Processing device for metal bracket of aviation seat

Abstract

The application relates to the technical field of aviation seat metal support processing, and discloses a processing device for aviation seat metal supports, which comprises a machine tool, a movable door is slidably connected to the surface of the machine tool, a polishing device is arranged on the inner wall of the machine tool, a processing device is arranged in the machine tool, a filter plate is fixedly connected to the inner wall of the machine tool, and a clamping component is arranged in the machine tool; the clamping component comprises a sliding groove plate, the surface of the sliding groove plate is fixedly connected with the inner wall of the machine tool, a power device is fixedly connected to the end of the sliding groove plate, and a threaded rod is fixedly connected to the output end of the power device. When the adjusting frame moves, the ball-shaped rod pushes the extrusion ring to move, the extrusion ring extrudes the inclined frame when moving, the inclined frame moves to the inside of the limiting frame after being extruded, the inclined plate extrudes and fixes the aviation seat metal support along with the movement of the inclined frame, the stability of the aviation seat metal support during processing is improved, and the aviation seat metal support can be clamped and fixed in the inside of the sleeve by twisting the adjusting frame.

Description

Technical Field

[0001] This invention relates to the field of metal bracket processing technology for aircraft seats, specifically to a processing device for metal brackets for aircraft seats. Background Technology

[0002] Aviation seats are designed specifically for aviation safety and comfort, and are widely used in aircraft, automobiles and special equipment. Aviation seats refer to widened seats that are derived from the design of first class cabins of aircraft, equipped with independent armrests and leg rests, and can be converted into reclining chairs. They are now widely used in the fields of aircraft and luxury cars, emphasizing multifunctionality, comfort and ergonomic support. Aviation seats must pass the 16G dynamic impact test and flame retardant certification. During the production of aircraft seats, the metal frame needs to be processed by machine tools. Some metal frame parts may develop rust during transportation or storage. Rust will cause changes in the surface roughness of the workpiece, which will lead to changes in the cutting resistance of the machine tool and affect the stability of the feed. Summary of the Invention

[0003] The purpose of this invention is to provide a processing apparatus for metal brackets for aircraft seats, so as to solve the problems mentioned in the background art.

[0004] To solve the above-mentioned technical problems, the present invention is achieved through the following technical solution: This invention relates to a processing device for metal brackets of aircraft seats, comprising a machine tool, a sliding door slidably connected to the surface of the machine tool, a grinding device provided on the inner wall of the machine tool, a processing device provided inside the machine tool, a filter plate fixedly connected to the inner wall of the machine tool, and a clamping component provided inside the machine tool. The clamping component includes a slide plate, the surface of which is fixedly connected to the inner wall of the machine tool. A power device is fixedly connected to one end of the slide plate, and a threaded rod is fixedly connected to the output end of the power device. A movable frame is slidably connected to the surface of the slide plate, and the surface of the threaded rod is threadedly connected to the inner wall of the movable frame. A mounting plate is fixedly connected to the surface of the movable frame, and a drive device is fixedly connected to the surface of the mounting plate. A support rod is fixedly connected to the output end of the drive device. A turntable is fixedly connected to the end of the support rod away from the drive device, and a sleeve is fixedly connected to the end of the turntable away from the support rod. The surface of the machine tool is fixedly connected to a limiting frame. A spring rod is fixedly connected to the inner wall of the limiting frame. An inclined plate is fixedly connected to the end of the spring rod away from the limiting frame. An inclined frame is fixedly connected to the end of the inclined plate near the spring rod. A threaded cylinder is fixedly connected to the surface of the turntable. An adjusting frame is threadedly connected to the surface of the threaded cylinder. A ball rod is fixedly connected to the surface of the adjusting frame. A compression ring is slidably connected to the surface of the ball rod. An aviation seat metal bracket is installed inside the sleeve. A pushing component is installed below the slide plate. A storage component is installed at the bottom of the filter plate. A cooling component is installed inside the machine tool.

[0005] Furthermore, the grinding device and the processing device are symmetrically arranged with the machine tool as the center. The slide plate is located at the end of the machine tool away from the grinding device. The mounting plate is set at a right angle. The inner wall of the moving frame is slidably connected to the inner wall of the slide plate. The end of the support rod away from the driving device passes through the mounting plate and extends to the outer end of the mounting plate. The surface of the support rod is rotatably connected to the inner wall of the mounting plate.

