A double-end synchronous welding device for processing the load-bearing rod of an aircraft

By designing a dual-end synchronous welding device for aircraft load bearing rod processing, automatic clamping and synchronous welding of the rod body and joints is achieved using clamping components and motor drive systems, the problem of inefficient production efficiency in the prior art is solved and the welding efficiency is improved.

CN119820206BActive Publication Date: 2025-06-27上海多弗众云航空科技有限公司
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Patent Information

Application Number
CN202510316176.6
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2025-03-18
Publication Date
2025-06-27
Estimated Expiration
2045-03-18

AI Technical Summary

Technical Problem

The existing aircraft load-bearing rod processing technology has low degree of automation, resulting in low production efficiency, and it requires manual positioning and welding of the rod body and joints, which is time-consuming and labor-intensive.

Method used

A double-end synchronous welding device for aircraft load bearing rod processing is designed, and the rod body and joint are clamped and fixed by clamping assembly, and the rotor and drum are driven synchronously, so that the rod body and joint are rotated and welded at the welding station.

Benefits of technology

Automatic centering clamping and synchronous rotation welding of the double-end joint of the aircraft load-bearing rod is realized, which significantly improves work efficiency and reduces the time and energy of manual operation.

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Abstract

The present invention relates to the field of aircraft accessory processing, and specifically to a double-end synchronous welding device for processing aircraft load-bearing rods. The device includes a base, and further includes: a conveying mechanism fixed to the base through a first bracket. Multiple first clamping assemblies and second clamping assemblies for clamping the rod body and the connecting joint are arranged on the conveying mechanism. The first clamping assembly includes a claw for clamping the rod body, and the second clamping assembly includes two rotating cylinders for clamping the connecting joint; a motor and a welding machine fixed to a second bracket, the second bracket is fixed to the base. The output shaft end of the motor is coaxially fixedly connected with a first turntable and a second turntable. An arc-shaped rack one is fixed on the circumferential wall of the first turntable, and the rotating cylinder is intermittently driven to rotate through the arc-shaped rack one. An arc-shaped rack two is fixed on the circumferential wall of the second turntable, and the conveying mechanism is driven to operate through the arc-shaped rack two. This double-end synchronous welding device for processing aircraft load-bearing rods realizes automatic centering clamping and rotary welding, thereby greatly improving the working efficiency.
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Description

Technical Field

[0001] The invention relates to the field of aircraft accessory processing, in particular to a double-end synchronous welding device for processing aircraft load-bearing rods. Background Art

[0002] The load-bearing rods designed in aircraft are usually composed of a rod body and two connecting joints welded together, and the welding part is a circular weld. The current welding equipment has a low degree of automation, and the ends of the rod body and the two connecting joints need to be welded separately, so the production efficiency is low. Since the rod body and the joints at both ends need to be manually positioned and fixed, it is time-consuming and labor-intensive. In view of this, we propose a double-end synchronous welding device for aircraft load-bearing rod processing. Summary of the invention

[0003] The purpose of the present invention is to provide a double-end synchronous welding device for processing aircraft load-bearing rods to solve the problems raised in the above background technology. To achieve the above purpose, the present invention provides the following technical solutions: a double-end synchronous welding device for processing aircraft load-bearing rods, comprising a base, and also comprising:

[0004] A conveying mechanism is fixed on the base through a bracket 1, and a plurality of clamping components 1 and 2 for clamping the rod body and the connecting joint are arranged on the conveying mechanism, and the clamping components 1 and 2 are arranged one by one correspondingly, the clamping component 1 includes a clamping claw for clamping the rod body, and the clamping component 2 includes two rotating drums for clamping the connecting joint;

[0005] The motor and the welding machine are fixed on the bracket 2, and the bracket 2 is fixed on the base. Two brackets are provided and are symmetrically arranged on both sides of the conveying mechanism. The output shaft end of the motor is coaxially fixedly connected to the turntable 1 and the turntable 2. An arc-shaped rack 1 is fixed on a peripheral wall of the turntable, and the rotating drum is intermittently driven to rotate through the arc-shaped rack 1. An arc-shaped rack 2 is fixed on a peripheral wall of the turntable 2, and the conveying mechanism is driven to operate through the arc-shaped rack 2.

