate, and the placement plate is rotatably connected to the spraying chamber, a U-shaped frame is installed on the execution end of the linear module, a plurality of electric telescopic rods are symmetrically embedded at the bottom of the U-shaped frame, and the execution ends of the electric telescopic rods are respectively rectangular plates; a spray head, the spray head is arranged at the bottom of the rectangular plate; an adjusting mechanism, respectively located at the bottom of the two rectangular plates, for adjusting the angle between the spray head and the aircraft tail; a protector, located at the bottom, for preventing the material sprayed from the spray head from splashing.

[0006] As a further solution of the present invention: the adjusting mechanism includes two fixed plates respectively installed at the bottom of the rectangular plate, wherein the side wall of one of the fixed plates is provided with a rotating motor, the executing end of the rotating motor penetrates through the side wall of one of the fixed plates and is connected to the movable plate, the side wall of the movable plate away from the rotating motor is connected to one of the fixed plates through a rotating shaft, a second motor is provided on one side of the movable plate, a first screw rod is installed on the executing end of the second motor, and one end of the first screw rod penetrates through the inner side of the movable plate and is rotatably connected to the movable plate, the outer wall of the first screw rod is threadedly connected to a slider, the nozzle is installed on the side of the slider away from the first screw rod, and the nozzle is connected to an external feeding device through a pipe inside the slider.

[0007] As a further solution of the present invention: the guard includes a slide groove opened on the inner wall of the movable plate, a connecting block is installed on one side of the movable plate, and the connecting block matches the slide groove, a U-shaped rack is installed on the side wall of the connecting block, and two connecting seats are fixedly connected to one side of the movable plate, and the two connecting seats are symmetrically arranged about the central axis of the movable plate, and a large gear is rotatably connected to one side of each connecting seat, and the two large gears are meshed with the U-shaped rack, and a small gear is meshed on one side of the large gear, and a first shaft rod is fixedly connected to one side of the small gear, and the first shaft rod is rotatably connected to the inner side of the connecting seat, and a baffle is fixedly connected to the outer wall of the first shaft rod, and a bending protection component is installed on the side of the baffle away from the connecting seat.

[0008] As a further solution of the present invention: the bending protection assembly includes a second limit seat fixedly connected to one end of the baffle, a folding plate is arranged on the inner side of the second limit seat, a rotating shaft is fixedly connected on both sides of the folding plate, and one end of the rotating shaft passes through the inner side of the second limit seat and is rotatably connected to the second limit seat, and a torsion spring is installed between the folding plate and the second limit seat.

[0009] As a further solution of the present invention: the bending protection assembly also includes a first limit seat fixedly connected to the end of the baffle, a second screw rod is rotatably connected to the inner side of the first limit seat, a power block is threadedly connected to the outer wall of the second screw rod, a roller is rotatably connected to one end of the power block, a spur gear is fixedly connected to the outer wall of the second screw rod, a spur rack is meshed with the bottom of the spur gear, and a toggle assembly for moving the spur rack is provided on the inner side of the first shaft.

[0010] As a further solution of the present invention: a rectangular limit block is fixedly connected to the inner side of the first limit seat, and limit grooves matching the rectangular limit block are opened on both sides of the power block, and the power block is slidably connected to the rectangular limit block through the limit grooves opened on both sides.

[0011] As a further solution of the present invention: the toggle assembly includes a second shaft rod slidably connected to the inner side of the first shaft rod, a connecting rod is fixedly connected to the outer wall of the second shaft rod, the inner side of the first shaft rod is provided with a through groove that penetrates to the outside and matches the connecting rod, one end of the connecting rod is fixedly connected to the spur rack, one end of the second shaft rod penetrates to the outer wall of the first shaft rod and is fixedly connected to a push block, and a connecting spring is installed between the inner side of the push block and the end of the first shaft rod.