[0006] Furthermore, the end of the threaded rod away from the power device passes through the slide plate and is rotatably connected to the inner wall of the slide plate. The number of inclined plates is four, and the four inclined plates are arranged circumferentially around the sleeve. The inclined surface of the inclined plate is located at the end of the sleeve away from the turntable.

[0007] Furthermore, the end of the inclined frame away from the inclined panel passes through the limiting frame and extends to the outer end of the limiting frame, the end of the inclined panel away from the inclined frame contacts the surface of the metal bracket of the aircraft seat, the compression ring is located at the end of the spherical rod away from the adjusting frame, and the inner wall of the compression ring contacts the surface of the inclined frame.

[0008] Furthermore, the pushing component includes a positioning rod, the end of which is fixedly connected to the inner wall of the machine tool, a pushing plate is slidably connected to the surface of the positioning rod, a tripod is rotatably connected to the surface of the pushing plate, a spring is hinged to the center of the tripod, and a roller extrusion frame is fixedly connected to the bottom of the moving frame.

[0009] Furthermore, there are two pusher plates, which are symmetrically arranged around the positioning rod. The bottom of the pusher plate contacts the top of the filter plate, the top of the tripod contacts the bottom of the slide plate, and the roller extrusion frame is located above the pusher plate.

[0010] Furthermore, the storage component includes a linkage rod, the upper surface of which is hinged to the center of the tripod. An elastic frame is fixedly connected to the bottom of the linkage rod, and a triangular plate is fixedly connected to the bottom of the elastic frame. A sieve storage rack is fixedly connected to the inner wall of the filter plate, and an elastic telescopic rod is fixedly connected to the inner wall of the sieve storage rack. A through-hole extrusion plate is fixedly connected to the end of the elastic telescopic rod away from the sieve storage rack, and an opening and closing door is hinged to the end of the sieve storage rack.

[0011] Furthermore, the number of through-hole extrusion plates is set to six, and the six through-hole extrusion plates are set to three groups, with two in each group. The number of sieve storage racks is set to three, and the three groups of through-hole extrusion plates are respectively located inside the three sieve storage racks. The triangular plate is located at the end of the two through-hole extrusion plates that are close to each other, and the bottom of the through-hole extrusion plate is in contact with the bottom of the inner wall of the sieve storage rack.

[0012] Furthermore, the cooling component includes a water pump, the bottom of which is fixedly connected to the bottom of the inner wall of the machine tool. The output end of the water pump is connected to a bend pipe, and the end of the bend pipe away from the water pump is slidably connected to a moving pipe. The end of the moving pipe away from the bend pipe is connected to a transfer pipe, and the end of the transfer pipe away from the moving pipe is connected to a spray frame.

[0013] Furthermore, the end of the bend away from the water pump extends above the chute plate, the bottom of the movable pipe is fixedly connected to the top of the movable frame, and the spraying frame is tilted towards the direction of the aircraft seat metal bracket.

[0014] The present invention has the following beneficial effects: When processing the metal bracket of an aircraft seat, the present invention starts the power unit to drive the threaded rod to rotate inside the slide plate. As the threaded rod rotates, it pushes the moving frame on the surface of the slide plate via the thread. During movement, the moving frame pushes the turntable towards the center of the machine tool via the mounting plate, facilitating the operator to install the aircraft seat metal bracket inside the sleeve. When the aircraft seat metal bracket enters the inner wall of the sleeve, it is pushed by the inclined surface of the inclined plate to compress the elastic rod. At this time, the inclined plate utilizes the elasticity of the elastic rod to compress and fix the aircraft seat metal bracket, improving the stability of the aircraft seat metal bracket after insertion into the sleeve and preventing it from falling off during fixing. After placing the aircraft seat metal bracket inside the sleeve, the operator twists the adjusting frame to rotate on the surface of the threaded cylinder. During rotation, the adjusting frame moves towards the sleeve via the thread. During movement, the adjusting frame pushes the compression ring to move via the ball rod. The compression ring compresses the inclined frame during movement, causing the inclined frame to move inwards towards the limiting frame. The inclined plate, along with the movement of the inclined frame, compresses and fixes the aircraft seat metal bracket, improving the stability of the aircraft seat metal bracket during processing. The metal bracket of the aircraft seat can be clamped and fixed inside the sleeve by twisting the adjustment bracket, improving the convenience of installation. After the metal bracket is adjusted, the position of the turntable is adjusted by the forward and reverse rotation of the power unit. After the metal bracket is adjusted to correspond with the grinding device, the grinding device is started to grind the surface of the metal bracket to avoid rust affecting the processing accuracy. The grinding position of the metal bracket is adjusted by the threaded rod to perform comprehensive grinding. When the metal bracket needs to be flipped, the drive unit is started to drive the support rod to rotate inside the mounting plate. The rotation of the support rod drives the turntable to rotate, thereby adjusting the grinding surface of the metal bracket and improving the processing accuracy of the metal bracket. After the metal bracket is processed, the threaded rod pushes the metal bracket to the processing position of the processing device for processing.