[0006] Preferably, the conveying mechanism includes a frame fixed on a bracket one, and rollers are rotatably connected to both ends of the frame. The two rollers are connected through a conveyor belt transmission, and multiple groups of clamping components one and clamping components two are arranged on the conveyor belt at equal intervals along the length direction of the conveyor belt, and grooves corresponding to the clamping components one are provided on the upper and lower surfaces of the frame.

[0007] Preferably, the clamping assembly 1 also includes two groups of support rods 2 fixed on the conveyor belt, and each group of support rods 2 has two support rods, and the upper ends of the support rods 2 are connected with clamping claws, the clamping claws on each group of support rods 2 are symmetrically arranged, and the lower ends of the clamping claws are fixed with shifting rods, and the two shifting rods are cross-arranged, and strip-shaped through holes are opened on the shifting rods.

[0008] Preferably, a convex rod is slidably connected between each pair of second support rods, and a sliding rod is fixed in the middle of the convex rod. The convex rod is connected to the conveyor belt through a second spring. One end of the sliding rod pointing to the clamping jaw is fixed with a first pin rod, and the first pin rod is inserted and slidably connected in two corresponding strip-shaped through holes at the same time. One end of the sliding rod away from the first pin rod penetrates and is slidably connected to the conveyor belt, and this end is located in the corresponding groove. A second pin rod is fixed at one end of the sliding rod located in the groove. A straight groove is formed on the inner wall of the groove, and a V-shaped groove is also formed on the inner wall of the groove on the upper surface of the frame corresponding to the position of the welding machine. Both ends of the V-shaped groove are connected to the corresponding straight groove, and the second pin rod is slidably connected in the V-shaped groove and the straight groove.

[0009] Preferably, the second clamping assembly further includes two slide rails fixed on the surface of the conveyor belt, and the two slide rails are symmetrically arranged on both sides of the corresponding first clamping assembly. A slide seat is slidably connected to the slide rails, and a second shaft bracket is fixed on the slide seat. The two rotating cylinders are fixedly connected to the two second shaft brackets by fixed axes, and gear three is coaxially fixed to the opposite ends of the two rotating cylinders.

[0010] Preferably, one end of the rotating cylinder facing away from gear three is open, and a magnetic block is fixed in the middle of the inner wall of the rotating cylinder. A plurality of gear fours are rotatably connected to the peripheral wall of the rotating cylinder by fixed axes, and the plurality of gear fours are arranged at equal intervals along the circumferential direction of the rotating cylinder. A screw rod passes through and is threadedly connected to the center of the gear four, and one end of the screw rod pointing to the central axis of the rotating cylinder is fixedly connected with a clamping plate. A guide rod parallel to the screw rod is fixed on the side of the clamping plate facing away from the central axis of the rotating cylinder, and the guide rod penetrates and is slidably connected to the side wall of the rotating cylinder.

[0011] Preferably, a first toothed ring is sleeved and rotatably connected to the peripheral wall of the rotating cylinder, and a second toothed ring is fixed on the annular surface of the first toothed ring. The second toothed ring is meshed with each gear four. A gear six is rotatably connected to the peripheral wall of the rotating cylinder by a fixed axis, and the gear six is meshed with the first toothed ring. One end of the slide rail facing away from the second clamping assembly is fixed with a first support rod, and a twist rod is fixed on the first support rod. An avoidance hole is formed on the second shaft bracket, and the twist rod passes through the avoidance hole and then penetrates and is slidably connected to the center of the gear six.

[0012] Preferably, a cylinder is fixed on the second support, and the piston rod end of the cylinder can be in contact with the slide seat. One end of the slide rail facing the second clamping assembly is fixed with a third touch switch, and the slide seat can be in contact with the third touch switch. The slide seat is connected to one end of the slide rail facing the second clamping assembly through a first spring.

