CN220259941U - Aviation pipe fitting welding set - Google Patents
Aviation pipe fitting welding set Download PDFInfo
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- CN220259941U CN220259941U CN202321389515.6U CN202321389515U CN220259941U CN 220259941 U CN220259941 U CN 220259941U CN 202321389515 U CN202321389515 U CN 202321389515U CN 220259941 U CN220259941 U CN 220259941U
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- bearing
- pipe fitting
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- 238000003466 welding Methods 0.000 title claims abstract description 47
- 230000001681 protective effect Effects 0.000 claims description 9
- 239000002699 waste material Substances 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 238000005493 welding type Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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- Butt Welding And Welding Of Specific Article (AREA)
Abstract
The utility model relates to an aviation pipe fitting welding device in the technical field of welding devices, which comprises a bottom plate, wherein a first limiting block is fixedly connected to one side of the top end of the bottom plate, a second limiting block is fixedly connected to the other side of the top end of the bottom plate, a servo motor is fixedly connected to one side of the second limiting block, a first gear is fixedly connected to the output end of the servo motor, a second gear is connected to the first gear in a meshed manner, a connecting block is fixedly connected to the surface of the third gear, a sliding rod is fixedly connected to the top end of the connecting block, limiting plates are fixedly connected to the upper end and the lower end of the sliding rod, and welding heads are connected to the surface of the sliding rod in a sliding manner. The servo motor, the first gear, the second gear, the third gear, the second bearing, the connecting block and the welding head are arranged, so that the third gear can rotate, the third gear drives the welding head to rotate on the outer surface of the pipe fitting, welding between two pipe fittings is facilitated, time and labor waste are avoided, and welding efficiency is improved.
Description
Technical Field
The utility model relates to the technical field of welding devices, in particular to an aviation pipe fitting welding device.
Background
The aircraft sheet metal parts can be divided into three types, namely extrusion profile parts, plate parts and aviation pipe parts.
The variety of pipe fittings is very many, and according to the processing technology difference, divide into four major categories: welding type pipe fitting, socket joint welding pipe fitting, screw thread pipe fitting and flange pipe fitting, at the in-process of welding type pipe fitting processing, adopt the manual work to weld the pipe fitting generally, welding efficiency is lower, and current most welding set can't directly weld the pipe fitting, generally needs manual hand welding set to weld the circumference to the pipe fitting, welds two pipe fittings together, and the mode is more physical power and time consuming to lead to welding efficiency to reduce, for this reason we propose an aviation pipe fitting welding set.
Disclosure of Invention
In view of the above problems, the utility model provides an aviation pipe fitting welding device, which has the advantages of being convenient for pipe fitting welding, saving time and labor and improving welding efficiency.
The technical scheme of the utility model is as follows:
the utility model provides an aviation pipe fitting welding set, includes the bottom plate, top one side fixedly connected with stopper first of bottom plate, the top opposite side fixedly connected with stopper second of bottom plate, one side fixedly connected with servo motor of stopper second, servo motor's output fixedly connected with first gear, first gear engagement is connected with the second gear, second gear engagement is connected with the third gear, the round hole has been seted up on the surface of third gear, the inner wall rotation of round hole is connected with bearing second, the fixed surface of third gear is connected with the connecting block, the top fixedly connected with slide bar of connecting block, the equal fixedly connected with limiting plate in upper and lower both ends of slide bar, the surface sliding connection of slide bar has the soldered connection.
In further technical scheme, the surface cover of slide bar is equipped with the slider, the surface cover of slide bar is equipped with reset spring one, reset spring one's bottom fixed connection is at the upper surface of slider, the other end fixedly connected with protecting crust one of slider, logical groove has been seted up to protecting crust one's bottom, logical inslot fixedly connected with reset spring two, reset spring two's bottom fixedly connected with gleitbretter, the bottom fixed connection pillar of gleitbretter, the bottom fixedly connected with protecting crust two of pillar, protecting crust two's bottom rotation is connected with the pivot.
In a further technical scheme, the surface of the first limiting block is provided with a groove, the surface of the second limiting block, which is close to the first limiting block, is provided with a first through hole and a circular groove, and the first through hole is located on one side of the circular groove.
In a further technical scheme, the inner wall of the circular groove is rotationally connected with a first bearing, the inner wall of the first bearing is rotationally connected with a bearing rod, one end of the bearing rod is fixedly connected to one side of the second gear, and the inner wall of the first through hole is rotationally connected to the outer surface of the second bearing.
In a further technical scheme, a sliding groove is formed in one side surface of the sliding block, the inner wall of the sliding groove is slidably connected to the outer surface of the sliding rod, and the top end of the first reset spring is fixedly connected to the lower surface of the limiting plate.
