Automatic stamping equipment and method for shell of multimedia touch screen controller of aero seat

Abstract

The invention belongs to the technical field of aero seat accessories, and particularly relates to an automatic stamping device and method for an aero seat multimedia touch screen controller shell. The stamping device is reasonable in design, a conveying assembly is used for driving linear displacement in the length direction of a material sliding plate base, and a first stamping assembly is used for stamping and forming a touch screen groove; a heat dissipation groove and a U-shaped groove are formed through a second stamping assembly in a stamping mode, a lock groove and a switch groove are formed through a third stamping assembly in a stamping mode, a step fastening groove is formed through a drilling assembly in a stamping mode, a cup groove is formed through a fourth stamping assembly and a pressure bearing assembly in a stamping mode, a plate body in the U-shaped groove is bent through a bending assembly, and an opening hinge ring is formed through a rounding assembly. According to the punching device, automatic batch punching of shells of the aero seat multimedia touch screen controllers can be achieved, and the punching efficiency is high; the prepared shell can meet the shell protection requirement of a large-size multimedia touch screen controller, and can be used as a dining table plate of an aero seat.

Description

Technical Field

[0001] The present invention belongs to the technical field of aviation seat accessories, and in particular relates to an automated stamping device and method for an aviation seat multimedia touch screen controller housing. Background Art

[0002] Stamping is a process that uses metal sheets as raw materials and stamping dies for forming. It uses stamping machinery to apply pressure to the metal sheet, causing it to undergo plastic deformation under the action of the die, and finally obtains the finished product in the desired shape. In the aerospace field, stamping parts are widely used in the manufacture of aircraft structural parts, such as the housing of multimedia touch screen controllers for aircraft seats.

[0003] The role of the aviation seat multimedia touch screen controller shell is mainly reflected in the following aspects: 1) Protecting internal components: The primary role of the shell is to protect the internal multimedia touch screen controller components. These components are very delicate and are susceptible to physical damage or environmental impact. The shell can provide a solid layer of protection to prevent the touch screen controller from being damaged by external factors such as impact, vibration or liquid. 2) Providing an operating interface: The shell is usually designed with a touch screen to allow passengers to interact with the multimedia system of the airline seat. Passengers can browse various information, watch movies, listen to music or play games through the touch screen, which greatly enriches their travel life. 3) Enhancing user experience: The design of the shell also takes into account ergonomics and aesthetics to ensure that passengers can operate comfortably when using it, while providing an aesthetically pleasing appearance. This helps to enhance the overall flight experience of passengers. 4) Adapting to different environments: The material and design of the shell are usually able to adapt to various conditions in the aviation environment, such as changes in air pressure and temperature. This ensures that the multimedia touch screen controller can work properly under various flight conditions. 5) Integrating other functions: In some advanced designs, the shell may also integrate other functions, such as information display in emergency situations, passenger status monitoring, etc. These functions are implemented through screens or other indicators on the casing, providing important information and guidance to passengers and crew.

[0004] The traditional automated stamping equipment for the shell of the multimedia touch screen controller for airline seats was found to have some shortcomings during use. First, it cannot realize the batch automatic stamping of the shell of the multimedia touch screen controller for airline seats, with low automation and low efficiency. Second, the shell of the multimedia touch screen controller for airline seats prepared by it has a single function and cannot meet the shell protection requirements of large-size multimedia touch screen controllers, nor can it be used as a dining table for airline seats. Therefore, it is necessary to optimize and improve the automated stamping equipment for the shell of the multimedia touch screen controller for airline seats. Summary of the invention

[0005] The object of the present invention is to overcome at least one of the above-mentioned problems existing in the prior art and to provide an automated stamping device and method for the housing of an aviation seat multimedia touch screen controller.

[0006] In order to achieve the above technical objectives and the above technical effects, the present invention is implemented through the following technical solutions: The present invention provides an automated stamping device for an aviation seat multimedia touch screen controller housing, the automated stamping device comprising a base, a sliding plate seat, a transmission component, a first stamping component, a second stamping component, a third stamping component, a drilling component, a fourth stamping component, a pressure bearing component, a bending component and a rounding component; A sliding plate seat is fixed on the base, and the sliding plate seat is provided with a first stamping station and a second stamping station; The conveying assembly is arranged below the slide plate seat and is used to drive the material to move linearly along the length direction of the slide plate seat; The first stamping assembly and the second stamping assembly are respectively arranged on two sides of the first stamping station, the first stamping assembly is used to stamp a touch screen groove on the shell body, and the second stamping assembly is used to stamp a heat dissipation groove and a U-shaped groove on the shell body; The third punching assembly and the drilling assembly are arranged above the first punching station, the third punching assembly is used to punch and form a lock slot and a switch slot on the shell body, and the drilling assembly is used to punch and form a step fastening slot on the shell body; The fourth stamping assembly and the pressure-bearing assembly are arranged at both sides of the second stamping station and are used together to stamp and form a cup groove on the shell body; The bending assembly and the rounding assembly are arranged at both sides of the second punching station. The bending assembly is used to bend the plate body in the U-shaped groove, and the rounding assembly is used to round the bent plate body to obtain an open hinged ring.