[0013] Preferably, a shaft rod is rotatably connected to the second support by a fixed axis. A gear one and a gear two are coaxially fixed to both ends of the shaft rod respectively. The first arc-shaped rack can be meshed with the gear one, and the gear three can be meshed with the gear two. A first touch rod is fixed on the disk surface of the gear two. A first touch switch is fixed on the second support, and the first touch rod can be in contact with the first touch switch.

[0014] Preferably, a shaft bracket one is fixed on the bracket one, and a gear five is rotatably connected to the shaft bracket one. The gear five is drivingly connected to one of the drums through a pulley assembly. A contact rod two is fixed on the gear five, and a touch switch two is fixed on the shaft bracket one, and the contact rod two can be in abutting contact with the touch switch two.

[0015] Compared with the prior art, the beneficial effects of the present invention are as follows:

[0016] In the present invention, the clamping assembly one and the clamping assembly two are respectively arranged to clamp and fix the connecting joint and the rod body. The motor drives the turntable one and the turntable two to work synchronously, so that the turntable two intermittently drives the conveying mechanism to convey each component of the load-bearing rod. When it is conveyed to the welding station, the cylinder drives the clamping assembly one to centeringly clamp the connecting joint, and the turntable one drives the rotating cylinder to rotate, so that the connecting joint and the rod body rotate synchronously, so that the welding machine performs circular welding on the connection part. After the welding is completed, the clamping assembly one releases and resets the connecting joint, and the turntable two drives the conveying mechanism to convey the components of the load-bearing rod to be welded downward again, and the clamping assembly two releases the welded load-bearing rod, so as to be taken off, realizing automatic centering clamping of the connecting joints at both ends of the rod body and synchronous rotary welding, thereby greatly improving the working efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 is a schematic cross-sectional structure diagram of the general assembly of the present invention Figure 1 ;

[0018] Figure 2 is a schematic cross-sectional structure diagram of the general assembly of the present invention Figure 2 ;

[0019] Figure 3 is Figure 1 an enlarged schematic structural diagram of part A in

[0020] Figure 4 is Figure 1 a schematic cross-sectional structure diagram of section B-B in

[0021] Figure 5 is a schematic side view of the structures of the turntable one, the turntable two and the gear five in the present invention;

[0022] Figure 6 is a schematic diagram of the structures of the frame, the conveyor belt and the drum in the present invention;

[0023] Figure 7 is a schematic diagram of the open state structure of the clamping assembly one in the present invention.

[0024] In the figure: 1, base; 2, first bracket; 3, frame; 4, conveyor belt; 5, groove; 6, first clamping assembly; 7, second clamping assembly; 8, second bracket; 9, cylinder; 10, motor; 11, shaft rod; 12, first gear; 13, second gear; 14, rotating cylinder; 15, third gear; 16, welding machine; 17, pulley assembly; 18, first turntable; 19, first shaft bracket; 20, second turntable; 21, slide rail; 22, first support rod; 23, first touch switch; 24, first spring; 25, sliding seat; 26, avoidance hole; 27, twist rod; 28, second shaft bracket; 29, first contact rod; 30, third touch switch; 31, magnetic block; 32, clamping plate; 33, screw rod; 34, guide rod; 35, first gear ring; 36, second gear ring; 37, fourth gear; 38, first arc-shaped rack; 39, second arc-shaped rack; 40, fifth gear; 41, second contact rod; 42, second touch switch; 43, roller; 44, straight groove; 45, V-shaped groove; 46, second support rod; 47, clamping jaw; 48, lever; 49, strip-shaped through hole; 50, slide bar; 51, convex rod; 52, second spring; 53, first pin rod; 54, second pin rod; 55, sixth gear. Detailed implementation manner

[0025] Next, the technical solutions in the embodiments of the present invention will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0026] Please refer to Figures 1 to 7 , the present invention provides a technical solution: a double-end synchronous welding device for processing aircraft load-bearing rods, including a base 1, and further including:

[0027] A conveying mechanism fixed to the base 1 through the first bracket 2, and multiple groups of first clamping assemblies 6 and second clamping assemblies 7 for clamping the rod body and the connecting joint are arranged on the conveying mechanism, and the first clamping assemblies 6 and the second clamping assemblies 7 are arranged in one-to-one correspondence. The first clamping assembly 6 includes a clamping jaw 47 for clamping the rod body, and the second clamping assembly 7 includes two rotating cylinders 14 for clamping the connecting joint;

