CN115229232A - A fully automated manufacturing equipment for aviation parts - Google Patents

Abstract

The invention discloses full-automatic manufacturing equipment for aviation parts, which comprises a main body, wherein a cavity is arranged in the main body, an automatic feeding structure and an automatic ejection structure are arranged in the cavity, an opening is formed in the upper side of the cavity, an automatic scrap discharge structure and an aviation plate fixing structure are respectively arranged on the upper side of the opening, a punching structure is arranged on one side of the opening, and a scrap collecting structure is arranged on the other side of the opening; the automatic feeding structure comprises: the automatic feeding mechanism comprises a conveying channel, a material frame, 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.

Description

A fully automated manufacturing equipment for aviation parts

technical field

The invention relates to the technical field of aviation parts, in particular to a fully automatic manufacturing equipment for aviation parts.

Background technique

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 has provided people with a fast, convenient, economical, safe and comfortable means of transportation, and has become the most important way for people to travel between continents. The main tool has been closely connected with countries around the world; in aviation parts, most of the plate parts are processed, such as chassis panels, wing panels, etc., because the flight design requires that the shape of the chassis for aviation is basically streamlined, That is, the casing plate is composed of a plurality of special-shaped plates with curved surfaces. In the prior art, when preparing aviation parts, it is necessary to perform operations such as punching the aviation plate, etc., but most of the existing punching devices cooperate with the manipulator. However, when the manipulator is running, only a single plate can be transported back and forth. During the whole process, the manipulator has a large moving stroke. Due to the limited movement speed of the manipulator, the overall efficiency of the device will be low when the device is running as a whole. , When drilling, the waste chips generated will splash around, and cleaning is very inconvenient. In view of this, in-depth research on the above problems led to this case.

SUMMARY OF THE INVENTION

The purpose of the present invention is to solve the above problems, design a fully automatic manufacturing equipment for aviation parts, and solve the existing background technical problems.

The technical solution of the present invention to achieve the above objects is as follows: a fully automated manufacturing equipment for aviation parts, including a main body, a cavity is arranged inside the main body, and an automatic feeding structure and an automatic ejecting structure are installed inside the cavity, so the The upper side of the cavity is provided with an opening, the upper side of the opening is respectively provided with an automatic waste discharge structure and an aviation board fixing structure, one side of the opening is provided with a punching structure, and the other side of the opening is provided with a waste dust collection structure;

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 return springs and feeding board;

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 the connection between the material rack and the conveying channel is provided with a feeding port, and the movable plate is arranged at the bottom of the conveying channel. On the lower side of the material rack, the two first connecting plates are respectively installed on both sides of the movable plate, and the two second connecting plates are respectively installed on both sides of the material rack. The push rod driving end is fixedly installed on the bottom of the two second connecting plates, and the output ends of the two feeding electric push rods are fixedly connected with the tops of the two first connecting plates, and one end of the two transmission rods is connected to the top of the two first connecting plates. The top of the movable plate is connected on both sides, and the other ends of the two transmission rods penetrate through the bottom wall of the material rack and are fixedly connected to both sides of the bottom of the movable plate. The four return springs are distributed on both sides of the material rack. One end of the four return springs is connected with the two first connecting plates, the other end is fixedly connected with the outer walls of the material rack on both sides, and the two sides of the bottom of the feeding plate are respectively fixed with the tops of the two transmission rods. connect;

The automatic feeding structure includes: feeding motor, rotating disc, transmission block, telescopic frame, four ejector electric push rods, tray and first control button;

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

The automatic waste discharge structure includes: a temporary storage groove, a material guide groove, a plurality of conveying rollers, an electric opening and closing door and two first electric sliding rails;

The two first electric sliding rails are installed on the top of the main body, and the two first electric sliding rails are arranged on one side of the opening, and the bottom side of the temporary storage slot is connected to the two first electric sliding rails. connection, the material guide groove is arranged on one side of the inside of the temporary storage tank, a plurality of the conveying rollers are arranged on the top of the material guide tank, and the electric opening and closing door is arranged on the other side of the inside of the temporary storage tank;

The waste collection structure includes: a collection bin, a rotating door, a rotating motor, a driving gear and a driven half-tooth;

The collection bin is arranged inside the main body, and the top of the collection bin is provided with a feeding port, the rotating door is set inside the collection bin, and the rotating door is set on the lower side of the feeding port, and the rotating The door is hinged with the lower side of the feeding port, the rotating motor is installed inside the collecting bin, the driving gear is connected with the driving end of the rotating motor, and the driven half-tooth is arranged on the lower side of the rotating door.