[0007] Furthermore, in the above-mentioned automated stamping equipment for the aviation seat multimedia touch screen controller shell, the aviation seat multimedia touch screen controller shell includes a shell body in the shape of a rectangular tube, the front side panel of the shell body is provided with a touch screen groove for exposing the touch screen in the multimedia touch screen controller, the middle part of the rear side panel of the shell body is provided with a plurality of heat dissipation grooves and a plurality of cup grooves protruding outward, the rear side panel of the shell body is provided with a U-shaped groove near the left and right ends, the shell body is connected with an outward-turned open hinge ring at the bottom edge of the U-shaped groove, the center of the upper side panel of the shell body is provided with a locking groove for facilitating it to be locked by the rear side locking member of the aviation seat, the upper side panel of the shell body is provided with a switch groove for facilitating exposing the switch key in the multimedia touch screen controller, and the upper side panel of the shell body is provided with step fastening grooves near the left and right ends for facilitating the fasteners to be inserted into the decorative strips in the opening areas on both sides of the shell body to tighten them.

[0008] Furthermore, in the above-mentioned automated stamping equipment for the aviation seat multimedia touch screen controller shell, the slide plate seat includes a slide plate seat body, the slide plate seat body is located at the first stamping station and is provided with a first stamping avoidance groove cooperating with the touch screen groove, a second stamping avoidance groove cooperating with the heat dissipation groove, a third stamping avoidance groove cooperating with the U-shaped groove, a fourth stamping avoidance groove cooperating with the lock groove, a fifth stamping avoidance groove cooperating with the switch groove and a sixth stamping avoidance groove cooperating with the step fastening groove, the slide plate seat body is located at the second stamping station and is provided with a seventh stamping avoidance groove cooperating with the cup groove and a bending avoidance groove for facilitating the forming of an opening hinge ring.

[0009] Furthermore, in the above-mentioned automated stamping equipment for the aviation seat multimedia touch screen controller shell, the conveying assembly includes a conveying linear guide pair and a conveying suction cup installed on the upper side of its slider, and the shape of the conveying suction cup cooperates with the shape of the lower side plate of the shell body.

[0010] Furthermore, in the above-mentioned automated stamping equipment for the housing of the multimedia touch screen controller of the aircraft seat, the first stamping assembly includes a first substrate, a first push rod, a material transfer suction cup and a first punch, the first substrate is mounted with the first push rod, the movable end of the first push rod is mounted with the material transfer suction cup and the first punch, and the shape of the first punch matches the shape of the touch screen slot; The second punching assembly includes a second substrate, a second push rod, a first mounting plate, a second punch and a third punch, the second substrate is mounted with the second push rod, the movable end of the second push rod is mounted with the second punch and the third punch via the first mounting plate, the shape of the second punch matches the shape of the heat dissipation groove, and the shape of the third punch matches the shape of the U-shaped groove; The third stamping assembly includes a third base plate, a third push rod, a second mounting plate, a fourth punch and a fifth punch. The third base plate is mounted with a third push rod, and the movable end of the third push rod is mounted with a fourth punch and a fifth punch via the second mounting plate. The shape of the fourth punch matches the shape of the lock slot, and the shape of the fifth punch matches the shape of the switch slot.

[0011] Furthermore, in the above-mentioned automated stamping equipment for the aviation seat multimedia touch screen controller housing, the drilling assembly includes a fourth substrate, a fourth push rod, a third mounting plate, a drill and a step drill bit, the fourth substrate is mounted with a fourth push rod, the movable end of the fourth push rod is mounted with a drill via the third mounting plate, and the output end of the drill is mounted with a step drill bit for forming a step fastening groove.

[0012] Furthermore, in the above-mentioned automated stamping equipment for the housing of the multimedia touch screen controller of the aviation seat, the fourth stamping assembly includes a fifth substrate, a fifth push rod and a cup groove forming punch, the fifth substrate is mounted with a fifth push rod, and the movable end of the fifth push rod is mounted with a cup groove forming punch; The pressure-bearing assembly comprises a sixth base plate, a sixth push rod and a cup groove forming pressure-bearing head, the sixth base plate is mounted with a sixth push rod, and the movable end of the sixth push rod is mounted with a cup groove forming pressure-bearing head; The cup groove forming punch and the cup groove forming pressure bearing head are butted against each other to form a cup groove forming area.

[0013] Furthermore, in the above-mentioned automated stamping equipment for the aviation seat multimedia touch screen controller housing, the bending assembly includes a seventh substrate, a seventh push rod and a bending push head, the seventh substrate is equipped with a seventh push rod, the movable end of the seventh push rod is equipped with a bending push head, and the bending push head can pass through the bending avoidance groove and bend the plate body in the U-shaped groove during the outward movement.

[0014] Further, in the above-mentioned automated stamping equipment for the housing of the multimedia touch screen controller for the aviation seat, the folding assembly includes a folding linear guide pair, an eighth push rod, a mounting frame, a folding positioning column, a folding motor, a flap, a first folding pressure rod and a second folding pressure rod, an eighth push rod is installed on the outer side of the slider of the folding linear guide pair, a mounting frame is fixed to the movable end of the eighth push rod, a folding positioning column is fixed to the lower part of the mounting frame, a folding motor is fixed to the upper part of the mounting frame, and the output shaft of the folding motor is installed with the first folding pressure rod and the second folding pressure rod via the flap; The folding positioning column is located at the periphery of the rotation area where the first folding pressure rod is located, and the minimum gap value between the rotation area where the first folding pressure rod is located and the folding positioning column is greater than the thickness value of the ring body of the open hinge ring; The folding positioning column is located at the inner periphery of the rotation area where the second folding pressure rod is located, and the minimum gap value between the rotation area where the second folding pressure rod is located and the folding positioning column is equal to the thickness value of the ring body of the open hinged ring.