[0028] A motor 10 and a welding machine 16 fixed to the second bracket 8, and the second bracket 8 is fixed to the base 1. There are two second brackets 8, which are symmetrically arranged on both sides of the conveying mechanism. The output shaft end of the motor 10 is coaxially and fixedly connected to the first turntable 18 and the second turntable 20. An arc-shaped rack 38 is fixed on the circumferential wall of the first turntable 18, and the rotating cylinder 14 is intermittently driven to rotate through the arc-shaped rack 38. An arc-shaped rack 39 is fixed on the circumferential wall of the second turntable 20, and the conveying mechanism is driven to operate through the arc-shaped rack 39.

[0029] In this embodiment, the conveying mechanism includes a frame 3 fixed to the first bracket 2. Both ends of the frame 3 are rotatably connected to rollers 43 through fixed axes. The two rollers 43 are connected by a conveyor belt 4. A plurality of sets of the first clamping components 6 and the second clamping components 7 are arranged on the conveyor belt 4 at equal intervals along the length direction of the conveyor belt 4. Grooves 5 corresponding to the first clamping components 6 are formed on the upper and lower surfaces of the frame 3.

[0030] In this embodiment, the first clamping component 6 further includes two sets of second support rods 46 fixed to the conveyor belt 4. Each set of the second support rods 46 has two rods. The upper ends of the second support rods 46 are joined to form a clamping jaw 47. The clamping jaws 47 on each set of the second support rods 46 are symmetrically arranged. A dial rod 48 is fixed to the lower end of the clamping jaw 47. The two dial rods 48 are cross - arranged. A strip - shaped through - hole 49 is formed in the dial rod 48. A convex rod 51 is slidably connected between each set of the second support rods 46. A sliding rod 50 is fixed to the middle of the convex rod 51. The convex rod 51 is connected to the conveyor belt 4 through a second spring 52. One end of the sliding rod 50 pointing to the clamping jaw 47 is fixed with a first pin 53. The first pin 53 is inserted into and slidably connected to the corresponding two strip - shaped through - holes 49 at the same time. The end of the sliding rod 50 away from the first pin 53 penetrates and is slidably connected to the conveyor belt 4, and this end is located in the corresponding groove 5. A second pin 54 is fixed to the end of the sliding rod 50 located in the groove 5. A straight groove 44 is formed on the inner wall of the groove 5. A V - shaped groove 45 is further formed on the inner wall of the groove 5 on the upper surface of the frame 3 corresponding to the position of the welding machine 16. The two ends of the V - shaped groove 45 are connected to the corresponding straight groove 44. The second pin 54 is slidably connected in the V - shaped groove 45 and the straight groove 44.

[0031] In this embodiment, the second clamping component 7 further includes two slide rails 21 fixed to the surface of the conveyor belt 4. The two slide rails 21 are symmetrically arranged on both sides of the corresponding first clamping component 6. A slide seat 25 is slidably connected to the slide rails 21. An axle support two 28 is fixed to the slide seat 25. Two rotating cylinders 14 are rotatably connected to the two axle supports two 28 through fixed axes. Gear three 15 is coaxially fixed to the opposite ends of the two rotating cylinders 14.