In a further technical scheme, one side of the first protecting shell is fixedly connected with a connecting rod, and the bottom end of the connecting rod is fixedly connected to the top end of the welding head.
In a further technical scheme, the inner wall of the second protecting shell is fixedly connected with a connecting shaft, two ends of the rotating shaft are provided with second through holes, and the outer surface of the connecting shaft is rotationally connected to the inner wall of the second through holes.
The beneficial effects of the utility model are as follows:
1. the third gear can rotate through the arranged servo motor, the first gear, the second gear, the third gear, the second bearing, the connecting block and the welding head, the third gear can drive the welding head to rotate on the outer surface of the pipe fitting, welding between two pipe fittings is facilitated, time and labor waste are avoided, and meanwhile welding efficiency is improved;
2. the first reset spring, the sliding block, the first protective shell, the second reset spring, the support column, the second protective shell and the rotating shaft are arranged, so that the welding head can rotate on the outer surface of the pipe fitting, one end of the welding head is tightly attached to the outer surface of the pipe fitting, and the welding head can conveniently weld the pipe fitting.
Drawings
FIG. 1 is a schematic overall structure of an embodiment of the present utility model;
FIG. 2 is a schematic diagram of a first limiting block according to an embodiment of the present utility model;
FIG. 3 is a schematic view showing the position structure of the through hole I and the circular groove according to the embodiment of the utility model;
FIG. 4 is a schematic diagram of the structure of a second gear and a third gear according to an embodiment of the present utility model;
fig. 5 is a schematic view of the position structures of the first return spring and the second return spring according to the embodiment of the present utility model.
Reference numerals illustrate:
1. a bottom plate; 2. a first limiting block; 3. a second limiting block; 4. a groove; 5. a first through hole; 6. a circular groove; 7. a servo motor; 8. a first gear; 9. a second gear; 10. a bearing rod; 11. a first bearing; 12. a third gear; 13. a round hole; 14. a second bearing; 15. a connecting block; 16. a slide bar; 17. a limiting plate; 18. a first reset spring; 19. a slide block; 20. a chute; 21. a first protective shell; 22. a connecting rod; 23. a welding head; 24. a second reset spring; 25. a sliding sheet; 26. a support post; 27. a second protective shell; 28. a connecting shaft; 29. a rotating shaft; 30. and a second through hole.
Detailed Description
Embodiments of the present utility model are further described below with reference to the accompanying drawings.
Examples:
as shown in fig. 1-5, an aviation pipe fitting welding device comprises a bottom plate 1, a first limiting block 2 is fixedly connected to one side of the top end of the bottom plate 1, a groove 4 is formed in the surface of the first limiting block 2, a second limiting block 3 is fixedly connected to the other side of the top end of the bottom plate 1, a first through hole 5 and a round groove 6 are formed in the surface of the second limiting block 3, which is close to the first limiting block 2, the first through hole 5 is positioned on one side of the round groove 6, a servo motor 7 is fixedly connected to one side of the second limiting block 3, a first gear 8 is fixedly connected to the output end of the servo motor 7, a second gear 9 is in meshed connection with the first gear 8, a bearing rod 10 is fixedly connected to the surface of one side of the second gear 9, a first bearing 11 is rotatably connected to the outer surface of one end of the bearing rod 10, the outer surface of the first bearing 11 is rotatably connected to the inner wall of the round groove 6, a third gear 12 is in meshed connection with the second gear 9, the surface of the third gear 12 is provided with a round hole 13, the inner wall of the round hole 13 is rotationally connected with a second bearing 14, the surface of the third gear 12 is fixedly connected with a connecting block 15, the top end of the connecting block 15 is fixedly connected with a sliding rod 16, the outer surface of the sliding rod 16 is sleeved with a first protecting shell 18, the upper end and the lower end of the sliding rod 16 are fixedly connected with limiting plates 17, the outer surface of the sliding rod 16 is sleeved with a sliding block 19, one side surface of the sliding block 19 is provided with a sliding groove 20, the inner wall of the sliding groove 20 is slidingly connected with the outer surface of the sliding rod 16, the top end of the first protecting shell 18 is fixedly connected with the lower surface of the limiting plates 17, the bottom end of the first protecting shell 18 is fixedly connected with the upper surface of the sliding block 19, the other end of the sliding block 19 is fixedly connected with a first protecting shell 21, one side of the protecting shell 21 is fixedly connected with a connecting rod 22, the bottom end of the connecting rod 22 is fixedly connected with a welding head 23, the bottom end of the protecting shell 21 is provided with a through groove, the reset spring II 24 is fixedly connected in the through groove, the sliding vane 25 is fixedly connected at the bottom end of the reset spring II 24, the support column 26 is fixedly connected at the bottom end of the sliding vane 25, the second protective shell 27 is fixedly connected at the bottom end of the support column 26, the connecting shaft 28 is fixedly connected to the inner wall of the second protective shell 27, the rotating shaft 29 is rotatably connected to the outer surface of the connecting shaft 28, the through holes II 30 are formed in the two ends of the rotating shaft 29, and the outer surface of the connecting shaft 28 is rotatably connected to the inner wall of the through holes II 30.
