A fully automated manufacturing device for aviation parts

Abstract

The present invention discloses a fully automated manufacturing device for aviation components, including a main body. There is a cavity inside the main body, and an automatic feeding structure and an automatic ejecting structure are installed inside the cavity. An opening is provided on the upper side of the cavity. An automatic waste discharging structure and an aviation plate fixing structure are respectively provided on the upper side of the opening. A punching structure is provided on one side of the opening, and a waste collecting structure is provided on the other side of the opening. The automatic feeding structure includes: a conveying channel, a material rack, a movable plate, two first connecting plates, two second connecting plates, two feeding electric push rods, two transmission rods, four reset springs and a feeding plate. The beneficial effect of the present invention is that by adopting the automatic feeding structure, the automatic ejecting structure, the automatic waste discharging structure, the aviation plate fixing structure, the punching structure and the waste collecting structure, the above-mentioned several structures cooperate with each other to realize the automated processing and manufacturing of aviation components from feeding to waste collection, and has characteristics such as high automation degree.

Description

Technical Field

[0001] The invention relates to the technical field of aviation parts, in particular to fully automated manufacturing equipment for aviation parts. Background Art

[0002] With the development of society, the aviation industry is also making great progress. The development of aviation has greatly changed the structure of transportation. Aircraft provides people with a fast, convenient, economical, safe and comfortable means of transportation. It has become the main tool for people to travel between continents and has strengthened the exchanges between countries around the world. Most of the processing of aviation parts is on panels, such as casing panels, wing panels, etc. Since the flight design requires that the shape of the aviation casing is basically streamlined, that is, the casing panel is composed of a plurality of special-shaped panels with curved surfaces. In the prior art, when preparing aviation parts, it is necessary to perform operations such as punching on aviation panels, etc. However, most of the existing punching devices are equipped with robots to achieve automated preparation. However, when the robot is in operation, it can only carry out back and forth transportation operations on a single plate. During the whole process, the robot has a large moving stroke. Due to the limited moving speed of the robot, the overall efficiency of the device will be low when it is running. At the same time, when drilling, the waste chips generated will splash everywhere, which is very inconvenient to clean. In view of this, in-depth research was conducted on the above-mentioned problems, and thus this case was created. Summary of the invention

[0003] The purpose of the present invention is to solve the above problems and to design a fully automated manufacturing equipment for aviation parts to solve the existing background technology problems.

[0004] The technical solution of the present invention to achieve the above-mentioned purpose is: a fully automated manufacturing equipment for aviation parts, comprising a main body, a cavity is provided inside the main body, an automatic feeding structure and an automatic ejection structure are installed inside the cavity, an opening is provided on the upper side of the cavity, a waste automatic discharge structure and an aviation plate fixing structure are respectively provided on the upper side of the opening, a punching structure is provided on one side of the opening, and a waste collection structure is provided on the other side of the opening;

[0005] The automatic feeding structure comprises: a conveying channel, a material rack, a movable plate, two first connecting plates, two second connecting plates, two feeding electric push rods, two transmission rods, four return springs and a feeding plate;

[0006] The conveying channel is arranged inside the cavity. The top of the material rack is fixedly installed at the bottom of the conveying channel, and a feeding port is arranged at the connection between the material rack and the conveying channel. The movable plate is arranged on the lower side of the material rack. Two first connecting plates are respectively installed on both sides of the movable plate. Two second connecting plates are respectively installed on both sides of the material rack. The driving ends of two feeding electric push rods are fixedly installed at the bottoms of two second connecting plates, and the output ends of two feeding electric push rods are fixedly connected to the tops of two first connecting plates. One ends of two transmission rods are connected to both sides of the top of the movable plate, and the other ends of two transmission rods penetrate through the bottom wall surface of the material rack and are fixedly connected to both sides of the bottom of the movable plate. Four reset springs are distributed in pairs on both sides of the material rack, and one ends of four reset springs are connected to two first connecting plates, and the other ends are fixedly connected to the outer walls on both sides of the material rack. Both sides of the bottom of the feeding plate are respectively fixedly connected to the tops of two transmission rods;