The punching structure includes: a lifting electric push rod, a horizontal plate, a second electric sliding rail, a third electric sliding rail, a fixed seat, a driving motor and a drill bit;

The driving end of the lift electric push rod is installed on the top of the main body, the bottom side of the horizontal plate is fixedly connected to the top of the output end of the lift electric push rod, and the top of the second electric slide rail is fixedly connected to the bottom of the horizontal 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 drive motor is connected to the fixed seat, and the drill bit The top is connected with the drive end of the drive motor.

The first control button is electrically connected with the four ejector electric push rods and the two first electric slide rails.

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, and the two fixed electric push rod driving ends 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, and the rear ends of the two clamping blocks are respectively fixedly connected with the output ends of the two fixed electric push rods.

The driving gear and the driven half-tooth are in mesh with each other.

The front end of the main body is provided with a feeding port, and the position of the feeding port corresponds to the position of the material rack. At the same time, the front end of the main body is provided with a waste removal door, and the position of the waste removal door corresponds to the position of the collection bin.

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 with the rotating motor and the electric opening and closing door.

The telescopic frame as a whole is in a "T" shape, and the upper side of the telescopic frame is provided with a through hole, and the transmission block is slidably connected to the through hole on the upper side of the telescopic frame.

Both the middle parts of the two clamping blocks are provided with rectangular grooves, and the rectangular grooves are matched with the thickness of the aviation board to be processed.

A fully automatic manufacturing equipment for aviation parts is produced by using the technical solution of the present invention. Compared with the prior art, the structure has the following beneficial effects: through the automatic feeding structure and the automatic ejection structure, the uninterrupted automatic feeding operation of the aviation special plate can be carried out. With the cooperation of the punching structure, the aviation board can be fixed and punched, and the waste generated by the punching can be automatically collected through the cooperation of the automatic waste discharge structure and the waste collection structure while the punching operation is in progress. The structure cooperates with each other to realize the automatic processing and manufacturing of aviation parts from feeding to waste collection, and has the characteristics of high degree of automation.

Description of drawings

FIG. 1 is a schematic cross-sectional structural schematic diagram of a front view of a fully automated manufacturing equipment for aviation parts according to the present invention.

FIG. 2 is a schematic front view of the structure of a fully automated manufacturing equipment for aviation parts according to the present invention.

FIG. 3 is a schematic top-view structural diagram of a fully automated manufacturing equipment for aviation parts according to the present invention.

FIG. 4 is a schematic top-view cross-sectional structural diagram of a fully automated manufacturing equipment for aviation parts according to the present invention.

FIG. 5 is a schematic front view of the automatic feeding structure of the fully automatic manufacturing equipment for aviation parts according to the present invention.

FIG. 6 is a partial top-view structural schematic diagram of a fully automated manufacturing equipment for aviation parts according to the present invention.

FIG. 7 is an enlarged schematic view of the structure of part A of a fully automated manufacturing equipment for aviation parts according to the present invention.

FIG. 8 is an enlarged schematic view of the structure at B of a fully automated manufacturing equipment for aviation parts according to the present invention.

In the figure: 1. Main body, 2. Cavity, 3. Conveying channel, 4. Material rack, 5. Active 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 disc, 14, transmission block, 15, telescopic frame, 16, ejector electric push rod, 17, tray, 18, The first control button, 19, the temporary storage slot, 20, the material guide slot, 21, the conveying roller, 22, the electric opening and closing door, 23, the first electric sliding rail, 24, the collection bin, 25, the rotating door, 26, Rotating motor, 27, driving gear, 28, driven half tooth, 29, lift electric push rod, 30, horizontal plate, 31, second electric slide rail, 32, third electric slide rail, 33, fixed seat, 34, Drive motor, 35, drill bit, 36, vertical plate, 37, clamping block, 38, fixed electric push rod, 39, feeding port, 40, waste removal door, 41, second control button.

Detailed ways

The present invention will be described in detail below with reference to the accompanying drawings, as shown in FIGS. 1-8 .

All the electrical components in this case are connected with the power supply to which they are adapted through wires by those skilled in the art, and an appropriate controller should be selected according to the actual situation to meet the control requirements. The specific connection and control sequence should refer to the following working principles Among them, the electrical connection between the electrical components is completed in sequence, and the detailed connection means are known in the art. The following mainly introduces the working principle and process, and does not describe the electrical control.