[0015] The present invention also provides an automated stamping method for an aviation seat multimedia touch screen controller housing, which is implemented based on the automated stamping equipment for the aviation seat multimedia touch screen controller housing, and comprises the following steps: S1. Use the conveying assembly to convey the housing body to the first stamping station of the slide plate seat, and the first stamping assembly, the second stamping assembly, the third stamping assembly and the drilling assembly are in motion. Use the first stamping assembly to stamp a touch screen groove on the housing body, use the second stamping assembly to stamp a heat dissipation groove and a U-shaped groove on the housing body, use the third stamping assembly to stamp a lock groove and a switch groove on the housing body, and use the drilling assembly to stamp a step fastening groove on the housing body; S2, using the conveying assembly to convey the shell body to the second stamping station of the sliding plate seat, the fourth stamping assembly and the pressure-bearing assembly are actuated, and the fourth stamping assembly and the pressure-bearing assembly are used to stamp the cup groove on the shell body; the bending assembly is actuated, and the plate body in the U-shaped groove is bent by the bending assembly; the rounding assembly is actuated, and the bent plate body is rounded by the rounding assembly to obtain an open hinge ring; S3, using the conveying assembly to convey the shell body in the reverse direction, so that the shell body is separated from the slide plate seat, using the manipulator to take away the shell body that has completed the stamping process, and realizing the loading operation of the shell body to be stamped.

[0016] The beneficial effects of the present invention are: 1. The present invention provides an automated stamping device for the shell of an aviation seat multimedia touch screen controller, which is mainly composed of a base, a sliding plate seat, a transmission component, a first stamping component, a second stamping component, a third stamping component, a drilling component, a fourth stamping component, a pressure-bearing component, a bending component and a rounding component. The transmission component is used to drive the sliding plate seat to perform linear displacement along the length direction, the first stamping component is used to stamp a touch screen groove on the shell body, the second stamping component is used to stamp a heat dissipation groove and a U-shaped groove on the shell body, the third stamping component is used to stamp a lock groove and a switch groove on the shell body, the drilling component is used to stamp a step fastening groove on the shell body, the fourth stamping component and the pressure-bearing component are used to stamp a cup groove on the shell body, the bending component is used to bend the plate body in the U-shaped groove, and the rounding component is used to round the bent plate body to obtain an open hinge ring that is convenient for the shell body to be flipped and lowered; in this way, the present invention can realize batch automatic stamping of the shell of an aviation seat multimedia touch screen controller with high stamping efficiency.

[0017] 2. The aviation seat multimedia touch screen controller shell prepared by the present invention has rich functions. On the one hand, it can meet the shell protection requirements of a large-size multimedia touch screen controller, and on the other hand, it can also be used as a dining table board for an aviation seat.

[0018] Of course, any product implementing the present invention does not necessarily need to achieve all of the above advantages at the same time. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the accompanying drawings required for describing the embodiments will be briefly introduced below. Obviously, the accompanying drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other accompanying drawings can be obtained based on these accompanying drawings without paying creative work.

[0020] Figure 1 It is a schematic diagram of the use state of the automated stamping equipment of the present invention at the first stamping station; Figure 2 It is a schematic diagram of the use state of the automated stamping equipment of the present invention at the second stamping station; Figure 3 The figure is a schematic diagram of the processing flow of the housing of the multimedia touch screen controller for an aviation seat in the present invention; Figure 4 A schematic diagram of the structure of the housing of the multimedia touch screen controller for an aviation seat according to the present invention at one angle; Figure 5 This is a schematic diagram of the structure of the housing of the multimedia touch screen controller for an aviation seat in the present invention from another angle; Figure 6 A schematic diagram of the structure of the sliding plate seat at one angle in the present invention; Figure 7 A schematic diagram of the structure of the sliding plate seat at another angle in the present invention; Figure 8 It is a structural schematic diagram of the transmission component in the present invention; Fig. 9 A schematic diagram of the structure of the first and second stamping components of the present invention at one angle; Fig.10 It is a structural schematic diagram of the first and second stamping components in the present invention from another angle; Fig.11 It is a structural schematic diagram of the third stamping assembly in the present invention; Fig.12 It is a structural schematic diagram of the drilling assembly in the present invention; Fig.13 A schematic structural diagram of a fourth stamping assembly and a pressure-bearing assembly in the present invention at one angle; Fig.14 It is a structural schematic diagram of the fourth stamping assembly and the pressure-bearing assembly in the present invention from another angle; Fig.15 It is a schematic diagram of the structure of the bending component and the rounding component in the present invention; Fig.16 It is a schematic diagram of the use state of the circle bending component in the present invention; In the accompanying drawings, the components represented by the reference numerals are as follows: 1- base; 2-sliding plate seat, 201-sliding plate seat body, 202-first punching avoidance groove, 203-second punching avoidance groove, 204-third punching avoidance groove, 205-fourth punching avoidance groove, 206-fifth punching avoidance groove, 207-sixth punching avoidance groove, 208-cup groove, 209-bending avoidance groove; 3-transmission assembly, 301-linear guide pair, 302-transmission suction cup; 4-first punching assembly, 401-first substrate, 402-first push rod, 403-material transfer suction cup, 404-first punch; 5-second punching assembly, 501-second base plate, 502-second push rod, 503-first mounting plate, 504-second punch, 505-third punch; 6-third punching assembly, 601-third substrate, 602-third push rod, 603-second mounting plate, 604-fourth punch, 605-fifth punch; 7-drilling assembly, 701-fourth base plate, 702-fourth push rod, 703-third mounting plate, 704-drilling machine, 705-step drill bit; 8-fourth punching assembly, 801-fifth base plate, 802-fifth push rod, 803-cup groove forming punch; 9-pressure bearing assembly, 901-sixth substrate, 902-sixth push rod, 903-cup groove forming pressure bearing head; 10-bending assembly, 101-seventh base plate, 102-seventh push rod, 103-bending push head; 11-folding assembly, 111-folding linear guide pair, 112-eighth push rod, 113-mounting frame, 114-folding positioning column, 115-folding motor, 116-flip plate, 117-first folding pressure rod, 118-second folding pressure rod; 12-airline seat multimedia touch screen controller housing, 121-housing body, 122-touch screen slot, 123-heat dissipation slot, 124-U-shaped slot, 125-lock slot, 126-switch slot, 127-step fastening slot, 128-cup slot, 129-open hinge ring. DETAILED DESCRIPTION