[0007] The automatic feeding structure includes: a feeding motor, a rotating disk, a transmission block, a telescopic frame, four ejecting electric push rods, a tray and a first control button;

[0008] The feeding motor is installed inside the cavity. The bottom of the rotating disk is connected to the driving end of the feeding motor. The transmission block is installed on the top of the rotating disk. One side of the telescopic frame is inserted into the conveying channel, and the other side of the telescopic frame is slidably connected to the transmission block. The driving ends of four ejecting electric push rods are fixedly installed on the bottom wall surface of the cavity. The bottom of the tray is fixedly connected to the tops of the output ends of four ejecting electric push rods. The first control button is installed on one side of the top of the tray.

[0009] The waste chip automatic discharging structure includes: a temporary storage tank, a guiding chute, a plurality of conveying roller wheels, an electric opening and closing door and two first electric slide rails;

[0010] Two first electric slide rails are installed on the top of the main body, and two first electric slide rails are arranged on one side of the opening. One side of the bottom of the temporary storage tank is connected to two first electric slide rails. The guiding chute is arranged on one side inside the temporary storage tank. A plurality of conveying roller wheels are arranged on the top of the guiding chute. The electric opening and closing door is arranged on the other side inside the temporary storage tank;

[0011] The waste chip collection structure includes: a collection bin, a rotating door, a rotating motor, a driving gear and a driven half gear;

[0012] The collection bin is arranged inside the main body, and a feeding port is arranged at the top of the collection bin. The rotating door is arranged inside the collection bin, below the feeding port. The rotating door is hinged to the lower side of the feeding port. The rotating motor is installed inside the collection bin, and the driving gear is connected to the driving end of the rotating motor. The driven half-tooth is arranged at the lower side of the rotating door.

[0013] The punching structure includes: a lifting electric push rod, a cross plate, a second electric slide rail, a third electric slide rail, a fixed seat, a driving motor, and a drill bit.

[0014] The driving end of the lifting electric push rod is installed at the top of the main body. One side of the bottom of the cross plate is fixedly connected to the top of the output end of the lifting electric push rod. The top of the second electric slide rail is fixedly connected to the bottom of the cross plate. The top of the third electric slide rail is slidably connected to the bottom of the second electric slide rail. The bottom of the fixed seat is slidably connected to the bottom of the third electric slide rail. The driving motor is connected to the fixed seat, and the top of the drill bit is connected to the driving end of the driving motor.

[0015] The first control button is electrically connected to the four ejecting electric push rods and the two first electric slide rails.

[0016] The aviation plate fixing structure includes: two vertical plates, two clamping blocks, and two fixed electric push rods.

[0017] The two vertical plates are installed at the top of the main body, and the two vertical plates are respectively located on the front and back sides of the opening. The driving ends of the two fixed electric push rods are respectively installed on the outer sides of the two vertical plates, and the driving ends of the two fixed electric push rods penetrate through the two vertical plates. The rear ends of the two clamping blocks are respectively fixedly connected to the output ends of the two fixed electric push rods.

[0018] The driving gear meshes with the driven half-tooth.

[0019] A feeding port is arranged at the front end of the main body, and the position of the feeding port corresponds to the position of the material rack. At the same time, a waste chip removal door is arranged at the front end of the main body, and the position of the waste chip removal door corresponds to the position of the collection bin.

[0020] Two second control buttons are arranged on one side of the top of the main body, and the two second control buttons are respectively electrically connected to the rotating motor and the electric opening and closing door.

[0021] The telescopic frame is integrally in a "T" shape, and a through hole is arranged on the upper side of the telescopic frame. The transmission block is slidably connected to the through hole on the upper side of the telescopic frame.

[0022] A rectangular groove is provided in the middle part of each of the two clamping blocks, and the rectangular groove matches the thickness of the aviation plate to be processed.