[0015] When the movable frame of this invention moves, it drives the roller extrusion frame to move as well. The roller extrusion frame contacts the surface of the tripod during movement, and as it moves, the center of the extrusion tripod moves downwards. This downward movement of the tripod's center pushes the pusher plates away from each other. The pusher plates clean the impurities on the top of the filter plate, pushing them into the sieve storage rack for storage, preventing them from clogging the filter plate and affecting the circulation of coolant. When the roller extrusion frame separates from the tripod, the tripod uses the elasticity of its springs to reset, pulling the pusher plates closer together. The pusher plates clean the impurities on the top of the filter plate, allowing them to enter the sieve storage rack for centralized storage, thus improving the convenience of waste disposal.

[0016] This invention features an opening and closing door at the end of the sieve storage rack, facilitating the handling of waste materials inside the rack. When the center of the tripod moves downwards, it pushes the elastic frame to move via a connecting rod. This movement pushes the triangular plate against the through-hole extrusion plate, which in turn compresses the waste materials inside the rack. This allows the coolant in the waste to quickly enter the machine tool for circulation. The extrusion plate also compacts the waste, improving the storage efficiency of the sieve storage rack. The connection between the elastic frame and the triangular plate allows the connecting rod to contract due to the elasticity of the frame, preventing waste materials from affecting the tripod's operation. The water pump is then started, drawing coolant into the curved pipe. Through the curved pipe and the moving pipe, the coolant is transferred to the spraying frame, which sprays the coolant onto the surface of the aircraft seat's metal frame for cooling. The moving pipe moves synchronously with the moving frame, further enhancing the cooling effect on the aircraft seat's metal frame.

[0017] Of course, any product implementing this invention does not necessarily need to achieve all of the advantages described above at the same time. Attached Figure Description

[0018] To more clearly illustrate the technical solutions of the embodiments of the present invention, the accompanying drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0019] Figure 1 This is a schematic diagram of the overall structure of the present invention; Figure 2 This is a schematic diagram of the filter plate structure of the present invention; Figure 3 This is a schematic cross-sectional view of the machine tool of the present invention; Figure 4This is a schematic diagram of the overall structure of the clamping component of the present invention; Figure 5 This is a schematic diagram of another structure of the clamping component of the present invention; Figure 6 This is a schematic diagram of the overall structure of the feeding component of the present invention; Figure 7 This is another structural schematic diagram of the feeding component of the present invention; Figure 8 This is a schematic diagram of the overall structure of the storage component of the present invention; Figure 9 This is a schematic diagram of the overall structure of the cooling component of the present invention.

[0020] The following is a list of components represented by each label in the attached diagram: In the diagram: 1. Machine tool; 2. Sliding door; 3. Grinding device; 4. Machining device; 5. Filter plate; 6. Metal frame for aircraft seat; 7. Clamping component; 8. Pushing component; 9. Storage component; 10. Cooling component; 20. Slide plate; 21. Threaded rod; 22. Moving frame; 23. Power unit; 24. Drive unit; 25. Turntable; 26. Sleeve; 27. Mounting plate; 28. Threaded cylinder; 29. ​​Support rod; 30. Adjusting frame; 31. Extrusion ring; 32. Spherical rod; 33. Limiting frame; 34. Inclined panel; 35. Inclined frame; 36. Elastic rod; 40. Positioning rod; 41. Push plate; 42. Triangular frame; 43. Spring plate; 44. Roller extrusion frame; 50. Linking rod; 51. Elastic frame; 52. Triangular plate; 53. Screen hole storage rack; 54. Elastic telescopic rod; 55. Opening and closing door; 56. Through hole extrusion plate; 60. Water pump; 61. Bend; 62. Moving pipe; 63. Transfer pipe; 64. Spraying frame. Detailed Implementation