[0021] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0022] like Figure 1-Figure 3As shown, this embodiment provides an automated stamping equipment for the shell of an aviation seat multimedia touch screen controller, which includes a base 1, a slide plate seat 2, a transmission component 3, a first stamping component 4, a second stamping component 5, a third stamping component 6, a drilling component 7, a fourth stamping component 8, a pressure-bearing component 9, a bending component 10 and a rounding component 11. The slide plate seat 2 is fixed on the base 1, and the slide plate seat 2 is provided with a first stamping station and a second stamping station. The transmission component 3 is arranged below the slide plate seat 2, and is used to drive the material (referring to the shell 12 of the aviation seat multimedia touch screen controller) to perform linear displacement along the length direction of the slide plate seat 2. The first stamping component 4 and the second stamping component 5 are respectively arranged on both sides of the first stamping station, and the first stamping component 4 is used to stamp and form the touch screen groove 122 on the shell body 121, and the second stamping component 5 is used to stamp and form the heat dissipation groove 123 and the U-shaped groove 124 on the shell body 121. The third punching assembly 6 and the drilling assembly 7 are arranged above the first punching station. The third punching assembly 6 is used to punch the lock groove 125 and the switch groove 126 on the shell body 121, and the drilling assembly 7 is used to punch the step fastening groove 127 on the shell body 121. The fourth punching assembly 8 and the pressure bearing assembly 9 are arranged on both sides of the second punching station, and are used together to punch the cup groove 128 on the shell body 121. The bending assembly 10 and the rounding assembly 11 are arranged on both sides of the second punching station. The bending assembly 10 is used to bend the plate body in the U-shaped groove 124, and the rounding assembly 11 is used to round the bent plate body to obtain an open hinge ring 129.

[0023] like Figure 4-Figure 5As shown, the aviation seat multimedia touch screen controller housing 12 includes a housing body 121 in a rectangular tubular shape. The front side panel of the housing body 121 is provided with a touch screen slot 122 for exposing the touch screen in the multimedia touch screen controller. The middle part of the rear side panel of the housing body 121 is provided with a plurality of heat dissipation slots 123 and a plurality of cup slots 128 protruding outward (in consideration of actual needs, two cup slots 128 can be provided, symmetrically distributed on both sides). The rear side panel of the housing body 121 is provided with a U-shaped slot 124 near the left and right ends, and the bottom edge of the housing body 121 located at the U-shaped slot 124 is connected with an open hinge ring 129 turned outward. The center of the upper side panel of the housing body 121 is provided with a lock slot 125 for facilitating its locking by the rear lock of the aviation seat. The lock can be rotated to clamp the lock head into the lock slot 125, thereby locking the position of the aviation seat multimedia touch screen controller housing 12. The upper side panel of the shell body 121 is provided with a switch slot 126 for exposing the switch button in the multimedia touch screen controller. The upper side panel of the shell body 121 is provided with step fastening slots 127 for installing fasteners near the left and right ends. The fasteners can be used to tighten the decorative strips inserted into the opening areas on both sides of the shell body 121. The decorative strips on both sides can improve the overall decorative appearance. At the same time, the decorative strips on both sides can limit the multimedia touch screen controller inserted in the middle.

[0024] In this embodiment, the aviation seat multimedia touch screen controller housing 12 mainly has two functions. The first function is to provide housing protection for the multimedia touch screen controller, and the second function is to serve as an aviation seat dining table.