[0023] An all - automatic manufacturing equipment for aviation parts made by using the technical solution of the present invention. This technical solution adopts an automatic feeding structure, an automatic ejecting structure, an automatic waste discharging structure, an aviation plate fixing structure, a drilling structure, and a waste collection structure. Compared with the prior art, the following beneficial effects exist: Through the automatic feeding structure and the automatic ejecting structure, continuous automatic feeding operation of special aviation plates can be carried out. At the same time, after the feeding is completed, with the cooperation of the aviation plate fixing structure and the drilling structure, the aviation plate can be fixed and drilled. And while the drilling operation is in progress, through the cooperation of the automatic waste discharging structure and the waste collection structure, the waste generated by drilling is automatically collected. The above - mentioned several structures cooperate with each other to realize the automatic processing and manufacturing of aviation parts from feeding to waste collection, and has the characteristics of high automation. Brief Description of the Drawings

[0024] Figure 1 It is a schematic main - sectional view structure diagram of an all - automatic manufacturing equipment for aviation parts described in the present invention.

[0025] Figure 2 It is a schematic main - view structure diagram of an all - automatic manufacturing equipment for aviation parts described in the present invention.

[0026] Figure 3 It is a schematic top - view structure diagram of an all - automatic manufacturing equipment for aviation parts described in the present invention.

[0027] Figure 4 It is a schematic top - sectional view structure diagram of an all - automatic manufacturing equipment for aviation parts described in the present invention.

[0028] Figure 5 It is a schematic main - view structure diagram of the automatic feeding structure of an all - automatic manufacturing equipment for aviation parts described in the present invention.

[0029] Figure 6 It is a schematic partial top - view structure diagram of an all - automatic manufacturing equipment for aviation parts described in the present invention.

[0030] Figure 7 It is a schematic enlarged - view structure diagram at position A of an all - automatic manufacturing equipment for aviation parts described in the present invention.

[0031] Figure 8 It is a schematic enlarged - view structure diagram at position B of an all - automatic manufacturing equipment for aviation parts described in the present invention.

[0032] In the figure: 1. Main body, 2. Cavity, 3. Conveyor channel, 4. Material rack, 5. Movable plate, 6. First connecting plate, 7. Second connecting plate, 8. Feeding electric push rod, 9. Transmission rod, 10. Return spring, 11. Feeding plate, 12. Feeding motor, 13. Rotating disk, 14. Transmission block, 15. Telescopic frame, 16. Ejecting electric push rod, 17. Tray, 18. First control button, 19. Temporary storage tank, 20. Guide chute, 21. Conveyor roller, 22. Electrically operated opening and closing door, 23. First electric slide rail, 24. Collection bin, 25. Rotating door, 26. Rotating motor, 27. Driving gear, 28. Driven half gear, 29. Lifting electric push rod, 30. Horizontal plate, 31. Second electric slide rail, 32. Third electric slide rail, 33. Fixed seat, 34. Driving motor, 35. Drill bit, 36. Vertical plate, 37. Clamping block, 38. Fixed electric push rod, 39. Feeding port, 40. Chip removal door, 41. Second control button. Detailed implementation mode

[0033] The present invention will be specifically described below with reference to the accompanying drawings, as Figure 1 shown in Figures -8.

[0034] Those skilled in the art connect all the electrical components in this case to their adapted power supplies through wires, and should select a suitable controller according to the actual situation to meet the control requirements. For the specific connection and control sequence, reference should be made to the sequence of operation of each electrical component in the following working principle to complete the electrical connection. The detailed connection means are well-known techniques in the art. The following mainly introduces the working principle and process, and no description of electrical control will be given.