Embodiment: According to the accompanying drawings 1-8 of the description, a fully automated manufacturing equipment for aviation parts includes a main body 1, a cavity 2 is arranged inside the main body 1, and an automatic feeding structure and an automatic ejection structure are installed inside the cavity 2 The upper side of the cavity 2 is provided with an opening, and the upper side of the opening is respectively provided with an automatic waste discharge structure and an aviation plate fixing structure, one side of the opening is provided with a punching structure, and the other side of the opening is provided with a waste collection structure;

The automatic feeding structure consists of conveying channel 3, material rack 4, movable plate 5, two first connecting plates 6, two second connecting plates 7, two feeding electric push rods 8, two transmission rods 9, four The return spring 10 and the feeding plate 11 are composed, and their connection relationship and positional relationship are as follows;

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 the connection between the material rack 4 and the conveying channel 3 is provided with a feeding port, and the movable plate 5 is arranged on the lower side of the material rack 4, and the two The first connecting plates 6 are respectively installed on both sides of the movable plate 5, the two second connecting plates 7 are respectively installed on both sides of the material rack 4, and the driving ends of the two feeding electric push rods 8 are fixedly installed on the two second connecting plates 7 bottom, and the output ends of the two feeding electric push rods 8 are fixedly connected to the top of the two first connecting plates 6, one end of the two transmission rods 9 is connected to both sides of the top of the movable plate 5, and the other end of the two transmission rods 9 penetrates the material The bottom wall of the rack 4 is fixedly connected with the bottom two sides of the movable plate 5, four return springs 10 are distributed on both sides of the material rack 4, and one end of the four return springs 10 is connected with the two first connecting plates 6, and the other end is connected with the material The outer walls on both sides of the frame 4 are fixedly connected, and the two sides of the bottom of the feeding plate 11 are fixedly connected with the tops of the two transmission rods 9 respectively;

In the specific implementation process, the operation of the two feeding electric push rods 8 is first controlled, and the two feeding electric push rods 8 can drive the feeding plate 11 through the two first connecting plates 6 , the movable plate 5 and the two transmission rods 9 . Move downward, and during this process, the four return springs 10 will also be stretched. At this time, a number of aerospace plates and the like are fed into the middle part of the material rack 4 through the feeding port 39 at the front end of the main body 1, and some The plate, etc. are placed on the top of the feeding plate 11, and then the two feeding electric push rods 8 are controlled to stop running. At this time, the four return springs 10 are not stretched by the two feeding electric push rods 8, and the four return springs 10 The two first connecting plates 6 will drive the movable plate 5, the two transmission rods 9, the feeding plate 11 and several aviation boards on the top of the feeding board 11 to move upward, and the topmost board among the several boards can be passed through the feeding port. 39 is sent into the conveying channel 3. At this time, with the automatic ejection structure, the automatic feeding operation can be realized, and the two second connecting plates 7 are used to support the two feeding electric push rods 8;

According to the accompanying drawings 1-8 of the description, the automatic feeding structure is composed of a feeding motor 12, a rotating disc 13, a transmission block 14, a telescopic frame 15, four electric push rods 16 for ejecting, a tray 17 and a first control button 18. Its connection relationship and location relationship are as follows;

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

In the specific implementation process, after the top plate among several plates is fed into the conveying channel 3 through the feeding port 39 , the feeding motor 12 is controlled to run intermittently, and the feeding motor 12 drives the rotating disc 13 to rotate, and when the rotating disc 13 At the same time of rotation, the transmission block 14 can be driven to slide inside the through hole on the side of the telescopic frame 15, and as the transmission block 14 continuously slides inside the through hole of the telescopic frame 15, the telescopic frame 15 can be driven to reciprocate, so that the telescopic frame 15 The topmost board among several boards can be pushed to the top of the tray 17. The top of the tray 17 is provided with several guide pulleys, which can increase the smoothness of the movement of the board. After the board moves on the top of the tray 17, the side of the board will hit the first control button. 18, at this time, the four ejecting electric push rods 16 operate, which can drive the tray 17 and the plate on the top of the tray 17 to rise from the opening. At this time, the two first electric sliding rails 23 operate, which can temporarily store The slot 19 is moved away, so as not to block the tray 17 when the four push-out electric push rods 16 drive the tray 17 to rise;