[0012] As a further solution of the present invention: the toggle assembly also includes a convex block fixedly connected to one side of the movable plate, a mating block is fixedly connected to the inner side of the convex block, an end face of the mating block is provided with an arc track, a spherical rod is fixedly connected to one side of the push block, and the spherical rod rests on the lowest point of the arc track.

[0013] The present invention also discloses a spraying method for an aircraft tail wing, which uses the above-mentioned spraying machine device for an aircraft tail wing, and comprises the following steps: S1. First, the aircraft tail to be sprayed is fixed on the placement plate by a conveying device, and then the linear module and the electric telescopic rod are started to drive the rectangular plate at the bottom of the U-shaped frame to move inside the spraying chamber, and then the paint is sent from the pipe inside the slider to the nozzle through the spraying equipment, and the two nozzles are used to spray both sides of the aircraft tail. When the spraying of both sides is completed, the nozzle is moved to the top of the aircraft tail with the cooperation of the linear module and the electric telescopic rod, and then the rotating motor located at the top of the aircraft tail is started to drive the movable plate to rotate ninety degrees on the fixed plate. The second motor is started while the movable plate is rotating, and the output end of the second motor drives the first screw to rotate, and the first screw drives the slider and the nozzle to move inside the movable plate, thereby increasing the distance between the nozzle and the top of the aircraft tail wing. In this way, when the nozzle is spraying the top of the aircraft tail wing, the paint sprayed by the nozzle and the top of the aircraft tail wing will not generate a large impact force to cause a large amount of paint to splash to other parts of the aircraft tail wing, thereby avoiding uneven paint in other parts, thereby improving the spraying effect; S2, when the slider drives the spray head to move toward the inner side of the movable plate, the U-shaped rack is driven to move synchronously through the connecting block, thereby driving the large gear to rotate, and then driving the small gear to drive the spur gear to rotate toward the side of the aircraft tail through the first shaft rod. When the slider stops moving, the two baffles are rotated in an inclined state on both sides of the aircraft tail, thereby blocking the paint splashed by the spray head and the top of the aircraft tail, thereby preventing the splashed paint from flying to other parts of the aircraft tail and causing uneven paint, thereby further improving the uniformity of the aircraft tail spraying; S3, when the spray head is in a horizontal state to spray the side of the aircraft tail, the two baffles initially unfolded at 30 degrees can also play the role of preventing the paint sprayed from the spray head from hitting the aircraft tail to produce splashes; S4. When the first shaft rotates, the spherical rod rotates along the lowest point of the arc track at the end of the mating block to the highest point, so that the spherical rod is pushed to drive the second shaft to move toward the first shaft under the action of the arc track, thereby driving the spur rack to move toward the spur gear through the connecting rod, and then driving the second screw rod to rotate. The second screw rod rotates to drive the power block to drive the roller to move toward the folding plate, thereby pushing the folding plate to rotate toward the inside of the baffle. When the baffle stops rotating, the roller is close to the side of the aircraft tail, thereby reducing the gap between the baffle and the aircraft tail, thereby better blocking the splashing paint.