[0035] Embodiment: As can be seen from the attached drawings of the specification Figure 1 -8, an all-automatic manufacturing equipment for aviation parts includes a main body 1. A cavity 2 is provided inside the main body 1. An automatic feeding structure and an automatic ejecting structure are installed inside the cavity 2. An opening is provided on the upper side of the cavity 2. An automatic chip discharging structure and an aviation plate fixing structure are respectively provided on the upper side of the opening. A drilling structure is provided on one side of the opening, and a chip collection structure is provided on the other side of the opening;

[0036] The automatic feeding structure is composed of a conveyor channel 3, a material rack 4, a movable plate 5, two first connecting plates 6, two second connecting plates 7, two feeding electric push rods 8, two transmission rods 9, four return springs 10 and a feeding plate 11. The connection relationship and positional relationship are as follows;

[0037] The conveying channel 3 is arranged inside the cavity 2. The top of the material rack 4 is fixedly installed at the bottom of the conveying channel 3, and a feeding port is arranged at the connection between the material rack 4 and the conveying channel 3. The movable plate 5 is arranged on the lower side of the material rack 4. Two first connecting plates 6 are respectively installed on both sides of the movable plate 5. Two second connecting plates 7 are respectively installed on both sides of the material rack 4. The driving ends of two feeding electric push rods 8 are fixedly installed at the bottom of the two second connecting plates 7, and the output ends of the two feeding electric push rods 8 are fixedly connected to the tops of the two first connecting plates 6. One ends of two transmission rods 9 are connected to both sides of the top of the movable plate 5, and the other ends of the two transmission rods 9 penetrate through the bottom wall surface of the material rack 4 and are fixedly connected to both sides of the bottom of the movable plate 5. Four reset springs 10 are distributed in pairs on both sides of the material rack 4, and one ends of the four reset springs 10 are connected to the two first connecting plates 6, and the other ends are fixedly connected to the outer walls on both sides of the material rack 4. Both sides of the bottom of the feeding plate 11 are fixedly connected to the tops of the two transmission rods 9;

[0038] In the specific implementation process, first, control the operation of the two feeding electric push rods 8. The two feeding electric push rods 8 can drive the feeding plate 11 to move downward through the two first connecting plates 6, the movable plate 5 and the two transmission rods 9. And in this process, the four reset springs 10 will also be stretched. At this time, several aerospace plates, etc. are sent into the middle part of the material rack 4 through the feeding port 39 at the front end of the main body 1, and several plates, etc. are placed on the top of the feeding plate 11. Subsequently, control the two feeding electric push rods 8 to stop operating. At this time, the four reset springs 10 are no longer stretched by the two feeding electric push rods 8, and the four reset springs 10 will drive the movable plate 5, the two transmission rods 9, the feeding plate 11 and several aerospace plates on the top of the feeding plate 11 to move upward through the two first connecting plates 6, and the topmost plate among several plates can be sent into the conveying channel 3 through the feeding port 39. At this time, with the cooperation of the automatic ejection structure, the automatic feeding operation can be realized. The two second connecting plates 7 are used to support the two feeding electric push rods 8;

[0039] According to the specification appendix Figure 1 -8, it can be seen that the automatic feeding structure is composed of a feeding motor 12, a rotating disk 13, a transmission block 14, a telescopic frame 15, four ejection electric push rods 16, a tray 17 and a first control button 18. The connection relationship and the positional relationship are as follows;

[0040] The feeding motor 12 is installed inside the cavity 2. The bottom of the rotating disk 13 is connected to the driving end of the feeding motor 12. The transmission block is installed on the top of the rotating disk 13. One side of the telescopic frame 15 is inserted into the conveying channel 3, and the other side of the telescopic frame 15 is slidably connected to the transmission block 14. The driving ends of the four ejection electric push rods 16 are fixedly installed on the bottom wall surface of the cavity 2. The bottom of the tray 17 is fixedly connected to the tops of the output ends of the four ejection electric push rods 16. The first control button 18 is installed on one side of the top of the tray 17;