[0021] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0022] Please see Figures 1-9 As shown, the present invention is a processing device for metal brackets of aircraft seats, including a machine tool 1, a movable door 2 slidably connected to the surface of the machine tool 1, a grinding device 3 provided on the inner wall of the machine tool 1, a processing device 4 provided inside the machine tool 1, a filter plate 5 fixedly connected to the inner wall of the machine tool 1, and a clamping component 7 provided inside the machine tool 1. The clamping component 7 includes a slide plate 20, the surface of which is fixedly connected to the inner wall of the machine tool 1. A power unit 23 is fixedly connected to the end of the slide plate 20, and a threaded rod 21 is fixedly connected to the output end of the power unit 23. A movable frame 22 is slidably connected to the surface of the slide plate 20, and the surface of the threaded rod 21 is threadedly connected to the inner wall of the movable frame 22. A mounting plate 27 is fixedly connected to the surface of the movable frame 22, and a drive unit 24 is fixedly connected to the surface of the mounting plate 27. The output end of the drive unit 24 is fixedly connected to... A support rod 29 is connected to a turntable 25 at the end of the support rod 29 away from the drive device 24. A sleeve 26 is fixedly connected to the end of the turntable 25 away from the support rod 29. A limit frame 33 is fixedly connected to the surface of the sleeve 26. A spring rod 36 is fixedly connected to the inner wall of the limit frame 33. An inclined plate 34 is fixedly connected to the end of the spring rod 36 away from the limit frame 33. An inclined frame 35 is fixedly connected to the end of the inclined plate 34 near the spring rod 36. A threaded cylinder 28 is fixedly connected to the surface of the turntable 25. The surface of sleeve 26 is threaded with an adjusting bracket 30. The surface of the adjusting bracket 30 is fixedly connected with a ball rod 32. The surface of the ball rod 32 is slidably connected with a compression ring 31. The interior of sleeve 26 is equipped with an aircraft seat metal bracket 6. When the aircraft seat metal bracket 6 needs to be processed, the power unit 23 is started to drive the threaded rod 21 to rotate inside the slide plate 20. When the threaded rod 21 rotates, it pushes the moving frame 22 to move on the surface of the slide plate 20 through the thread. When the moving frame 22 moves, it pushes the turntable 25 to move towards the center of the machine tool 1 through the mounting plate 27, so that the operator can install the aircraft seat metal bracket 6 inside the sleeve 26. When the aircraft seat metal bracket 6 enters the inner wall of sleeve 26, it is pushed by the inclined surface of the inclined plate 34 to squeeze the elastic rod 36. At this time, the inclined plate 34 will use the elasticity of the elastic rod 36 to squeeze and fix the aircraft seat metal bracket 6. A pushing component 8 is provided below the slide plate 20, a storage component 9 is provided at the bottom of the filter plate 5, and a cooling component 10 is provided inside the machine tool 1.

[0023] The grinding device 3 and the processing device 4 are symmetrically arranged around the machine tool 1. The slide plate 20 is located at the end of the machine tool 1 away from the grinding device 3. The mounting plate 27 is set at a right angle. The inner wall of the moving frame 22 is slidably connected to the inner wall of the slide plate 20. The end of the support rod 29 away from the drive device 24 passes through the mounting plate 27 and extends to the outer end of the mounting plate 27. The surface of the support rod 29 is rotatably connected to the inner wall of the mounting plate 27. After the metal bracket 6 of the aviation seat is placed inside the sleeve 26, the operator twists the adjusting bracket 30 to rotate on the surface of the threaded cylinder 28. The adjusting bracket 30 rotates... When moving, the adjusting bracket 30 moves towards the sleeve 26 via the thread. When moving, the adjusting bracket 30 pushes the extrusion ring 31 to move via the ball rod 32. When moving, the extrusion ring 31 will extrude the inclined bracket 35. After being extruded, the inclined bracket 35 moves into the interior of the limiting bracket 33. The inclined panel 34 extrudes and fixes the aircraft seat metal bracket 6 as the inclined bracket 35 moves, improving the stability of the aircraft seat metal bracket 6 during processing. Twisting the adjusting bracket 30 can clamp and fix the aircraft seat metal bracket 6 inside the sleeve 26, improving the convenience of installation of the aircraft seat metal bracket 6.