[0014] Compared with the prior art, the present invention has the following beneficial effects: 1. Through the adjustment mechanism, the linear module and the electric telescopic rod cooperate to move the nozzle to the top of the aircraft tail wing, and then start the rotating motor located at the top of the aircraft tail wing to drive the movable plate to rotate 90 degrees on the fixed plate, so that the nozzle rotates toward the top of the aircraft tail wing. While the movable plate rotates, start the second motor, and the output end of the second motor drives the first screw to rotate. The first screw drives the slider and the nozzle to move inside the movable plate, thereby increasing the distance between the nozzle and the top of the aircraft tail wing. In this way, when the nozzle sprays the top of the aircraft tail wing, the paint sprayed by the nozzle and the top of the aircraft tail wing will not generate a large impact force, causing a large amount of paint to splash to other parts of the aircraft tail wing, thereby avoiding uneven paint in other parts, thereby improving the spraying effect; 2. Through the set protector, the slider drives the nozzle to move to the inside of the movable plate and drives the U-shaped rack to move synchronously through the connecting block, thereby driving the large gear to rotate, and then driving the small gear to drive the spur gear to rotate to the side of the aircraft tail through the first shaft rod. When the slider stops moving, the two baffles rotate in an inclined state on both sides of the aircraft tail, thereby blocking the paint splashed by the nozzle and the top of the aircraft tail, thereby preventing the splashed paint from flying to other parts of the aircraft tail and causing uneven paint, thereby further improving the uniformity of the aircraft tail spraying; 3. By setting up the bending protection component, when the first shaft rod rotates, the spherical rod rotates along the lowest point to the highest point of the arc track at the end of the fitting block, so that the spherical rod is pushed to drive the second shaft rod to move toward the first shaft rod under the action of the arc track, thereby driving the spur rack to move toward the spur gear through the connecting rod, and then driving the second screw rod to rotate. The second screw rod rotates to drive the power block to drive the roller to move toward the folding plate, thereby pushing the folding plate to rotate toward the inside of the baffle. When the baffle stops rotating, the roller is close to the side of the aircraft tail, thereby reducing the gap between the baffle and the aircraft tail, thereby better blocking the splashing paint. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 It is an axial view of the present invention; Figure 2 It is a back axial view of the present invention; Figure 3 is a side sectional view of the present invention; Figure 4 It is the axial view of the U-shaped frame of the present invention; Figure 5 An exploded view of the electric telescopic rod of the present invention; Figure 6 is a cross-sectional view of the movable panel of the present invention; Figure 7 A cross-sectional view of a slider of the present invention; Figure 8 It is a schematic diagram of the structure of the protector of the present invention; Fig. 9 It is a schematic diagram of the local structure of the convex block of the present invention; Fig.10 It is a schematic diagram of the back structure of the folding plate of the present invention; Fig.11 For the present invention Fig.10 Middle A enlarged view; Fig.12 It is a schematic diagram of the connection between the baffle and the folding plate of the present invention; Fig.13 It is a schematic diagram of the structure after the baffle and the folding plate of the present invention are adjusted.

[0016] In the figure: 1, spray chamber; 2, linear module; 3, first motor; 4, placement plate; 5, U-shaped frame; 6, electric telescopic rod; 7, rectangular plate; 8, fixed plate; 9, movable plate; 10, second motor; 11, first screw rod; 12, slider; 13, slide groove; 14, connecting block; 15, U-shaped rack; 16, connecting seat; 17, large gear; 18, small gear; 19, first shaft rod; 20, baffle; 22, first Two-axis rod; 23, push block; 24, connecting spring; 25, fitting block; 26, connecting rod; 27, folding plate; 28, first limit seat; 29, spur rack; 30, spur gear; 31, second screw rod; 32, power block; 33, roller; 34, rectangular limit block; 35, second limit seat; 36, rotating shaft; 37, nozzle; 38, rotating motor; 39, convex block; 40, torsion spring; 41, spherical rod. DETAILED DESCRIPTION

[0017] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0018] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inside", "outside" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the drawings, which are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as limiting the present invention. In addition, the terms "first", "second", and "third" are only used for descriptive purposes and cannot be understood as indicating or implying relative importance. In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "connected", "connected", and "set" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be directly connected, or indirectly connected through an intermediate medium, or it can be the internal connection of two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to specific circumstances. The following is an explanation of an embodiment of the present invention based on the overall structure of the present invention.