[0041] In the specific implementation process, after the topmost sheet among several sheets is fed into the conveying channel 3 through the feeding port 39, the feeding motor 12 is controlled to run intermittently. The feeding motor 12 drives the rotating disk 13 to rotate, and while the rotating disk 13 is rotating, it can drive the transmission block 14 to slide inside the through hole on one side of the telescopic frame 15. Furthermore, as the transmission block 14 continuously slides inside the through hole of the telescopic frame 15, it can drive the telescopic frame 15 to perform reciprocating motion, so that the telescopic frame 15 can push the topmost sheet among several sheets to the top of the tray 17. A number of guiding pulleys are arranged on the top of the tray 17, which can increase the smoothness of the movement of the sheet. After the sheet moves on the top of the tray 17, one side of the sheet will hit the first control button 18. At this time, the four ejecting electric push rods 16 operate, and can drive the tray 17 and the sheet on the top of the tray 17 to rise from the opening. At the same time, the two first electric slide rails 23 operate, and can move the temporary storage tank 19 away, so that when the four ejecting electric push rods 16 drive the tray 17 to rise, it will not block the tray 17;

[0042] According to the attached drawings Figure 1 -8, the waste chip automatic discharge structure is composed of a temporary storage tank 19, a material guiding groove 20, a number of conveying rollers 21, an electric opening and closing door 22, and two first electric slide rails 23. The connection relationship and the position relationship are as follows;

[0043] The two first electric slide rails 23 are installed on the top of the main body 1, and the two first electric slide rails 23 are arranged on one side of the opening. One side of the bottom of the temporary storage tank 19 is connected to the two first electric slide rails 23. The material guiding groove 20 is arranged on one side inside the temporary storage tank 19. A number of conveying rollers 21 are arranged on the top of the material guiding groove 20. The electric opening and closing door 22 is arranged on the other side inside the temporary storage tank 19;

[0044] In the specific implementation process, after the four ejecting electric push rods 16 operate to drive the tray 17 and the sheet on the top of the tray 17 to rise from the opening, the aviation sheet fixing structure and the punching structure operate, and can clamp and fix the ejected sheet. During this process, the two first electric slide rails 23 will operate again to drive the temporary storage tank 19 to reset. Therefore, when the aviation sheet fixing structure and the punching structure operate to punch the sheet, the waste chips will fall onto the top of the material guiding groove 20. At the same time, a number of conveying rollers 21 rotate, which can increase the movement of the waste chips on the material guiding groove 20. Subsequently, the waste chips will accumulate on the top of the electric opening and closing door 22. When the next sheet is ejected from the inside of the main body 1, another sheet will squeeze the first control button 18 again. At this time, the two first electric slide rails 23 operate, and can drive the temporary storage tank 19 to move again. Subsequently, one end of the temporary storage tank 19 will squeeze the two second control buttons 41 and trigger the two second control buttons 41. At this time, the electric opening and closing door 22 opens, and can put the waste chips accumulated on the top of the electric opening and closing door 22 into the waste chip collection structure for collection;

[0045] According to FIGS. Figure 1 -8, the waste chip collection structure is composed of a collection bin 24, a rotating door 25, a rotating motor 26, a driving gear 27, and a driven half gear 28. Their connection relationship and positional relationship are as follows;

[0046] The collection bin 24 is arranged inside the main body 1, and a feeding port is arranged at the top of the collection bin 24. The rotating door 25 is arranged inside the collection bin 24, below the feeding port. The rotating door 25 is hinged to the lower side of the feeding port. The rotating motor 26 is installed inside the collection bin 24, the driving gear 27 is connected to the driving end of the rotating motor 26, and the driven half gear 28 is arranged at the lower side of the rotating door 25;

[0047] In the specific implementation process, the two first electric slide rails 23 will drive the electric opening and closing door 22 on the temporary storage tank 19 to move to the top of the collection bin 24 and trigger two second control buttons 41. After the two second control buttons 41 are triggered, the rotating motor 26 and the electric opening and closing door 22 run synchronously. The rotation of the rotating motor can drive the driving gear 27 to rotate, and then drive the rotating door 25 to rotate through the driven half gear 28, so that the feeding port at the top of the collection bin 24 can be exposed. The electric opening and closing door 22 runs synchronously, and the waste chips accumulated on the top of the electric opening and closing door 22 can be put into the collection bin 24 through the feeding port;