[0032] In this embodiment, the end of the rotating drum 14 away from the gear three 15 is open, and a magnetic block 31 is fixed in the middle of the inner wall of the rotating drum 14, and a plurality of gears 37 are rotatably connected to the peripheral wall of the rotating drum 14. The plurality of gears 37 are arranged at equal intervals along the circumferential direction of the rotating drum 14, and a screw 33 passes through the center of the gear four 37 and is threadedly connected, and a clamping plate 32 is fixedly connected to one end of the screw 33 pointing to the central axis of the rotating drum 14, and a guide rod 34 parallel to the screw 33 is fixed on the side of the clamping plate 32 away from the central axis of the rotating drum 14, and the guide rod 34 passes through and is slidably connected to the rotating drum 1 4, a gear ring 1 35 is sleeved on the circumferential wall of the rotating drum 14 and is connected to the fixed axis rotation, and a gear ring 2 36 is fixed on the annular surface of the gear ring 1 35, and the gear ring 2 36 is meshed with each gear 4 37, and a gear 6 55 is connected to the circumferential wall of the rotating drum 14 for fixed axis rotation, and the gear 6 55 is meshed with the gear ring 1 35, a support rod 1 22 is fixed to the end of the slide rail 21 away from the clamping assembly 27, and a twisted rod 27 is fixed on the support rod 1 22, and an avoidance hole 26 is opened on the shaft frame 28, and the twisted rod 27 passes through the avoidance hole 26 and then penetrates and is slidably connected to the center of the gear 6 55.

[0033] In this embodiment, a cylinder 9 is fixed on the bracket 28, and the piston rod end of the cylinder 9 can be in contact with the slide seat 25. A touch switch 30 is fixed to the end of the slide rail 21 pointing to the clamping component 27, and the slide seat 25 can be in contact with the touch switch 30. The slide seat 25 is connected to the end of the slide rail 21 pointing to the clamping component 27 through a spring 1 24.

[0034] In this embodiment, a shaft rod 11 is rotatably connected to bracket 2 8, and the two ends of the shaft rod 11 are coaxially fixedly connected to gear 1 12 and gear 2 13 respectively. The arc rack 1 38 can be meshed and connected with gear 1 12, and gear 3 15 can be meshed and connected with gear 2 13. A touch rod 1 29 is fixed on the disk surface of gear 2 13, and a touch switch 1 23 is fixed on bracket 2 8, and the touch rod 1 29 can be in contact with the touch switch 1 23.

[0035] In this embodiment, an axis frame 19 is fixed on the bracket 2, and a gear 5 40 is rotatably connected to the axis frame 19. The gear 5 40 is transmission-connected to one of the rollers 43 through a pulley assembly 17. A touch rod 2 41 is fixed on the gear 5 40, and a touch switch 2 42 is fixed on the axis frame 19, and the touch rod 2 41 can be in contact with the touch switch 2 42.

[0036] Working principle and advantages of the present invention: When the double-end synchronous welding device for processing aircraft load-bearing rods is used, the working process is as follows:

[0037] like Figure 3 and Figure 7As shown, place the rod to be welded between each pair of jaws 47, place the connecting joint inside the corresponding rotating cylinder 14, and adsorb it on the magnet block 31. The magnet block 31 plays a role of pre-fixing. After welding is completed, the magnetic suction force of the magnet block 31 is not sufficient to move the load-bearing rod as a whole, and it will automatically detach. Start the motor 10 to work through the controller. As Figure 1 、 Figure 2 and Figure 5 shown, make the motor 10 drive the first turntable 18 and the second turntable 20 to rotate synchronously. At this time, the second turntable 20 drives the fifth gear 40 and the contact rod two 41 thereon to rotate through the second arc-shaped rack 39, so that the fifth gear 40 drives the corresponding roller 43 to rotate through the pulley assembly 17, thereby making the roller 43 drive the conveyor belt 4 to run, and further making the conveyor belt 4 drive the first clamping assembly 6 and the second clamping assembly 7 thereon to run synchronously. During this process, the first arc-shaped rack 38 does not contact the first gear 12, and the cylinder 9 is in a contracted state. The third gear 15 does not contact the second gear 13. When the fifth gear 40 rotates one circle, the contact rod two 41 contacts the second touch switch 42, and at this time the second arc-shaped rack 39 just disengages from the fifth gear 40 and does not contact, so that the fifth gear 40 stops driving the conveyor belt 4 to run. As Figure 4 shown, and at this time the second pin rod 54 slides from the straight groove 44 to the middle of the V-shaped groove 45. During this process, the second pin rod 54 drives the slide rod 50 to move downward, and applies a downward pressure to the two toggle levers 48 through the first pin rod 53, so that the toggle levers 48 drive the jaws 47 to clamp the rod.