According to Figures 1-8 in the description, the automatic waste discharge structure is composed of a temporary storage slot 19, a material guide slot 20, a number of conveying rollers 21, an electric opening and closing door 22 and two first electric sliding rails 23. The connection relationship is And the location relationship is as follows;

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. The bottom side of the temporary storage slot 19 is connected with the two first electric slide rails 23 , and the material guide slot is connected to the two first electric slide rails 23 . 20 is arranged on one side of the inside of the temporary storage tank 19, a plurality of conveying rollers 21 are arranged on the top of the guide tank 20, and the electric opening and closing door 22 is arranged on the other side of the inside of the temporary storage tank 19;

In the specific implementation process, after the four ejector electric push rods 16 are operated to drive the tray 17 and the plate on the top of the tray 17 to rise from the opening, the aviation plate fixing structure and the punching structure operate, and the ejected plate can be Clamping and fixing, and during this process, the two first electric slide rails 23 will run again, driving the temporary storage slot 19 to reset, and then in the aviation plate fixing structure and the punching structure operation, when the plate is punched, the waste is The chips will fall to the top of the guide chute 20, and at the same time, a number of conveying rollers 21 rotate, which can increase the movement of the waste chips on the guide chute 20, and then, the waste chips will accumulate on the top of the electric opening and closing door 22, and the next plate When being ejected from the inside of the main body 1, another plate will squeeze the first control button 18 again. At this time, the two first electric slide rails 23 run, which can drive the temporary storage slot 19 to move again, and then the temporary storage slot 19 One end 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 is opened, and the waste chips accumulated on the top of the electric opening and closing door 22 can be put into the waste chips. Collect the inside of the structure to collect;

According to Figures 1-8 of the description, the waste collection structure consists of a collection bin 24, a rotating door 25, a rotating motor 26, a driving gear 27 and a driven half tooth 28, and the connection relationship and positional relationship are as follows;

The collection bin 24 is arranged inside the main body 1, and the top of the collection bin 24 is provided with a feeding port. The rotating door 25 is set inside the collecting bin 24. The motor 26 is installed inside the collection bin 24, the driving gear 27 is connected with the driving end of the rotating motor 26, and the driven half-tooth 28 is arranged on the lower side of the rotating door 25;

In the specific implementation process, the two first electric sliding rails 23 will drive the electric opening and closing door 22 on the temporary storage slot 19 to move to the top of the collection bin 24, and trigger the two second control buttons 41. After the second control button 41 is triggered, the rotating motor 26 and the electric opening and closing door 22 run synchronously, and the rotating electric drive can drive the driving gear 27 to rotate, and then drive the rotating door 25 to rotate through the driven half-tooth 28, so that the top of the collection bin 24 can be driven to rotate. The feeding port leaks out, and the electric opening and closing door 22 runs synchronously, and the wastes accumulated on the top of the electric opening and closing door 22 can be put into the collection bin 24 through the feeding port;

According to the accompanying drawings 1-8 of the description, the punching structure is composed of a lifting electric push rod 29, a horizontal plate 30, a second electric sliding rail 31, a third electric sliding rail 32, a fixed seat 33, a driving motor 34 and a drill bit 35. The connection relationship and location relationship are as follows;

The driving end of the lifting electric push rod 29 is installed on the top of the main body 1, the bottom side of the horizontal plate 30 is fixedly connected to the top of the output end of the lifting electric push rod 29, the second electric sliding rail 31 is fixedly connected to the bottom of the top horizontal plate 30, and the third electric sliding rail The top of 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 drive motor 34 is connected to the fixed seat 33, and the top of the drill bit 35 is connected to the drive end of the drive motor 34;

In the specific implementation process, after the aviation plate fixing structure has finished clamping and fixing the plate, the lifting and lowering electric push rod 29 operates to drive the horizontal plate 30 and several parts at the bottom thereof to move downward. At the same time, the second electric sliding rail 31 and the first The operation of the three electric slide rails 32 can drive the drive motor 34 and the drill bit 35 to move in multiple directions in the horizontal direction. At the same time, the drive motor 34 can drive the drill bit 35 to rotate, and then the plate can be punched, and the electric push rod 29 can be lifted and lowered. , the second electric sliding rail 31 and the third electric sliding rail 32 cooperate to facilitate the drilling operation of multiple plates;

According to the accompanying drawings 1-8 of the description, the aviation plate fixing structure is composed of two vertical plates 36, two clamping blocks 37 and two fixed electric push rods 38, and the connection relationship and positional relationship are as follows;