[0048] According to FIGS. Figure 1 -8, the drilling structure is composed of a lifting electric push rod 29, a cross plate 30, a second electric slide rail 31, a third electric slide rail 32, a fixed seat 33, a driving motor 34, and a drill bit 35. Their connection relationship and positional relationship are as follows;

[0049] The driving end of the lifting electric push rod 29 is installed at the top of the main body 1. One side of the bottom of the cross plate 30 is fixedly connected to the top of the output end of the lifting electric push rod 29. The top of the second electric slide rail 31 is fixedly connected to the bottom of the cross plate 30. The top of the third electric slide rail 32 is slidably connected to the bottom of the second electric slide rail 31. The bottom of the fixed seat 33 is slidably connected to the bottom of the third electric slide rail 32. The driving motor 34 is connected to the fixed seat 33, and the top of the drill bit 35 is connected to the driving end of the driving motor 34;

[0050] In the specific implementation process, after the aviation plate fixing structure clamps and fixes the plate, the lifting electric push rod 29 operates to drive the cross plate 30 and several parts at its bottom to move downward. At the same time, the second electric slide rail 31 and the third electric slide rail 32 operate, which can drive the driving motor 34 and the drill bit 35 to move in multiple directions horizontally. At the same time, the driving motor 34 operates to drive the drill bit 35 to rotate, so as to perform drilling operations on the plate. The cooperation of the lifting electric push rod 29, the second electric slide rail 31 and the third electric slide rail 32 facilitates the drilling operation on multiple plates;

[0051] According to the attached drawings in the specification Figure 1 -8, it can be seen that the aviation plate fixing structure is composed of two vertical plates 36, two clamping blocks 37 and two fixed electric push rods 38. Their connection relationship and positional relationship are as follows;

[0052] The two vertical plates 36 are installed on the top of the main body 1, and the two vertical plates 36 are respectively located on the front and rear sides of the opening. The driving ends of the two fixed electric push rods 38 are respectively installed on the outer sides of the two vertical plates 36, and the driving ends of the two fixed electric push rods 38 penetrate the two vertical plates 36. The rear ends of the two clamping blocks 37 are respectively fixedly connected to the output ends of the two fixed electric push rods 38;

[0053] In the specific implementation process, after the four ejecting electric push rods 16 drive the aviation plate to rise through the tray 17, the two fixed electric push rods 38 operate to drive the two clamping blocks 37 to move, so as to clamp and fix both the front and rear ends of the plate, which is convenient for the next operations such as drilling the plate;