[0024] The end of the threaded rod 21 away from the power device 23 passes through the slide plate 20 and is rotatably connected to the inner wall of the slide plate 20. There are four inclined plates 34, which are arranged circumferentially around the sleeve 26. The inclined surface of the inclined plate 34 is located at the end of the sleeve 26 away from the turntable 25.

[0025] The end of the slant bracket 35 away from the slant panel 34 passes through the limit frame 33 and extends to the outer end of the limit frame 33. The end of the slant panel 34 away from the slant bracket 35 contacts the surface of the aircraft seat metal support 6. The compression ring 31 is located at the end of the ball rod 32 away from the adjustment frame 30. The inner wall of the compression ring 31 contacts the surface of the slant bracket 35.

[0026] The feeding component 8 includes a positioning rod 40, the end of which is fixedly connected to the inner wall of the machine tool 1. A feeding plate 41 is slidably connected to the surface of the positioning rod 40. A tripod 42 is rotatably connected to the surface of the feeding plate 41. A spring piece 43 is hinged to the center of the tripod 42. A roller extrusion frame 44 is fixedly connected to the bottom of the moving frame 22. When the moving frame 22 moves, it will drive the roller extrusion frame 44 to move. When the roller extrusion frame 44 moves, it will contact the surface of the tripod 42. As it moves, it will extrude the center of the tripod 42 downward. When the center of the tripod 42 moves downward, the end of it will push the feeding plate 41 to move away from each other. When the feeding plate 41 moves, it will clean the impurities on the top of the filter plate 5. The feeding plate 41 pushes the impurities into the interior of the sieve storage rack 53 for storage.

[0027] There are two pusher plates 41, which are symmetrically arranged around the positioning rod 40. The bottom of the pusher plate 41 contacts the top of the filter plate 5, and the top of the tripod 42 contacts the bottom of the slide plate 20. The roller extrusion frame 44 is located above the pusher plate 41. When the roller extrusion frame 44 separates from the tripod 42, the tripod 42 is reset by the elasticity of the spring piece 43. During the reset, the pusher plate 41 is pulled to move closer to each other, and the impurities on the top of the filter plate 5 are cleaned by the pusher plate 41.

[0028] Storage component 9 includes a linkage rod 50, the upper surface of which is hinged to the center of the tripod 42. An elastic frame 51 is fixedly connected to the bottom of the linkage rod 50, and a triangular plate 52 is fixedly connected to the bottom of the elastic frame 51. A sieve storage rack 53 is fixedly connected to the inner wall of the filter plate 5, and an elastic telescopic rod 54 is fixedly connected to the inner wall of the sieve storage rack 53. A through-hole pressing plate 56 is fixedly connected to the end of the elastic telescopic rod 54 away from the sieve storage rack 53. An opening and closing door 55 is hinged to the end of the sieve storage rack 53. The end of the frame 53 is provided with an opening and closing door 55, which facilitates the processing of waste inside the sieve storage rack 53 through the opening and closing door 55. When the center of the tripod 42 moves downward, it pushes the elastic frame 51 to move through the linkage rod 50. When the elastic frame 51 moves, it pushes the tripod 52 to squeeze the through hole extrusion plate 56. When the through hole extrusion plate 56 moves, it will squeeze the waste inside the sieve storage rack 53, so that the coolant in the waste can quickly enter the machine tool for internal circulation and reuse. The through hole extrusion plate 56 will also compact the waste.

[0029] There are six through-hole extrusion plates 56, which are arranged in three groups, with two plates in each group. There are three sieve storage racks 53. The three groups of through-hole extrusion plates 56 are located inside the three sieve storage racks 53 respectively. The triangular plate 52 is located at the end of the two through-hole extrusion plates 56 that are close to each other. The bottom of the through-hole extrusion plate 56 is in contact with the bottom of the inner wall of the sieve storage rack 53.