[0019] Example 1 See also Figures 1 to 13The present embodiment provides a spraying machine device for an aircraft tail, comprising: a spraying chamber 1, a door panel is installed on the side wall of the spraying chamber 1, a linear module 2 is installed on the inner top wall of the spraying chamber 1, a first motor 3 is installed on the outer wall of the spraying chamber 1, an execution end of the first motor 3 passes through the outer wall of the spraying chamber 1 and is connected to a placement plate 4, and the placement plate 4 is rotatably connected to the spraying chamber 1, a U-shaped frame 5 is installed on the execution end of the linear module 2, a plurality of electric telescopic rods 6 are symmetrically embedded at the bottom of the U-shaped frame 5, and the execution ends of the electric telescopic rods 6 are respectively rectangular plates 7; a spray head 37, the spray head 37 is arranged at the bottom of the rectangular plate 7; an adjustment mechanism is respectively located at the bottom of the two rectangular plates 7, and is used for adjusting the angle between the spray head 37 and the tail of the aircraft, and the adjustment mechanism It includes two fixed plates 8 respectively installed at the bottom of the rectangular plate 7, a rotating motor 38 is provided on the side wall of one of the fixed plates 8, the execution end of the rotating motor 38 penetrates the side wall of one of the fixed plates 8 and is connected to the movable plate 9, the side wall of the movable plate 9 away from the rotating motor 38 is connected to one of the fixed plates 8 through a rotating shaft, a second motor 10 is provided on one side of the movable plate 9, a first screw rod 11 is installed on the execution end of the second motor 10, and one end of the first screw rod 11 penetrates the inner side of the movable plate 9 and is rotatably connected to the movable plate 9, the outer wall of the first screw rod 11 is threadedly connected to the slider 12, a nozzle 37 is installed on the side of the slider 12 away from the first screw rod 11, and the nozzle 37 is connected to the external feeding equipment through the pipeline inside the slider 12. First, the aircraft tail to be sprayed is fixed on the placement plate 4 by a conveying device, and then the linear module 2 (the linear module here is the prior art and will not be described in detail here) and the electric telescopic rod 6 are started to drive the rectangular plate 7 at the bottom of the U-shaped frame 5 to move inside the spraying chamber 1, and then the paint is sent from the pipe inside the slider 12 to the nozzle 37 through the spraying equipment, and the two nozzles 37 are used to spray both sides of the aircraft tail. When the spraying of both sides is completed, the nozzle 37 is moved to the top of the aircraft tail with the cooperation of the linear module 2 and the electric telescopic rod 6, and then the rotating motor 38 located at the top of the aircraft tail is started to drive the movable plate 9 to move on the fixed plate 8 is rotated ninety degrees so that the nozzle 37 rotates toward the top of the aircraft tail wing. While the movable plate 9 is rotating, the second motor 10 is started, and the output end of the second motor 10 drives the first screw 11 to rotate. The first screw 11 drives the slider 12 and the nozzle 37 to move inside the movable plate 9, thereby increasing the distance between the nozzle 37 and the top of the aircraft tail wing. In this way, when the nozzle 37 is spraying the top of the aircraft tail wing, the paint sprayed by the nozzle 37 and the top of the aircraft tail wing will not generate a large impact force to cause a large amount of paint to splash to other parts of the aircraft tail wing, thereby avoiding uneven paint in other parts and improving the spraying effect.

[0020] Example 2 The guard is located at the bottom of 7 and is used to prevent the material sprayed from the nozzle 37 from splashing. The guard includes a slide groove 13 opened on the inner wall of the movable plate 9, a connecting block 14 is installed on one side of the movable plate 9, and the connecting block 14 matches the slide groove 13. A U-shaped rack 15 is installed on the side wall of the connecting block 14. Two connecting seats 16 are fixedly connected to one side of the movable plate 9. The two connecting seats 16 are symmetrically arranged with the central axis of the movable plate 9. A large gear 17 is rotatably connected to one side of each connecting seat 16. The two large gears 17 mesh with the U-shaped rack 15. A small gear 18 is meshed on one side of the large gear 17. A first shaft rod 19 is fixedly connected to one side of the small gear 18. The first shaft rod 19 is rotatably connected to the inner side of the connecting seat 16. The outer wall of the first shaft rod 19 is fixedly connected to a baffle 20. The slider 12 drives the spray head 37 to move toward the inner side of the movable plate 9 and drives the U-shaped rack 15 to move synchronously through the connecting block 14, thereby driving the large gear 17 to rotate, and then driving the small gear 18 to drive the spur gear 30 to rotate toward the side of the aircraft tail through the first shaft 19. When the slider 12 stops moving, the two baffles 20 rotate in an inclined state on both sides of the aircraft tail, thereby blocking the paint splashed by the spray head 37 and the top of the aircraft tail, thereby preventing the splashed paint from flying to other parts of the aircraft tail and causing uneven paint, thereby further improving the uniformity of the aircraft tail spraying; When the spray head 37 is in a horizontal state to spray the side of the aircraft tail, the two baffles 20 initially unfolded at 30 degrees can also play the role of preventing the paint sprayed from the spray head 37 from hitting the aircraft tail to produce splashes.