[0025] like Figure 6-Figure 7 As shown, the slide plate seat 2 includes a slide plate seat body 201, the slide plate seat body 201 is located at the first stamping station and is provided with a first stamping avoidance groove 202 cooperating with the touch screen groove 122, a second stamping avoidance groove 203 cooperating with the heat dissipation groove 123, a third stamping avoidance groove 204 cooperating with the U-shaped groove 124, a fourth stamping avoidance groove 205 cooperating with the lock groove 125, a fifth stamping avoidance groove 206 cooperating with the switch groove 126 and a sixth stamping avoidance groove 207 cooperating with the step fastening groove 127, and the slide plate seat body 201 is located at the second stamping station and is provided with a seventh stamping avoidance groove 208 cooperating with the cup groove 128 and a bending avoidance groove 209 for facilitating the forming of an opening hinge ring 129.

[0026] The working principle of the sliding plate seat 2 is: the main cross-section of the sliding plate seat 2 is matched with the inner cavity cross-section of the outer shell body 121, and the sliding plate seat 2 can provide a sliding guide for the outer shell body 121; at the same time, the sliding plate seat 2 can provide internal support for the outer shell body 121 during the stamping process, and the sliding plate seat 2 uses several stamping avoidance grooves opened by itself to achieve stamping avoidance.

[0027] like Figure 8As shown, the conveying assembly 3 includes a conveying linear guide pair 301 and a conveying suction cup 302 installed on the upper side of its slider, and the shape of the conveying suction cup 302 matches the shape of the lower side plate of the shell body 121.

[0028] The working principle of the conveying assembly 3 is: using the conveying suction cup 302 to absorb the material, and using the conveying linear guide pair 301 to drive the material to linearly move, so that the material reaches the first stamping station and the second stamping station in sequence.

[0029] like Figure 9-11 As shown, the first stamping assembly 4 includes a first substrate 401, a first push rod 402, a material transfer suction cup 403 and a first punch 404. The first push rod 402 is installed on the first substrate 401, and the movable end of the first push rod 402 is installed with the material transfer suction cup 403 and the first punch 404. The shape of the first punch 404 matches the shape of the touch screen groove 122.

[0030] The working principle of the first stamping assembly 4 is as follows: the first push rod 402 is used to drive the first punch 404 to move, and the first punch 404 punches the front side panel of the shell body 121 at the first stamping station to form a touch screen groove 122 that exposes the touch screen in the multimedia touch screen controller, and the material transfer suction cup 403 is used to adsorb the cut slices. When the material transfer suction cup 403 is reset, the adsorption of the slices is released, and the slices fall freely under the action of gravity.

[0031] The second punching assembly 5 includes a second substrate 501, a second push rod 502, a first mounting plate 503, a second punch 504 and a third punch 505. The second push rod 502 is mounted on the second substrate 501, and the second punch 504 and the third punch 505 are mounted on the movable end of the second push rod 502 via the first mounting plate 503. The shape of the second punch 504 matches the shape of the heat dissipation groove 123, and the shape of the third punch 505 matches the shape of the U-shaped groove 124.

[0032] The working principle of the second stamping assembly 5 is: the second push rod 502 is used to drive the second punch 504 and the third punch 505 to punch and cut the rear side plate of the shell body 121 at the first stamping station to form a heat dissipation groove 123 and a U-shaped groove 124.

[0033] The third punch assembly 6 includes a third base plate 601, a third push rod 602, a second mounting plate 603, a fourth punch 604 and a fifth punch 605. The third base plate 601 is mounted with the third push rod 602, and the movable end of the third push rod 602 is mounted with the fourth punch 604 and the fifth punch 605 via the second mounting plate 603. The shape of the fourth punch 604 matches the shape of the lock slot 125, and the shape of the fifth punch 605 matches the shape of the switch slot 126.

[0034] The working principle of the third stamping assembly 6 is: the third push rod 602 is used to drive the fourth punch 604 and the fifth punch 605 to move, and the fourth punch 604 and the fifth punch 605 punch and cut the upper side plate of the shell body 121 at the first stamping station to form a lock groove 125 and a switch groove 126.

[0035] like Fig.12 As shown, the drilling assembly 7 includes a fourth substrate 701, a fourth push rod 702, a third mounting plate 703, a drill rig 704 and a step drill bit 705. The fourth substrate 701 is mounted with the fourth push rod 702, the movable end of the fourth push rod 702 is mounted with the drill rig 704 via the third mounting plate 703, and the output end of the drill rig 704 is mounted with a step drill bit 705 for forming a step fastening groove 127.

[0036] The working principle of the drilling assembly 7 is: the fourth push rod 702 is used to drive the drill rig 704 and the step drill bit 705 to move downward, and the drill rig 704 drives the step drill bit 705 during the downward movement, and the step drill bit 705 is used to process the step fastening groove 127 on the upper side plate of the shell body 121 at the first stamping station.

[0037] like Figure 13-14 As shown, the fourth stamping assembly 8 includes a fifth substrate 801 , a fifth push rod 802 and a cup groove forming punch 803 . The fifth substrate 801 is mounted with the fifth push rod 802 , and the movable end of the fifth push rod 802 is mounted with the cup groove forming punch 803 .

[0038] The pressure-bearing assembly 9 includes a sixth base plate 901 , a sixth push rod 902 and a cup groove forming pressure-bearing head 903 . The sixth base plate 901 is provided with the sixth push rod 902 , and the movable end of the sixth push rod 902 is provided with the cup groove forming pressure-bearing head 903 .