[0030] The cooling component 10 includes a water pump 60. The bottom of the water pump 60 is fixedly connected to the bottom of the inner wall of the machine tool 1. The output end of the water pump 60 is connected to a bend pipe 61. The end of the bend pipe 61 away from the water pump 60 is slidably connected to a moving pipe 62. The end of the moving pipe 62 away from the bend pipe 61 is connected to a transfer pipe 63. The end of the transfer pipe 63 away from the moving pipe 62 is connected to a spray frame 64. When the water pump 60 is started, it will draw coolant into the interior of the bend pipe 61 and transfer the coolant to the interior of the spray frame 64 through the bend pipe 61 and the moving pipe 62. At this time, the spray frame 64 will spray the coolant onto the surface of the metal support frame 6 of the aircraft seat to cool it down.

[0031] The end of the bend 61 away from the water pump 60 extends above the slide plate 20, the bottom of the moving pipe 62 is fixedly connected to the top of the moving frame 22, and the spray frame 64 is tilted towards the direction of the aircraft seat metal bracket 6.

[0032] When the metal bracket 6 of the aircraft seat needs to be processed, the power unit 23 is started to drive the threaded rod 21 to rotate inside the slide plate 20. When the threaded rod 21 rotates, it pushes the moving frame 22 to move on the surface of the slide plate 20 through the thread. When the moving frame 22 moves, it pushes the turntable 25 to move towards the center of the machine tool 1 through the mounting plate 27, so that the operator can install the metal bracket 6 of the aircraft seat inside the sleeve 26. When the metal bracket 6 of the aircraft seat enters the inner wall of the sleeve 26, it is pushed by the inclined surface of the inclined plate 34 to squeeze the elastic rod 36. At this time, the inclined plate 34 will use the elasticity of the elastic rod 36 to squeeze the metal bracket 6 of the aircraft seat. To improve the stability of the aircraft seat metal bracket 6 after it is inserted into the sleeve 26 and to prevent it from falling off during fixation, the operator rotates the adjusting bracket 30 on the surface of the threaded cylinder 28 after placing the aircraft seat metal bracket 6 inside the sleeve 26. During rotation, the adjusting bracket 30 moves towards the sleeve 26 via the thread. As it moves, the adjusting bracket 30 pushes the compression ring 31 through the ball rod 32. The compression ring 31 compresses the inclined frame 35 during its movement, causing the inclined frame 35 to move inwards towards the limiting frame 33. The inclined panel 34, along with the movement of the inclined frame 35, compresses and fixes the aircraft seat metal bracket 6, improving the stability of the aircraft seat. To ensure the stability of the metal support frame 6 during processing, the adjusting bracket 30 can be twisted to clamp and fix the metal support frame 6 inside the sleeve 26, improving the ease of installation. After adjusting the metal support frame 6, the position of the turntable 25 is adjusted by the forward and reverse rotation of the power device 23. After adjusting the metal support frame 6 to correspond with the grinding device 3, the grinding device 3 is started to grind the surface of the metal support frame 6 to avoid rust affecting its processing accuracy. The grinding position of the metal support frame 6 is adjusted using the threaded rod 21 to facilitate grinding. When a comprehensive grinding process is required and the metal support frame 6 of the aircraft seat needs to be flipped, the drive device 24 is activated to drive the support rod 29 to rotate inside the mounting plate 27. The rotation of the support rod 29 drives the turntable 25 to rotate, thereby using the turntable 25 to adjust the grinding surface of the metal support frame 6 of the aircraft seat, thereby improving the processing accuracy of the processing device 4 on the metal support frame 6 of the aircraft seat and avoiding the presence of rust on the surface of the metal support frame 6 of the aircraft seat that would affect the processing accuracy of the processing device 4. After the processing of the metal support frame 6 of the aircraft seat is completed, the threaded rod 21 pushes the metal support frame 6 of the aircraft seat to the processing area of ​​the processing device 4, and the processing device 4 processes it. When the moving frame 22 moves, it drives the roller extrusion frame 44 to move. The roller extrusion frame 44 contacts the surface of the tripod 42 when it moves. As the center of the moving extrusion tripod 42 moves downward, the end of the tripod 42 pushes the pusher plate 41 to move away from each other. When the pusher plate 41 moves, it cleans the impurities on the top of the filter plate 5. The pusher plate 41 pushes the impurities into the interior of the sieve storage rack 53 for storage, so as to prevent the impurities from clogging the filter plate 5 and affecting the circulation of the coolant. When the roller extrusion frame 44 separates from the tripod 42, the tripod 42 returns to its original position using the elasticity of the spring piece 43. When it returns to its original position, it pulls the pusher plate 41 to move closer to each other. The pusher plate 41 cleans the impurities on the top of the filter plate 5 so that the impurities can enter the interior of the sieve storage rack 53 for centralized storage, which improves the convenience of waste disposal. An opening and closing door 55 is provided at the end of the sieve storage rack 53 to facilitate the processing of waste material inside the sieve storage rack 53. When the center of the tripod 42 moves downward, it pushes the elastic frame 51 to move through the connecting rod 50. When the elastic frame 51 moves, it pushes the tripod 52 to squeeze the through-hole extrusion plate 56. When the through-hole extrusion plate 56 moves, it squeezes the waste material inside the sieve storage rack 53, allowing the coolant in the waste material to quickly enter the machine tool for internal circulation. The through-hole extrusion plate 56 also compacts the waste material, improving the storage effect of the sieve storage rack 53. A pair of triangular plates 52 are connected, allowing the linkage rod 50 to contract due to the elasticity of the elastic frame 51. This prevents waste material inside the sieve storage rack 53 from affecting the operation of the triangular frame 42. The water pump 60 is started to begin operation. The water pump 60 draws coolant into the inside of the bent pipe 61. The coolant is then transferred to the inside of the spray frame 64 through the bent pipe 61 and the moving pipe 62. At this time, the spray frame 64 sprays the coolant onto the surface of the aircraft seat metal bracket 6 to cool it down. The moving pipe 62 moves synchronously with the moving frame 22, further improving the cooling effect on the aircraft seat metal bracket 6.