[0021] Example 3 A bending protection assembly is installed on the side of the baffle 20 away from the connecting seat 16, and the bending protection assembly includes a second limit seat 35 fixedly connected to one end of the baffle 20, and a folding plate 27 is arranged on the inner side of the second limit seat 35. A rotating shaft 36 is fixedly connected to both sides of the folding plate 27, and one end of the rotating shaft 36 passes through the inner side of the second limit seat 35 and is rotatably connected to the second limit seat 35. A torsion spring 40 is installed between the folding plate 27 and the second limit seat 35. The bending protection assembly also includes a fixed A first limiting seat 28 is fixedly connected to the end of the baffle 20, and a second screw rod 31 is rotatably connected to the inner side of the first limiting seat 28. A power block 32 is threadedly connected to the outer wall of the second screw rod 31. One end of the power block 32 is rotatably connected to a roller 33. A spur gear 30 is fixedly connected to the outer wall of the second screw rod 31. A spur rack 29 is meshed with the bottom of the spur gear 30. A toggle assembly for toggling the spur rack 29 to move is provided on the inner side of the first shaft 19. The inner side of the first limiting seat 28 is fixedly connected to the outer wall of the second screw rod 31. A rectangular limit block 34 is connected, and limit slots matching the rectangular limit block 34 are opened on both sides of the power block 32. The power block 32 is slidably connected to the rectangular limit block 34 through the limit slots opened on both sides. The toggle assembly includes a second shaft rod 22 slidably connected to the inner side of the first shaft rod 19, and the outer wall of the second shaft rod 22 is fixedly connected to the connecting rod 26. The inner side of the first shaft rod 19 is opened with a through groove that penetrates to the outside and matches the connecting rod 26. One end of the connecting rod 26 is connected to the spur rack 29. Fixedly connected, one end of the second shaft 22 penetrates through the outer wall of the first shaft 19 and is fixedly connected to a push block 23, a connecting spring 24 is installed between the inner side of the push block 23 and the end of the first shaft 19, the toggle assembly also includes a convex block 39 fixedly connected to one side of the movable plate 9, the inner side of the convex block 39 is fixedly connected to a fitting block 25, the end surface of the fitting block 25 is provided with an arc track, one side of the push block 23 is fixedly connected to a spherical rod 41, and the spherical rod 41 is against the lowest point of the arc track; When the first shaft 19 rotates, the spherical rod 41 rotates along the lowest point to the highest point of the arc track at the end of the fitting block 25, so that the spherical rod 41 is pushed to drive the second shaft 22 to move toward the first shaft 19 under the action of the arc track, thereby driving the spur rack 29 to move toward the spur gear 30 through the connecting rod 26, and then driving the second screw rod 31 to rotate. The second screw rod 31 rotates to drive the power block 32 to drive the roller 33 to move toward the folding plate 27, thereby pushing the folding plate 27 to rotate toward the inside of the baffle 20. When the baffle 20 stops rotating, the roller 33 is close to the side of the aircraft tail, thereby reducing the gap between the baffle 20 and the aircraft tail, thereby better blocking the splashing paint.