[0038] As described above, the touch switch two 42 transmits the touch signal of the touch rod two 41 to the controller, and the controller controls the cylinder 9 to work, so that the cylinder 9 extends the piston rod and pushes the slide seat 25 to compress the first spring 24, so that the first spring 24 obtains a restoring force. At the same time, while the slide seat 25 moves on the slide rail 21, it drives the rotating cylinder 14 and the third gear 15 to move synchronously through the second shaft bracket 28, and under the action of the twist rod 27, the sixth gear 55 drives the first gear ring 35 to rotate, so that the first gear ring 35 drives each fourth gear 37 to rotate through the second gear ring 36. Furthermore, the fourth gear 37 drives the clamping plate 32 to approach the connection joint through the screw rod 33 and clamps the connection joint. At the same time, it automatically aligns the connection joint, so that the connection joint is coaxial with the end of the rod body and is in tight contact. When the slide seat 25 contacts the touch switch three 30, the twist rod 27 just does not contact the sixth gear 55. The touch switch three 30 transmits the touch signal of the slide seat 25 to the controller, and the controller controls the cylinder 9 to hold and starts the welder 16 to work. At this time, the third gear 15 just meshes with the second gear 13, and at the same time, the first arc-shaped rack 38 meshes with the first gear 12, so that the first turntable 18 drives the first gear 12 to rotate through the first arc-shaped rack 38. Thus, the first gear 12 drives the second gear 13 to rotate synchronously through the shaft rod 11, so that the second gear 13 drives the rotating cylinder 14 to rotate through the third gear 15. Furthermore, the rotating cylinder 14 drives the connection joint and the rod body to rotate synchronously, so that the welder 16 can weld the connection part in a circular path.

[0039] As described above, while the second gear 13 rotates, it drives the first contact rod 29 to rotate. When the first contact rod 29 rotates one circle and makes contact with the first touch switch 23, at this time, the rotating cylinder 14 drives the connecting joint and the rod body to rotate one circle to complete welding. At the same time, the first arc-shaped rack 38 just disengages from the first gear 12 and is not in contact. At this time, the first touch switch 23 transmits the touch signal of the first contact rod 29 to the controller. The controller controls the welding machine to stop working and controls the cylinder 9 to retract the piston rod. At this time, under the restoring force of the first spring 24, the sliding seat 25 slides reversely and resets, so that the sliding seat 25 drives the rotating cylinder 14 and the third gear 15 to reset through the second shaft bracket 28, so that the third gear 15 disengages from the second gear 13 and is not in contact. And under the action of the twist rod 27, the sixth gear 55 drives the first toothed ring 35 to rotate reversely, so that the first toothed ring 35 drives each fourth gear 37 to rotate reversely through the second toothed ring 36. Thus, the fourth gear 37 drives the clamp 32 to loosen the connecting joint and reset through the screw rod 33. At this time, the second arc-shaped rack 39 meshes with the fifth gear 40 again, so that the fifth gear 40 drives the corresponding roller 43 to rotate through the belt pulley assembly 17, so that the roller 43 drives the conveyor belt 4 to run, and outputs the load-bearing rod corresponding to the V-shaped groove 45 that has been processed, and at the same time transfers each component of the next load-bearing rod to be welded to the V-shaped groove 45. During the process of the second pin rod 54 moving from the V-shaped groove 45 to the straight groove 44, the second pin rod 54 drives the slide bar 50 to move upward, and the slide bar 50 applies a thrust to the two toggle levers 48 through the first pin rod 53, so that the toggle levers 48 drive the jaws 47 to open, so as to remove the welded load-bearing rod. In this way, it only needs to place the connecting joint and the rod body on the corresponding first clamping assembly 6 and the second clamping assembly 7 in front of the welding station, and then realize automatic centering clamping of the connecting joints at both ends of the rod body and synchronous rotary welding, thus greatly improving work efficiency. Just remove the welded load-bearing rod at the back of the welding station, and the operation is simple and convenient.