[0033] The preferred embodiments of the present invention disclosed above are merely illustrative of the invention. These preferred embodiments do not exhaustively describe all details, nor do they limit the invention to the specific implementations described. Clearly, many modifications and variations can be made based on the content of this specification. This specification selects and specifically describes these embodiments to better explain the principles and practical applications of the invention, thereby enabling those skilled in the art to better understand and utilize the invention. The invention is limited only by the claims and their full scope and equivalents.

Claims

1. A processing device for a metal bracket of an aircraft seat, comprising a machine tool (1), a movable door (2) slidably connected to the surface of the machine tool (1), a grinding device (3) provided on the inner wall of the machine tool (1), a processing device (4) provided inside the machine tool (1), and a filter plate (5) fixedly connected to the inner wall of the machine tool (1), characterized in that, The machine tool (1) is equipped with a clamping component (7) inside; The clamping component (7) includes a slide plate (20), the surface of which is fixedly connected to the inner wall of the machine tool (1), a power device (23) is fixedly connected to the end of the slide plate (20), a threaded rod (21) is fixedly connected to the output end of the power device (23), a movable frame (22) is slidably connected to the surface of the slide plate (20), the surface of the threaded rod (21) is threadedly connected to the inner wall of the movable frame (22), a mounting plate (27) is fixedly connected to the surface of the movable frame (22), a driving device (24) is fixedly connected to the surface of the mounting plate (27), a support rod (29) is fixedly connected to the output end of the driving device (24), a turntable (25) is fixedly connected to the end of the support rod (29) away from the driving device (24), and a sleeve (26) is fixedly connected to the end of the turntable (25) away from the support rod (29). 6) The surface is fixedly connected to a limiting frame (33), the inner wall of the limiting frame (33) is fixedly connected to a spring rod (36), the end of the spring rod (36) away from the limiting frame (33) is fixedly connected to a slanted panel (34), the end of the slanted panel (34) near the spring rod (36) is fixedly connected to a slanted frame (35), the surface of the turntable (25) is fixedly connected to a threaded cylinder (28), the surface of the threaded cylinder (28) is threadedly connected to an adjusting frame (30), the surface of the adjusting frame (30) is fixedly connected to a ball rod (32), the surface of the ball rod (32) is slidably connected to a compression ring (31), the inside of the sleeve (26) is provided with an aviation seat metal bracket (6), the bottom of the slide plate (20) is provided with a pushing component (8), the bottom of the filter plate (5) is provided with a storage component (9), and the inside of the machine tool (1) is provided with a cooling component (10).