[0022] In combination with the above-mentioned spraying machine device for an aircraft tail wing, a method for using a spraying machine for an aircraft tail wing is provided below, which specifically includes the following steps: S1. First, the aircraft tail to be sprayed is fixed on the placement plate 4 by a conveying device, and then the linear module 2 and the electric telescopic rod 6 are started to drive the rectangular plate 7 at the bottom of the U-shaped frame 5 to move inside the spraying chamber 1, and then the paint is sent from the pipe inside the slider 12 to the nozzle 37 through the spraying equipment, and the two nozzles 37 are used to spray both sides of the aircraft tail. When the spraying of both sides is completed, the nozzle 37 is moved to the top of the aircraft tail with the cooperation of the linear module 2 and the electric telescopic rod 6, and then the rotating motor 38 located at the top of the aircraft tail is started to drive the movable plate 9 to rotate ninety degrees on the fixed plate 8, so that The nozzle 37 rotates toward the top of the aircraft tail wing. When the movable plate 9 rotates, the second motor 10 is started. The output end of the second motor 10 drives the first screw 11 to rotate. The first screw 11 drives the slider 12 and the nozzle 37 to move inside the movable plate 9, thereby increasing the distance between the nozzle 37 and the top of the aircraft tail wing. In this way, when the nozzle 37 sprays the top of the aircraft tail wing, the paint sprayed by the nozzle 37 and the top of the aircraft tail wing will not generate a large impact force to cause a large amount of paint to splash to other parts of the aircraft tail wing, thereby avoiding uneven paint in other parts, thereby improving the spraying effect; S2. When the slider 12 drives the spray head 37 to move toward the inside of the movable plate 9, the U-shaped rack 15 is driven to move synchronously through the connecting block 14, thereby driving the large gear 17 to rotate, and then driving the small gear 18 to drive the spur gear 30 to rotate toward the side of the aircraft tail through the first shaft 19. When the slider 12 stops moving, the two baffles 20 are rotated in an inclined state on both sides of the aircraft tail, thereby blocking the paint splashed by the spray head 37 and the top of the aircraft tail, thereby preventing the splashed paint from flying to other parts of the aircraft tail and causing uneven paint, thereby further improving the uniformity of the aircraft tail spraying; S3, when the spray head 37 is in a horizontal state to spray the side of the aircraft tail, the two baffles 20 initially unfolded at 30 degrees can also play the role of preventing the paint sprayed from the spray head 37 from hitting the aircraft tail to produce splashes; S4. When the first shaft 19 rotates, the spherical rod 41 rotates along the lowest point to the highest point of the arc track at the end of the fitting block 25, so that the spherical rod 41 is pushed to drive the second shaft 22 to move toward the first shaft 19 under the action of the arc track, thereby driving the spur rack 29 to move toward the spur gear 30 through the connecting rod 26, and then driving the second screw rod 31 to rotate. The second screw rod 31 rotates to drive the power block 32 to drive the roller 33 to move toward the folding plate 27, thereby pushing the folding plate 27 to rotate toward the inside of the baffle 20. When the baffle 20 stops rotating, the roller 33 is close to the side of the aircraft tail, thereby reducing the gap between the baffle 20 and the aircraft tail, thereby better blocking the splashing paint.

[0023] The above are only preferred specific implementation modes 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 according to the technical solutions and inventive concepts of the present invention within the technical scope disclosed by the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A spraying device for an aircraft tail, characterized in that: include: A spraying chamber (1), wherein a door panel is installed on the side wall of the spraying chamber (1), a linear module (2) is installed on the inner top wall of the spraying chamber (1), a first motor (3) is installed on the outer wall of the spraying chamber (1), an execution end of the first motor (3) passes through the outer wall of the spraying chamber (1) and is connected to a placement plate (4), and the placement plate (4) is rotatably connected to the spraying chamber (1), a U-shaped frame (5) is installed on the execution end of the linear module (2), a plurality of electric telescopic rods (6) are symmetrically embedded at the bottom of the U-shaped frame (5), and the execution ends of the electric telescopic rods (6) are respectively rectangular plates (7); A nozzle (37), wherein the nozzle (37) is arranged at the bottom of the rectangular plate (7); An adjustment mechanism, located at the bottom of each of the two rectangular plates (7), for adjusting the angle between the nozzle (37) and the tail wing of the aircraft; The protector is located at the bottom of the (7) and is used to prevent the material sprayed by the nozzle (37) from splashing.