[0040] For those skilled in the art, it is obvious that the present invention is not limited to the details of the above-described exemplary embodiments, and can be implemented in other specific forms without departing from the spirit or basic characteristics of the present invention. Therefore, from any point of view, the embodiments should be regarded as exemplary and non-limiting. The scope of the present invention is defined by the appended claims rather than the above description. Therefore, it is intended to embrace all changes falling within the meaning and scope of the equivalent elements of the claims in the present invention. Any reference signs in the claims should not be regarded as limiting the claimed rights.

[0041] In the description of the present invention, unless otherwise specified, "a plurality of" means two or more; the orientation or positional relationship indicated by the terms "upper", "lower", "left", "right", "inner", "outer", "front end", "rear end", "head", "tail", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus cannot be construed as a limitation on the present invention. In addition, the terms "first", "second", "third", etc. are only used for descriptive purposes and cannot be construed as indicating or implying relative importance.

[0042] In the description of the present invention, it should be noted that, unless otherwise clearly specified and defined, the terms "connected" and "coupled" should be understood in a broad sense. For example, it may be a fixed connection, a detachable connection, or an integral connection; it may be a mechanical connection or an electrical connection; it may be directly connected or indirectly connected through an intermediate medium. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

Claims

1. A double-end synchronous welding device for processing an aircraft load-bearing rod, comprising a base (1), characterized in that: Also includes: A conveying mechanism fixed to the base (1) by a bracket (2), and provided with a plurality of groups of clamping assemblies (1) and (2) for clamping the rod body and the connecting joint, wherein the clamping assemblies (1) and (2) (7) are arranged in a one-to-one correspondence, wherein the clamping assemblies (1) (6) include clamping claws (47) for clamping the rod body, and the clamping assemblies (2) (7) include two rotating drums (14) for clamping the connecting joint; A motor (10) and a welding machine (16) are fixed on a second bracket (8), and the second bracket (8) is fixed on a base (1). Two second brackets (8) are provided and are symmetrically arranged on both sides of a conveying mechanism. The output shaft end of the motor (10) is coaxially fixedly connected to a turntable (18) and a turntable (20). An arc-shaped rack (38) is fixed on the peripheral wall of the turntable (18), and the arc-shaped rack (38) drives the rotating drum (14) to rotate intermittently. An arc-shaped rack (39) is fixed on the peripheral wall of the turntable (20), and the arc-shaped rack (39) drives the conveying mechanism to operate; The conveying mechanism comprises a frame (3) fixed on a bracket 1 (2), both ends of the frame (3) are rotatably connected to rollers (43), the two rollers (43) are connected by a conveyor belt (4), and a plurality of groups of the clamping assembly 1 (6) and the clamping assembly 2 (7) are arranged on the conveyor belt (4) at equal intervals along the length direction of the conveyor belt (4), and the upper and lower surfaces of the frame (3) are provided with grooves (5) corresponding to the clamping assembly 1 (6); The clamping assembly (2) (7) further comprises two slide rails (21) for fixing the surface of the conveyor belt (4), and the two slide rails (21) are symmetrically arranged on both sides of the corresponding clamping assembly (6), a slide seat (25) is slidably connected to the slide rail (21), and a shaft frame (28) is fixed to the slide seat (25), the two rotating drums (14) are rotatably connected to the two shaft frames (28), and the opposite ends of the two rotating drums (14) are coaxially fixedly connected to the gear (15); The end of the rotating drum (14) facing away from the gear three (15) is open, and a magnetic block (31) is fixed in the middle of the inner wall of the rotating drum (14); a plurality of gear fours (37) are rotatably connected to the peripheral wall of the rotating drum (14); the plurality of gear fours (37) are arranged at equal intervals along the circumferential direction of the rotating drum (14); a screw rod (33) passes through the center of the gear four (37) and is threadedly connected; a clamping plate (32) is fixedly connected to one end of the screw rod (33) pointing to the central axis of the rotating drum (14); a guide rod (34) parallel to the screw rod (33) is fixed on the side of the clamping plate (32) facing away from the central axis of the rotating drum (14); and the guide rod (34) passes through and is slidably connected to the side wall of the rotating drum (14); A gear ring 1 (35) is sleeved on the peripheral wall of the rotating drum (14) and is connected to the rotating drum in a fixed axis, and a gear ring 2 (36) is fixed on the annular surface of the gear ring 1 (35), and the gear ring 2 (36) is meshingly connected with each gear 4 (37). A gear 6 (55) is connected to the peripheral wall of the rotating drum (14) in a fixed axis, and the gear 6 (55) is meshingly connected with the gear ring 1 (35). A support rod 1 (22) is fixed to the end of the slide rail (21) away from the clamping assembly 2 (7), and a twisted rod (27) is fixed on the support rod 1 (22). A avoidance hole (26) is opened on the shaft frame 2 (28), and the twisted rod (27) passes through the avoidance hole (26) and then penetrates and is slidably connected to the center of the gear 6 (55).