[0039] The working principle of the fourth stamping component 8 and the pressure-bearing component 9 is: the fifth push rod 802 is used to drive the cup groove forming punch 803 to move, and the sixth push rod 902 is used to drive the cup groove forming pressure head 903 to move. The cup groove forming punch 803 and the cup groove forming pressure head 903 are connected to form a cup groove forming area. The cup groove forming punch 803 and the cup groove forming pressure head 903 are connected to each other to stamp out the outwardly protruding cup groove 128 on the rear side panel of the shell body 121.

[0040] like Figure 15-16 As shown, the bending assembly 10 includes a seventh substrate 101, a seventh push rod 102 and a bending push head 103. The seventh push rod 102 is installed on the seventh substrate 101, and the bending push head 103 is installed on the movable end of the seventh push rod 102. The bending push head 103 can pass through the bending avoidance groove 209 and bend the plate body in the U-shaped groove 124 during the outward movement.

[0041] The folding assembly 11 includes a folding linear guide pair 111, an eighth push rod 112, a mounting frame 113, a folding positioning column 114, a folding motor 115, a flap 116, a first folding pressure rod 117 and a second folding pressure rod 118. The eighth push rod 112 is mounted on the outer side of the slider of the folding linear guide pair 111, the movable end of the eighth push rod 112 is fixed with the mounting frame 113, the lower part of the mounting frame 113 is fixed with the folding positioning column 114, the upper part of the mounting frame 113 is fixed with the folding motor 115, and the output shaft of the folding motor 115 is movably mounted with the first folding pressure rod 117 and the second folding pressure rod 118 which can rotate around its own axis through the flap 116.

[0042] The folding positioning column 114 is located at the periphery of the rotating area where the first folding pressure rod 117 is located, and the minimum gap value between the rotating area where the first folding pressure rod 117 is located and the folding positioning column 114 is greater than the thickness value of the ring body of the open hinged ring 129; the folding positioning column 114 is located at the inner periphery of the rotating area where the second folding pressure rod 118 is located, and the minimum gap value between the rotating area where the second folding pressure rod 118 is located and the folding positioning column 114 is equal to the thickness value of the ring body of the open hinged ring 129.

[0043] The working principle of the folding component 11 is as follows: the folding linear guide pair 111 of the folding component 11 drives the folding positioning column 114 to move longitudinally, and the eighth push rod 112 drives the folding positioning column 114 to move laterally. When the folding positioning column 114 reaches the set position and the bending component 10 bends the plate in the U-shaped groove 124, the folding motor 115 of the folding component 11 is activated. The folding motor 115 drives the first folding pressure rod 117 and the second folding pressure rod 118 to rotate through the flap 116. The first folding pressure rod 117 first contacts the bent plate and pushes it to perform a preliminary fold around the folding positioning column 114. Then the second folding pressure rod 118 contacts the preliminarily folded plate and pushes it to perform a fold around the folding positioning column 114 to obtain an open hinge ring 129. The folding linear guide pair 111 and the eighth push rod 112 of the folding component 11 are in action, so that the folding positioning column 114 is disengaged from the open hinge ring 129 and then reset. At this time, the outer shell body 121 can slide smoothly outward along the sliding plate seat 2 under the drive of the conveying component 3 to perform the unloading operation.

[0044] This embodiment also provides an automated stamping method for an aviation seat multimedia touch screen controller housing, comprising the following steps: S1. Use the conveying assembly 3 to convey the shell body 121 to the first stamping station of the slide plate seat 2. The first stamping assembly 4, the second stamping assembly 5, the third stamping assembly 6 and the drilling assembly 7 are in action. Use the first stamping assembly 4 to stamp the touch screen groove 122 on the shell body 121. Use the second stamping assembly 5 to stamp the heat dissipation groove 123 and the U-shaped groove 124 on the shell body 121. Use the third stamping assembly 6 to stamp the lock groove 125 and the switch groove 126 on the shell body 121. Use the drilling assembly 7 to stamp the step fastening groove 127 on the shell body 121. S2, using the conveying assembly 3 to convey the shell body 121 to the second stamping station of the sliding plate seat 2, the fourth stamping assembly 8 and the pressure-bearing assembly 9 are actuated, and the fourth stamping assembly 8 and the pressure-bearing assembly 9 are used to stamp the cup groove on the shell body; the bending assembly 10 is actuated, and the plate body in the U-shaped groove 124 is bent by the bending assembly 10; the rounding assembly 11 is actuated, and the bent plate body is rounded by the rounding assembly 11 to obtain the open hinge ring 129; S3, using the conveying assembly 3 to convey the shell body 121 in the reverse direction, so that the shell body 121 is separated from the slide plate seat 2, and the shell body 121 that has completed the stamping process is taken away by a manipulator, and the loading operation of the shell body 121 to be stamped is realized.