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 outside of the two vertical plates 36, and the two fixed electric push rods 38 The driving end runs through the two vertical plates 36, and the rear ends of the two clamping blocks 37 are respectively fixedly connected with the output ends of the two fixed electric push rods 38;

In the specific implementation process, after the four ejecting electric push rods 16 drive the aviation board to rise through the tray 17, the two fixed electric push rods 38 run, which can drive the two clamping blocks 37 to move, and then can adjust the movement of the board. Both the front and rear ends are clamped and fixed, which is convenient for the next operation such as punching the plate;

To sum up, when the technical solution is running, the two feeding electric push rods 8 are first controlled to run, and then a number of aerospace plates and the like are fed into the middle part of the material rack 4 through the feeding port 39 at the front end of the main body 1, and the two upper The feeding electric push rod 8 stops running, and the four return springs 10 can drive several sheets to rise, and the top one of the several sheets will enter the interior of the conveying channel 3. At this time, the feeding motor 12 runs intermittently, driving the telescopic frame 15. The reciprocating motion is performed to push the plate inside the conveying channel 3 to the top of the tray 17, and due to the elastic force of the four return springs 10, after the top one of several plates moves to the top of the tray 17, it will be driven down again. A plate enters the conveying channel 3 for replenishment, and after the plate moves to the top of the tray 17, the first control button 18 will be triggered. At this time, the two first electric slide rails 23 will operate to drive the temporary storage slot 19 to move. The top opening of the cavity 2 is exposed, and at the same time, the four ejecting electric push rods 16 can push the top of the tray 17 with the plates out to a certain height, and the two fixed electric push rods 38 run together with the two clamp The clamping block 37 can clamp the plate. At the same time, the four ejector electric push rods 16 are retracted into the cavity 2, and the two first electric slide rails 23 run in the opposite direction, which can drive the temporary storage slot 19 to reset. At the same time, the lifting and lowering electric push rod 29, the second electric sliding rail 31 and the third electric sliding rail 32 run to drive the driving motor 34 to move, so that the plate can be punched. And the waste generated during the punching process will fall into the temporary storage tank 19, and cooperate with the guide groove 20 and a number of conveying rollers 21, the waste will accumulate on the top of the electric opening and closing door 22, and will be deposited on the next plate. After the first control button 18 is activated, the two first electric slide rails 23 will drive the temporary storage slot 19 to move again, and then, one end of the temporary storage slot 19 will trigger the two second control buttons 41, and the door 22 will be electrically opened and closed at this time. Open, the rotary motor 26 runs, which can drive the rotary door 25 to rotate, leak the feeding port, and put the wastes accumulated on the top of the electric opening and closing door 22 into the collection bin 24 through the feeding port for collection. , the collected waste can be taken out through the waste removal door 40, and the temporary storage tank 19 can be reset. When the plate is punched, the above-mentioned operation process can be repeated, and the plate can be automatically fed and punched without interruption. Hole operation, and can automatically collect the waste generated by punching.

The above technical solutions only represent the preferred technical solutions of the technical solutions of the present invention, and some changes that those skilled in the art may make to some parts of them all reflect the principles of the present invention and fall within the protection scope of the present invention.

Claims (10)

1. The full-automatic manufacturing equipment for the aviation parts comprises a main body and is characterized in that a cavity is arranged in the main body, an automatic feeding structure and an automatic ejection structure are mounted in the cavity, an opening is formed in the upper side of the cavity, an automatic scrap discharging structure and an aviation plate fixing structure are respectively arranged on the upper side of the opening, a punching structure is arranged on one side of the opening, and a scrap collecting structure is arranged on the other side of the opening;

the automatic feeding structure comprises: the feeding device 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 reset springs and a feeding plate;

the conveying channel is arranged in the cavity, the top of the material frame is fixedly arranged at the bottom of the conveying channel, a feeding hole is formed in the joint of the material frame and the conveying channel, the movable plate is arranged on the lower side of the material frame, the two first connecting plates are respectively arranged on two sides of the movable plate, the two second connecting plates are respectively arranged on two sides of the material frame, the driving ends of the two feeding electric push rods are fixedly arranged at the bottoms of the two second connecting plates, the output ends of the two feeding electric push rods are fixedly connected with the tops of the two first connecting plates, one ends of the two transmission rods are connected with two sides of the top of the movable plate, the other ends of the two transmission rods penetrate through the wall surface of the bottom of the material frame and are fixedly connected with two sides of the bottom of the movable plate, the four reset springs are distributed on two sides of the material frame in pairs, one ends of the four reset springs are connected with the two first connecting plates, the other ends of the four reset springs are fixedly connected with the outer walls of two sides of the material frame, and two sides of the bottom of the upper material plate are respectively and fixedly connected with two tops of the two transmission rods;