2. The processing apparatus for a metal bracket for an aircraft seat according to claim 1, characterized in that: The grinding device (3) and the processing device (4) are symmetrically arranged with the machine tool (1) as the center. The slide plate (20) is located at the end of the machine tool (1) away from the grinding device (3). The mounting plate (27) is set at a right angle. The inner wall of the moving frame (22) is slidably connected to the inner wall of the slide plate (20). The end of the support rod (29) away from the drive device (24) passes through the mounting plate (27) and extends to the outer end of the mounting plate (27). The surface of the support rod (29) is rotatably connected to the inner wall of the mounting plate (27).

3. The processing apparatus for a metal bracket for an aircraft seat according to claim 2, characterized in that: The threaded rod (21) is located away from the power device (23) at one end, which passes through the slide plate (20) and is rotatably connected to the inner wall of the slide plate (20). There are four inclined plates (34), which are arranged circumferentially around the sleeve (26). The inclined surface of the inclined plate (34) is located at the end of the sleeve (26) away from the turntable (25).

4. The processing apparatus for a metal bracket for an aircraft seat according to claim 3, characterized in that: The end of the inclined frame (35) away from the inclined panel (34) passes through the limiting frame (33) and extends to the outer end of the limiting frame (33). The end of the inclined panel (34) away from the inclined frame (35) is in contact with the surface of the aircraft seat metal bracket (6). The compression ring (31) is located at the end of the ball rod (32) away from the adjusting frame (30). The inner wall of the compression ring (31) is in contact with the surface of the inclined frame (35).

5. The processing apparatus for a metal bracket for an aircraft seat according to claim 4, characterized in that: The pushing component (8) includes a positioning rod (40), the end of which is fixedly connected to the inner wall of the machine tool (1). A pushing plate (41) is slidably connected to the surface of the positioning rod (40), and a triangular frame (42) is rotatably connected to the surface of the pushing plate (41). A spring piece (43) is hinged to the center of the triangular frame (42), and a roller extrusion frame (44) is fixedly connected to the bottom of the moving frame (22).

6. The processing apparatus for a metal bracket for an aircraft seat according to claim 5, characterized in that: There are two pusher plates (41). The two pusher plates (41) are symmetrically arranged with the positioning rod (40) as the center. The bottom of the pusher plate (41) is in contact with the top of the filter plate (5). The top of the tripod (42) is in contact with the bottom of the slide plate (20). The roller extrusion frame (44) is located above the pusher plate (41).

7. The processing apparatus for a metal bracket for an aircraft seat according to claim 6, characterized in that: The storage component (9) includes a linkage rod (50), the upper surface of which is hinged to the center of the tripod (42). An elastic frame (51) is fixedly connected to the bottom of the linkage rod (50), and a triangular plate (52) is fixedly connected to the bottom of the elastic frame (51). A sieve storage rack (53) is fixedly connected to the inner wall of the filter plate (5). An elastic telescopic rod (54) is fixedly connected to the inner wall of the sieve storage rack (53). A through-hole extrusion plate (56) is fixedly connected to the end of the elastic telescopic rod (54) away from the sieve storage rack (53). An opening and closing door (55) is hinged to the end of the sieve storage rack (53).

8. The processing apparatus for a metal bracket for an aircraft seat according to claim 7, characterized in that: The number of through-hole extrusion plates (56) is set to six, and the six through-hole extrusion plates (56) are set to three groups, with two in each group. The number of sieve storage racks (53) is set to three. The three groups of through-hole extrusion plates (56) are located inside the three sieve storage racks (53) respectively. The triangular plate (52) is located at the end of the two through-hole extrusion plates (56) that are close to each other. The bottom of the through-hole extrusion plate (56) is in contact with the bottom of the inner wall of the sieve storage rack (53).

9. The processing apparatus for a metal bracket for an aircraft seat according to claim 8, characterized in that: The cooling component (10) includes a water pump (60), the bottom of which is fixedly connected to the bottom of the inner wall of the machine tool (1). The output end of the water pump (60) is connected to a bend (61). The end of the bend (61) away from the water pump (60) is slidably connected to a moving pipe (62). The end of the moving pipe (62) away from the bend (61) is connected to a transfer pipe (63). The end of the transfer pipe (63) away from the moving pipe (62) is connected to a spray frame (64).

10. The processing apparatus for a metal bracket for an aircraft seat according to claim 9, characterized in that: The end of the bend (61) away from the water pump (60) extends above the slide plate (20), the bottom of the moving pipe (62) is fixedly connected to the top of the moving frame (22), and the spray frame (64) is tilted toward the direction of the aircraft seat metal bracket (6).

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