[0045] The present embodiment provides an automated stamping equipment for the shell of a multimedia touch screen controller for an aviation seat, which is mainly composed of a base 1, a slide plate seat 2, a transmission component 3, a first stamping component 4, a second stamping component 5, a third stamping component 6, a drilling component 7, a fourth stamping component 8, a pressure-bearing component 9, a bending component 10 and a rounding component 11. The transmission component 3 is used to drive the slide plate seat 2 to perform linear displacement along the length direction, the first stamping component 4 is used to stamp a touch screen groove 122 on the shell body 121, the second stamping component 5 is used to stamp a heat dissipation groove 123 and a U-shaped groove 124 on the shell body 121, and the fourth stamping component 8 is used to drive the slide plate seat 2 to perform linear displacement along the length direction, and the first stamping component 4 is used to stamp a touch screen groove 122 on the shell body 121. The second stamping component 5 is used to stamp a heat dissipation groove 123 and a U-shaped groove 124 on the shell body 121. The third stamping component 6 stamps out a lock groove 125 and a switch groove 126 on the shell body 121, the drilling component 7 stamps out a step fastening groove 127 on the shell body 121, the fourth stamping component 8 and the pressure-bearing component 9 stamp out a cup groove 128 on the shell body 121, the bending component 10 bends the plate body in the U-shaped groove 124, and the rounding component 11 rounds the bent plate body to obtain an open hinge ring 129 that is convenient for the shell body 121 to be flipped over and lowered; in this way, the present embodiment can realize batch automatic stamping of the aviation seat multimedia touch screen controller shell with high stamping efficiency.

[0046] The aviation seat multimedia touch screen controller housing 12 prepared in this embodiment is rich in functions. On the one hand, it can meet the housing protection requirements of a large-size multimedia touch screen controller, and on the other hand, it can also be used as a dining table board for an aviation seat.

[0047] The preferred embodiments of the present invention disclosed above are only useful to help explain the present invention. The preferred embodiments do not describe all the details in detail, nor do they limit the invention to specific implementation methods. Obviously, many modifications and changes can be made according to the content of this specification. This specification selects and specifically describes these embodiments in order to better explain the principles and practical applications of the present invention, so that those skilled in the art can understand and use the present invention well. The present invention is limited only by the claims and their full scope and equivalents.

Claims

1. Automated stamping equipment for aviation seat multimedia touch screen controller housing, characterized in that: The automated stamping equipment comprises a base, a sliding plate base, a transmission component, a first stamping component, a second stamping component, a third stamping component, a drilling component, a fourth stamping component, a pressure-bearing component, a bending component and a rounding component; A sliding plate seat is fixed on the base, and the sliding plate seat is provided with a first stamping station and a second stamping station; The conveying assembly is arranged below the slide plate seat and is used to drive the material to move linearly along the length direction of the slide plate seat; The first stamping assembly and the second stamping assembly are respectively arranged on two sides of the first stamping station, the first stamping assembly is used to stamp a touch screen groove on the shell body, and the second stamping assembly is used to stamp a heat dissipation groove and a U-shaped groove on the shell body; The third punching assembly and the drilling assembly are arranged above the first punching station, the third punching assembly is used to punch and form a lock slot and a switch slot on the shell body, and the drilling assembly is used to punch and form a step fastening slot on the shell body; The fourth stamping assembly and the pressure-bearing assembly are arranged at both sides of the second stamping station and are used together to stamp and form a cup groove on the shell body; The bending assembly and the rounding assembly are arranged at both sides of the second punching station. The bending assembly is used to bend the plate body in the U-shaped groove, and the rounding assembly is used to round the bent plate body to obtain an open hinged ring.

2. The automated stamping equipment for the aviation seat multimedia touch screen controller housing according to claim 1 is characterized in that: The shell of the multimedia touch-screen controller for an aviation seat includes a shell body in the shape of a rectangular tube, a front side panel of the shell body is provided with a touch-screen groove for exposing the touch-screen in the multimedia touch-screen controller, a plurality of heat dissipation grooves and a plurality of cup grooves protruding outward are provided in the middle of the rear side panel of the shell body, a U-shaped groove is provided on the rear side panel of the shell body near the left and right ends, an open hinge ring turning outward is connected to the bottom edge of the U-shaped groove of the shell body, a locking groove is provided at the center of the upper side panel of the shell body for facilitating locking by the rear locking piece of the aviation seat, a switch groove is provided on the upper side panel of the shell body for exposing the switch key in the multimedia touch-screen controller, and step fastening grooves are provided on the upper side panel of the shell body near the left and right ends for facilitating fasteners to be inserted into the decorative strips in the opening areas on both sides of the shell body for tightening.

3. The automated stamping equipment for the aviation seat multimedia touch screen controller housing according to claim 2 is characterized in that: The sliding plate seat includes a sliding plate seat body, and the sliding plate seat body is located at the first stamping station and is provided with a first stamping avoidance groove cooperating with the touch screen groove, a second stamping avoidance groove cooperating with the heat dissipation groove, a third stamping avoidance groove cooperating with the U-shaped groove, a fourth stamping avoidance groove cooperating with the lock groove, a fifth stamping avoidance groove cooperating with the switch groove, and a sixth stamping avoidance groove cooperating with the step fastening groove. The sliding plate seat body is located at the second stamping station and is provided with a seventh stamping avoidance groove cooperating with the cup groove and a bending avoidance groove for facilitating the forming of an opening hinge ring.