the automatic feeding structure comprises: the feeding device comprises a feeding motor, a rotating disc, a transmission block, a telescopic frame, four ejection electric push rods, a tray and a first control button;

the feeding motor is installed inside the cavity, the bottom of the rotating disc is connected with the driving end of the feeding motor, the conveying block is installed at the top of the rotating disc, one side of the expansion bracket is inserted into the conveying channel, the other side of the expansion bracket is connected with the driving block in a sliding mode, the driving ends of the four ejection electric push rods are fixedly installed on the wall surface of the bottom of the cavity, the bottom of the tray is fixedly connected with the tops of the output ends of the four ejection electric push rods, and the first control button is installed on one side of the top of the tray.

2. The automatic aviation component manufacturing equipment according to claim 1, wherein the automatic scrap discharge structure comprises: the device comprises a temporary storage tank, a guide chute, a plurality of conveying rollers, an electric opening and closing door and two first electric slide rails;

the two first electric slide rails are arranged at the top of the main body, 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 with the two first electric slide rails, the material guide groove is arranged on one side of the interior of the temporary storage tank, the plurality of conveying rollers are arranged on the top of the material guide groove, and the electric opening and closing door is arranged on the other side of the interior of the temporary storage tank;

the scrap collecting structure comprises: the collecting bin, the rotating door, the rotating motor, the driving gear and the driven half gear;

collect the storehouse set up in inside the main part, just it is provided with the dog-house to collect the storehouse top, the revolving door set up in it is inside to collect the storehouse, the revolving door set up in the dog-house downside, the revolving door is articulated with the dog-house downside, the rotation motor install in it is inside to collect the storehouse, the driving gear with rotate the motor drive end and connect, driven half tooth set up in the side joint under the revolving door.

3. The apparatus according to claim 1, wherein the perforation structure comprises: the device comprises a lifting electric push rod, a transverse plate, a second electric slide rail, a third electric slide rail, a fixed seat, a driving motor and a drill bit;

the electric drill comprises a main body, a lifting electric push rod, a transverse plate, a second electric slide rail, a third electric slide rail, a fixed seat, a driving motor, a driving end of the lifting electric push rod, a transverse plate bottom, one side of the transverse plate bottom, an output end top of the lifting electric push rod, a transverse plate bottom, the second electric slide rail top, the third electric slide rail top, the second electric slide rail bottom, the fixed seat bottom, the third electric slide rail bottom, the driving motor, the fixed seat and the drill bit top, wherein the driving end of the driving motor is connected with the transverse plate.

4. The automatic aviation component manufacturing equipment according to claim 2, wherein the first control button is electrically connected to four of the ejecting electric push rods and two of the first electric slide rails.

5. The automatic aviation component manufacturing equipment according to claim 1, wherein the aviation plate fixing structure comprises: the clamping device comprises two vertical plates, two clamping blocks and two fixed electric push rods;

two the riser install in the main part top, and two the riser is located both sides around the opening respectively, two fixed electric putter drive end is installed respectively in two the riser outside, and two fixed electric putter drive end runs through two the riser, two press from both sides tight piece rear end respectively with two fixed electric putter output fixed connection.

6. The automatic aviation component manufacturing equipment according to claim 2, wherein the driving gear and the driven half-gear are meshed with each other.

7. The automatic aviation part manufacturing equipment according to claim 2, wherein a feed port is formed in the front end of the main body, the feed port corresponds to the position of the material rack, and a scrap discharge door is formed in the front end of the main body, and the scrap discharge door corresponds to the position of the collection bin.

8. The automatic aviation component manufacturing equipment according to claim 2, wherein two second control buttons are disposed on one side of the top of the main body, and are electrically connected to the rotating motor and the electric opening and closing door respectively.

9. The automatic aviation component manufacturing equipment according to claim 1, wherein the telescopic frame is integrally formed into a "T" shape, a through hole is formed in the upper side of the telescopic frame, and the transmission block is slidably connected with the through hole in the upper side of the telescopic frame.

10. The full-automatic aviation part manufacturing device according to claim 5, characterized in that rectangular grooves matched with the thickness of an aviation plate to be processed are formed in the middle of each of the two clamping blocks.

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