[0054] In summary, when this technical solution is in operation, first, control the two feeding electric push rods 8 to operate. Subsequently, through the feeding port 39 at the front end of the main body 1, several aerospace plates and the like are sent into the middle part of the material rack 4. When the two feeding electric push rods 8 stop operating, the four reset springs 10 can drive several plates to rise, and the topmost one of the several plates will enter the conveying channel 3. At this time, the feeding motor 12 operates intermittently, driving the telescopic frame 15 to move reciprocally, and then the plate located inside the conveying channel 3 can be pushed onto the top of the tray 17. Due to the elastic force of the four reset springs 10, after the topmost one of the several plates moves to the top of the tray 17, it will drive the next plate to enter the conveying channel 3 again for replenishment. After the plate moves to the top of the tray 17, it will trigger the first control button 18. At this time, the two first electric slide rails 23 will operate, driving the temporary storage slot 19 to move and exposing the opening at the top of the cavity 2. At the same time, the four ejecting electric push rods 16 can push the top of the tray 17 with the plate. After ejecting to a certain height, the two fixed electric push rods 38 operate, and cooperate with the two clamping blocks 37 to clamp the plate. At the same time, the four ejecting electric push rods 16 retract into the cavity 2, and the two first electric slide rails 23 run in the reverse direction, driving the temporary storage slot 19 to reset. At the same time, the lifting electric push rod 29, the second electric slide rail 31, and the third electric slide rail 32 operate, driving the driving motor 34 to move, and then the plate can be punched. After the punching is completed, the plate will be taken away by a manipulator or the like, and the waste chips generated during the punching process will fall into the temporary storage slot 19. Through the cooperation of the material guiding groove 20 and several conveying rollers 21, the waste chips will accumulate on the top of the electric opening and closing door 22. After the next plate triggers the first control button 18, the two first electric slide rails 23 will drive the temporary storage slot 19 to move again. Subsequently, one end of the temporary storage slot 19 will trigger the two second control buttons 41. At this time, the electric opening and closing door 22 will open, and the rotating motor 26 will operate, driving the rotating door 25 to rotate, exposing the feeding port, and the waste chips accumulated on the top of the electric opening and closing door 22 can be put into the collection bin 24 through the feeding port for collection. After the collection is completed, the collected waste chips can be taken out through the waste chip access door 40, and the temporary storage slot 19 is reset. When punching the plate, repeat the above operation process, and the plate can be automatically fed and automatically punched continuously, and the waste chips generated by punching can be automatically collected.

[0055] The above technical solution only reflects the preferred technical solution of the technical solution of the present invention. Some changes that those skilled in the art of this technology may make to some parts thereof all reflect the principle of the present invention and fall within the protection scope of the present invention.

Claims

1. An all-automatic manufacturing device for aviation parts, including a main body, characterized in that, The interior of the main body is provided with a cavity. An automatic feeding structure and an automatic ejecting structure are installed inside the cavity. An opening is provided on the upper side of the cavity. An automatic waste discharging structure and an aviation plate fixing structure are respectively provided on the upper side of the opening. A punching structure is provided on one side of the opening, and a waste collecting structure is provided on the other side of the opening; The automatic feeding structure includes: a conveying channel, a material rack, a movable plate, two first connecting plates, two second connecting plates, two feeding electric push rods, two transmission rods, four reset springs, and a feeding plate; The conveying channel is arranged inside the cavity. The top of the material rack is fixedly installed at the bottom of the conveying channel, and a feeding port is arranged at the connection between the material rack and the conveying channel. The movable plate is arranged below the material rack. The two first connecting plates are respectively installed on both sides of the movable plate. The two second connecting plates are respectively installed on both sides of the material rack. The driving ends of the two feeding electric push rods are fixedly installed at the bottoms of the two second connecting plates, and the output ends of the two feeding electric push rods are fixedly connected to the tops of the two first connecting plates. One ends of the two transmission rods are connected to both sides of the top of the movable plate, and the other ends of the two transmission rods penetrate through the bottom wall surface of the material rack and are fixedly connected to both sides of the bottom of the movable plate. The four reset springs are distributed in pairs on both sides of the material rack, and one ends of the four reset springs are connected to the two first connecting plates, and the other ends are fixedly connected to the outer walls on both sides of the material rack. Both sides of the bottom of the feeding plate are respectively fixedly connected to the tops of the two transmission rods; The automatic ejecting structure includes: a feeding motor, a rotating disk, a transmission block, a telescopic frame, four ejecting electric push rods, a tray, and a first control button; The feeding motor is installed inside the cavity. The bottom of the rotating disk is connected to the driving end of the feeding motor. The transmission block is installed on the top of the rotating disk. One side of the telescopic frame is inserted into the conveying channel, and the other side of the telescopic frame is slidably connected to the transmission block. The driving ends of the four ejecting electric push rods are fixedly installed on the bottom wall surface of the cavity. The bottom of the tray is fixedly connected to the tops of the output ends of the four ejecting electric push rods. The first control button is installed on one side of the top of the tray; The automatic waste discharging structure includes: a temporary storage tank, a guiding groove, a number of conveying roller wheels, an electric opening and closing door, and two first electric slide rails; The two first electric slide rails are installed on the top of the main body, and the two first electric slide rails are arranged on one side of the opening. One side of the bottom of the temporary storage tank is connected to the two first electric slide rails. The guiding groove is arranged on one side inside the temporary storage tank. A number of the conveying roller wheels are arranged on the top of the guiding groove. The electric opening and closing door is arranged on the other side inside the temporary storage tank; The waste collecting structure includes: a collecting bin, a rotating door, a rotating motor, a driving gear, and a driven half gear; The collection bin is arranged inside the main body, and a feeding port is arranged at the top of the collection bin. The rotating door is arranged inside the collection bin, below the feeding port. The rotating door is hinged to the lower side of the feeding port. The rotating motor is installed inside the collection bin, the driving gear is connected to the driving end of the rotating motor, and the driven half gear is arranged below the rotating door; The aviation board fixing structure includes: two vertical plates, two clamping blocks and two fixed electric push rods; The two vertical plates are installed on the top of the main body, and the two vertical plates are respectively located on the front and rear sides of the opening. The driving ends of the two fixed electric push rods are respectively installed on the outer sides of the two vertical plates, and the driving ends of the two fixed electric push rods penetrate through the two vertical plates. The rear ends of the two clamping blocks are respectively fixedly connected to the output ends of the two fixed electric push rods; During operation, when the board moves to the top of the tray, the first control button will be triggered. At this time, the two first electric slide rails will operate, driving the temporary storage tank to move and exposing the opening at the top of the cavity. At the same time, the four ejecting electric push rods will eject the tray with the board. After ejecting to a certain height, the two fixed electric push rods will operate, cooperating with the two clamping blocks to clamp the board. At the same time, the four ejecting electric push rods will retract into the cavity, and the two first electric slide rails will run in the reverse direction, driving the temporary storage tank to reset.