2. A spraying machine device for an aircraft tail according to claim 1, characterized in that: The adjustment mechanism comprises two fixed plates (8) respectively mounted on the bottom of the rectangular plate (7), wherein a rotating motor (38) is provided on the side wall of one of the fixed plates (8), an execution end of the rotating motor (38) penetrates through the side wall of one of the fixed plates (8) and is connected to a movable plate (9), a side wall of the movable plate (9) away from the rotating motor (38) is connected to one of the fixed plates (8) via a rotating shaft, a second motor (10) is provided on one side of the movable plate (9), a first screw rod (11) is installed on the execution end of the second motor (10), and one end of the first screw rod (11) penetrates through the inner side of the movable plate (9) and is rotatably connected to the movable plate (9), an outer wall of the first screw rod (11) is threadedly connected to a slider (12), a side of the slider (12) away from the first screw rod (11) is installed with the spray head (37), and the spray head (37) is connected to an external feeding device through a pipeline inside the slider (12).

3. A spraying machine device for an aircraft tail according to claim 2, characterized in that: The guard comprises a slide groove (13) provided on the inner wall of the movable plate (9); a connecting block (14) is installed on one side of the movable plate (9), and the connecting block (14) matches the slide groove (13); a U-shaped rack (15) is installed on the side wall of the connecting block (14); two connecting seats (16) are fixedly connected to one side of the movable plate (9); the two connecting seats (16) are symmetrically arranged with respect to the central axis of the movable plate (9); and one side of each connecting seat (16) is rotatable. A large gear (17) is connected, the two large gears (17) mesh with the U-shaped rack (15), one side of the large gear (17) meshes with a small gear (18), one side of the small gear (18) is fixedly connected to a first shaft (19), the first shaft (19) is rotatably connected to the inner side of the connecting seat (16), the outer wall of the first shaft (19) is fixedly connected to a baffle (20), and a bending protection component is installed on the side of the baffle (20) away from the connecting seat (16).

4. A spraying machine device for an aircraft tail according to claim 3, characterized in that: The bending protection assembly comprises a second limit seat (35) fixedly connected to one end of the baffle (20); a folding plate (27) is arranged on the inner side of the second limit seat (35); a rotating shaft (36) is fixedly connected to both sides of the folding plate (27); one end of the rotating shaft (36) passes through the inner side of the second limit seat (35) and is rotatably connected to the second limit seat (35); and a torsion spring (40) is installed between the folding plate (27) and the second limit seat (35).

5. A spraying machine device for an aircraft tail according to claim 4, characterized in that: The bending protection component further comprises a first limit seat (28) fixedly connected to the end of the baffle (20); a second screw rod (31) is rotatably connected to the inner side of the first limit seat (28); a power block (32) is threadedly connected to the outer wall of the second screw rod (31); a roller (33) is rotatably connected to one end of the power block (32); a spur gear (30) is fixedly connected to the outer wall of the second screw rod (31); a spur gear (29) is meshed with the bottom of the spur gear (30); and a toggle assembly for toggling the spur gear (29) to move is provided on the inner side of the first shaft rod (19).

6. A spraying machine device for an aircraft tail according to claim 5, characterized in that: A rectangular limit block (34) is fixedly connected to the inner side of the first limit seat (28), and limit slide grooves matching the rectangular limit block (34) are provided on both sides of the power block (32). The power block (32) is slidably connected to the rectangular limit block (34) via the limit slide grooves provided on both sides.

7. A spraying machine device for an aircraft tail according to claim 6, characterized in that: The toggle assembly comprises a second shaft (22) slidably connected to the inner side of the first shaft (19); a connecting rod (26) is fixedly connected to the outer wall of the second shaft (22); a through groove extending to the outside and matching the connecting rod (26) is provided on the inner side of the first shaft (19); one end of the connecting rod (26) is fixedly connected to the spur rack (29); one end of the second shaft (22) extends through the outer wall of the first shaft (19) and is fixedly connected to a push block (23); a connecting spring (24) is installed between the inner side of the push block (23) and the end of the first shaft (19).