2. The double-end synchronous welding device for processing aircraft load-bearing rods according to claim 1, characterized in that: The clamping assembly (6) further comprises two groups of supporting rods (46) fixed on the conveyor belt (4), each group of supporting rods (46) comprising two supporting rods, and the upper ends of the supporting rods (46) are connected with clamping claws (47), the clamping claws (47) on each group of supporting rods (46) are symmetrically arranged, and the lower ends of the clamping claws (47) are fixed with shifting rods (48), and the two shifting rods (48) are cross-arranged, and the shifting rods (48) are provided with strip-shaped through holes (49).

3. The double-end synchronous welding device for processing aircraft load-bearing rods according to claim 2, characterized in that: A convex rod (51) is slidably connected between each set of supporting rods (46), and a sliding rod (50) is fixed in the middle of the convex rod (51). The convex rod (51) is connected to the conveyor belt (4) through a spring (52). A pin rod (53) is fixed at one end of the sliding rod (50) pointing to the clamping claw (47), and the pin rod (53) is simultaneously inserted and slidably connected in the corresponding two bar-shaped through holes (49). The end of the sliding rod (50) away from the pin rod (53) penetrates and is slidably connected to the conveyor belt (4). ), and the end is located in the corresponding groove (5), one end of the slide bar (50) located in the groove (5) is fixed with a pin rod 2 (54), a straight groove (44) is provided on the inner wall of the groove (5), and a V-shaped groove (45) is also provided on the inner wall of the groove (5) located on the upper surface of the frame (3) at a position corresponding to the welding machine (16), and both ends of the V-shaped groove (45) are connected to the corresponding straight groove (44), and the pin rod 2 (54) is slidably connected in the V-shaped groove (45) and the straight groove (44).

4. The double-end synchronous welding device for processing aircraft load-bearing rods according to claim 1, characterized in that: A cylinder (9) is fixed on the bracket (8), and the piston rod end of the cylinder (9) can be in contact with the slide seat (25). A touch switch (30) is fixed to the end of the slide rail (21) pointing to the clamping component (7), and the slide seat (25) can be in contact with the touch switch (30). The slide seat (25) is connected to the end of the slide rail (21) pointing to the clamping component (7) through a spring (24).

5. The double-end synchronous welding device for processing aircraft load-bearing rods according to claim 1, characterized in that: The bracket 2 (8) is fixedly rotatably connected to a shaft rod (11), and the two ends of the shaft rod (11) are coaxially fixedly connected to a gear 1 (12) and a gear 2 (13), respectively. The arc-shaped rack 1 (38) can be meshedly connected to the gear 1 (12), and the gear 3 (15) can be meshedly connected to the gear 2 (13). A touch rod 1 (29) is fixed on the disk surface of the gear 2 (13). A touch switch 1 (23) is fixed on the bracket 2 (8), and the touch rod 1 (29) can be in contact with the touch switch 1 (23).

6. The double-end synchronous welding device for processing aircraft load-bearing rods according to claim 1, characterized in that: Axle frame one (19) is fixed on the bracket one (2), and a gear five (40) is fixedly rotatably connected to the shaft frame one (19), the gear five (40) is transmission-connected to one of the rollers (43) via a pulley assembly (17), a touch rod two (41) is fixed on the gear five (40), a touch switch two (42) is fixed on the shaft frame one (19), and the touch rod two (41) can be in contact with the touch switch two (42).

Citation Information

Patent Citations

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