2. An all-automatic manufacturing device for aviation parts according to claim 1, characterized in that, The drilling structure includes: a lifting electric push rod, a cross plate, a second electric slide rail, a third electric slide rail, a fixed seat, a driving motor and a drill bit; The driving end of the lifting electric push rod is installed on the top of the main body. One side of the bottom of the cross plate is fixedly connected to the top of the output end of the lifting electric push rod. The top of the second electric slide rail is fixedly connected to the bottom of the cross plate. The top of the third electric slide rail is slidably connected to the bottom of the second electric slide rail. The bottom of the fixed seat is slidably connected to the bottom of the third electric slide rail. The driving motor is connected to the fixed seat, and the top of the drill bit is connected to the driving end of the driving motor.

3. An all-automatic manufacturing device for aviation parts according to claim 1, characterized in that, The first control button is electrically connected to the four ejecting electric push rods and the two first electric slide rails.

4. An all-automatic manufacturing device for aviation parts according to claim 1, characterized in that, The driving gear meshes with the driven half gear.

5. An all - automated manufacturing device for aviation parts according to claim 1, characterized in that, A feeding port is arranged at the front end of the main body, and the position of the feeding port corresponds to the position of the material rack. At the same time, a waste chip removal door is arranged at the front end of the main body, and the position of the waste chip removal door corresponds to the position of the collection bin.

6. The fully automated manufacturing equipment for an aviation component according to claim 1, characterized in that, Two second control buttons are arranged on one side of the top of the main body, and the two second control buttons are respectively electrically connected to the rotating motor and the electric opening and closing door.

7. An all - automated manufacturing device for aviation parts according to claim 1, characterized in that, The telescopic frame is integrally in a "T" shape, and a through hole is arranged on the upper side of the telescopic frame. The transmission block is slidably connected to the through hole on the upper side of the telescopic frame.

8. An all-automatic manufacturing device for aviation parts according to claim 1, characterized in that Rectangular grooves are arranged in the middle parts of the two clamping blocks, and the rectangular grooves match the thickness of the aviation board to be processed.

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