8. A spraying device for an aircraft tail according to claim 7, characterized in that: The toggle assembly further comprises a convex block (39) fixedly connected to one side of the movable plate (9), a mating block (25) fixedly connected to the inner side of the convex block (39), an end surface of the mating block (25) being provided with an arc track, and a spherical rod (41) fixedly connected to one side of the push block (23), and the spherical rod (41) abuts against the lowest point of the arc track.

9. A method for using a spraying machine for an aircraft tail, characterized in that: The spraying device for an aircraft tail wing according to claim 7 comprises the following steps: S1. First, the aircraft tail to be sprayed is fixed on the placement plate (4) by a conveying device, then the linear module (2) and the electric telescopic rod (6) are started to drive the rectangular plate (7) at the bottom of the U-shaped frame (5) to move inside the spraying chamber (1), and then the paint is sent from the pipeline inside the slider (12) to the spray head (37) by the spraying device, and the two spray heads (37) spray the two sides of the aircraft tail. When the spraying of both sides is completed, the linear module (2) and the electric telescopic rod (6) are cooperated to move the spray head (37) to the top of the aircraft tail, and then the rotating motor (38) located at the top of the aircraft tail is started to drive the movable plate (9) to rotate on the fixed plate (8). The movable plate (9) is rotated by 90 degrees, so that the spray head (37) rotates toward the top of the aircraft tail wing. When the movable plate (9) rotates, the second motor (10) is started, and the output end of the second motor (10) drives the first screw rod (11) to rotate. The first screw rod (11) drives the slider (12) and the spray head (37) to move inside the movable plate (9), thereby increasing the distance between the spray head (37) and the top of the aircraft tail wing. When the spray head (37) sprays the top of the aircraft tail wing, the paint sprayed by the spray head (37) and the top of the aircraft tail wing will not generate a large impact force, causing a large amount of paint to splash onto other parts of the aircraft tail wing, thereby avoiding uneven paint in other parts, thereby improving the spraying effect; S2, when the slider (12) drives the spray head (37) to move toward the inside of the movable plate (9), the U-shaped rack (15) is driven to move synchronously through the connecting block (14), thereby driving the large gear (17) to rotate, and then driving the small gear (18) to drive the spur gear (30) to rotate toward the side of the aircraft tail through the first shaft (19); when the slider (12) stops moving, the two baffles (20) rotate in an inclined state on both sides of the aircraft tail, thereby blocking the paint sprayed by the spray head (37) and colliding with the top of the aircraft tail to generate splashes, thereby preventing the splashed paint from flying to other parts of the aircraft tail and causing uneven paint, thereby further improving the uniformity of the aircraft tail spraying; S3, when the spray head (37) is in a horizontal state and is spraying the side of the aircraft tail wing, the two baffles (20) initially spread out at a thirty-degree angle can also play a role in preventing the paint sprayed from the spray head (37) from hitting the aircraft tail wing and generating splashes; S4. When the first shaft (19) rotates, the spherical rod (41) rotates along the lowest point of the arc track at the end of the fitting block (25) toward the highest point, so that the spherical rod (41) is pushed under the action of the arc track to drive the second shaft (22) to move toward the first shaft (19), thereby driving the spur rack (29) to move toward the spur gear (30) through the connecting rod (26), thereby driving the second screw rod (31) to rotate. The second screw rod (31) rotates to drive the power block (32) to drive the roller (33) to move toward the folding plate (27), thereby pushing the folding plate (27) to rotate toward the inside of the baffle (20). When the baffle (20) stops rotating, the roller (33) is close to the side of the aircraft tail, thereby reducing the gap between the baffle (20) and the aircraft tail, thereby better blocking the splashed paint.

Images