4. The automated stamping equipment for the aviation seat multimedia touch screen controller housing according to claim 3 is characterized in that: The conveying assembly comprises a conveying linear guide pair and a conveying suction cup installed on the upper side of the slider thereof, and the shape of the conveying suction cup matches the shape of the lower side plate of the shell body.

5. The automated stamping equipment for the aviation seat multimedia touch screen controller housing according to claim 4 is characterized in that: The first punching assembly includes a first substrate, a first push rod, a material transfer suction cup and a first punch. The first substrate is equipped with the first push rod, and the movable end of the first push rod is equipped with the material transfer suction cup and the first punch. The shape of the first punch matches the shape of the touch screen slot. The second punching assembly includes a second substrate, a second push rod, a first mounting plate, a second punch and a third punch, the second substrate is mounted with the second push rod, the movable end of the second push rod is mounted with the second punch and the third punch via the first mounting plate, the shape of the second punch matches the shape of the heat dissipation groove, and the shape of the third punch matches the shape of the U-shaped groove; The third stamping assembly includes a third base plate, a third push rod, a second mounting plate, a fourth punch and a fifth punch. The third base plate is mounted with a third push rod, and the movable end of the third push rod is mounted with a fourth punch and a fifth punch via the second mounting plate. The shape of the fourth punch matches the shape of the lock slot, and the shape of the fifth punch matches the shape of the switch slot.

6. The automated stamping equipment for the aviation seat multimedia touch screen controller housing according to claim 5, characterized in that: The drilling assembly includes a fourth base plate, a fourth push rod, a third mounting plate, a drill and a step drill bit. The fourth base plate is mounted with a fourth push rod, the movable end of the fourth push rod is mounted with a drill via the third mounting plate, and the output end of the drill is mounted with a step drill bit for forming a step fastening groove.

7. The automated stamping equipment for the aviation seat multimedia touch screen controller housing according to claim 6, characterized in that: The fourth punching assembly comprises a fifth base plate, a fifth push rod and a cup groove forming punch, wherein the fifth base plate is provided with a fifth push rod, and the movable end of the fifth push rod is provided with a cup groove forming punch; The pressure-bearing assembly comprises a sixth base plate, a sixth push rod and a cup groove forming pressure-bearing head, the sixth base plate is mounted with a sixth push rod, and the movable end of the sixth push rod is mounted with a cup groove forming pressure-bearing head; The cup groove forming punch and the cup groove forming pressure bearing head are butted against each other to form a cup groove forming area.

8. The automated stamping equipment for the aviation seat multimedia touch screen controller housing according to claim 7, characterized in that: The bending assembly includes a seventh base plate, a seventh push rod and a bending push head. The seventh base plate is equipped with the seventh push rod, and the movable end of the seventh push rod is equipped with a bending push head. The bending push head can pass through the bending avoidance groove and bend the plate body in the U-shaped groove during the outward movement.

9. The automated stamping equipment for the aviation seat multimedia touch screen controller housing according to claim 8, characterized in that: The folding assembly includes a folding linear guide pair, an eighth push rod, a mounting frame, a folding positioning column, a folding motor, a flap, a first folding pressure rod and a second folding pressure rod, the eighth push rod is installed on the outer side of the slider of the folding linear guide pair, the movable end of the eighth push rod is fixed with a mounting frame, the lower part of the mounting frame is fixed with a folding positioning column, the upper part of the mounting frame is fixed with a folding motor, and the output shaft of the folding motor is installed with the first folding pressure rod and the second folding pressure rod via the flap; The folding positioning column is located at the periphery of the rotation area where the first folding pressure rod is located, and the minimum gap value between the rotation area where the first folding pressure rod is located and the folding positioning column is greater than the thickness value of the ring body of the open hinge ring; The folding positioning column is located at the inner periphery of the rotation area where the second folding pressure rod is located, and the minimum gap value between the rotation area where the second folding pressure rod is located and the folding positioning column is equal to the thickness value of the ring body of the open hinged ring.

10. An automated stamping method for an aircraft seat multimedia touch screen controller shell, implemented based on the automated stamping equipment for an aircraft seat multimedia touch screen controller shell according to claim 9, characterized in that: The steps include: S1. Use the conveying assembly to convey the housing body to the first stamping station of the slide plate seat, and the first stamping assembly, the second stamping assembly, the third stamping assembly and the drilling assembly are in motion. Use the first stamping assembly to stamp a touch screen groove on the housing body, use the second stamping assembly to stamp a heat dissipation groove and a U-shaped groove on the housing body, use the third stamping assembly to stamp a lock groove and a switch groove on the housing body, and use the drilling assembly to stamp a step fastening groove on the housing body; S2, using the conveying assembly to convey the shell body to the second stamping station of the sliding plate seat, the fourth stamping assembly and the pressure-bearing assembly are actuated, and the fourth stamping assembly and the pressure-bearing assembly are used to stamp the cup groove on the shell body; the bending assembly is actuated, and the plate body in the U-shaped groove is bent by the bending assembly; the rounding assembly is actuated, and the bent plate body is rounded by the rounding assembly to obtain an open hinge ring; S3, using the conveying assembly to convey the shell body in the reverse direction, so that the shell body is separated from the slide plate seat, using the manipulator to take away the shell body that has completed the stamping process, and realizing the loading operation of the shell body to be stamped.

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