The working principle of the technical scheme is as follows:
when the aviation pipe fitting is required to be welded, firstly, a section of pipe fitting is placed on the surface of the first limiting block 2, the outer surface of the pipe fitting is tightly attached to the inner wall of the groove 4, a section of pipe fitting is placed in the first through hole 5, the pipe fitting of the second section penetrates through the inner wall of the second bearing 14, the rotating shaft 29 is pushed upwards, the rotating shaft 29 drives the second protecting shell 27 and the supporting column 26, the sliding vane 25 slides on the inner wall of the through groove, the sliding vane 25 can push the second restoring spring 24, the second restoring spring 24 performs extrusion deformation, the bottom end of the sliding vane 25 with the through groove slides to the top end of the through groove, one end of the second pipe fitting is tightly attached to one end of the pipe fitting, the sliding vane 25 can slide from the top end of the through groove to the bottom end of the through groove due to rebound resilience of the second restoring spring 24, the sliding vane 25 can drive the supporting column 26 and the second protecting shell 27, the outer surface of the rotating shaft 29 is tightly attached to the outer surface of the pipe fitting, at this time, the servo motor 7 is driven, the output end of the servo motor 7 drives the first gear 8 to rotate, the second gear 9 which is meshed with the first gear 8 is rotated, when the second gear 9 rotates, the bearing rod 10 can be driven to rotate on the inner wall of the first bearing 11, the second gear 9 can be driven to rotate the third gear 12 which is meshed with the second gear 9, when the third gear 12 rotates, the inner wall of the round hole 13 can be driven to rotate on the outer surface of the second bearing 14, the rotating third gear 12 can drive the connecting block 15 to rotate, meanwhile, the welding head 23 is driven to rotate on the outer surface of the pipe fitting, when the welding head 23 rotates, the rotating shaft 29 can be driven to rotate on the outer surface of the connecting shaft 28, the outer surface of the rotating shaft 29 can be driven to rotate on the outer surface of the pipe fitting, the welding head 23 can weld pipe fittings with different diameters, but the welding head 23 can not accurately weld the pipe fittings with different diameters, the pivot 29 that sets up at this moment can rotate the surface at the pipe fitting, make through-hole two 30 rotate the surface at connecting axle 28, simultaneously the pipe fitting extrudees pivot 29, make pillar 26 slide the inner wall in logical groove, can drive the gleitbretter 25 and slide the inner wall in logical groove, can make gleitbretter 25 upwards move, extrude reset spring two 24, when the diameter of pipe fitting is great, can make protective housing one 21 drive slider 19 upwards move, make spout 20 slide the surface at slide bar 16, thereby can extrude reset spring one 18, reset spring one 18 has the resilience, can make reset spring one 18 promote slider 19, make the inner wall of spout 20 carry out the downmovement at the surface of slide bar 16, simultaneously reset spring two 24 can promote pillar 26, make the surface of pivot 29 carry out the inseparable laminating with the surface of pipe fitting, can weld the pipe fitting of different diameters, this device's setting is convenient for weld the pipe fitting, and labour saving and time saving can improve welding efficiency.
The foregoing examples merely illustrate specific embodiments of the utility model, which are described in greater detail and are not to be construed as limiting the scope of the utility model. It should be noted that it will be apparent to those skilled in the art that several variations and modifications can be made without departing from the spirit of the utility model, which are all within the scope of the utility model.
Claims (7)
1. Aviation pipe fitting welding set, including bottom plate (1), its characterized in that: the utility model discloses a welding device for the electric motor of the motor vehicle, including bottom plate (1), first gear (9) of top one side fixedly connected with stopper (2), top opposite side fixedly connected with stopper two (3) of bottom plate (1), one side fixedly connected with servo motor (7) of stopper two (3), the output fixedly connected with first gear (8) of servo motor (7), first gear (8) meshing is connected with second gear (9), second gear (9) meshing is connected with third gear (12), round hole (13) have been seted up on the surface of third gear (12), the inner wall rotation of round hole (13) is connected with bearing two (14), the fixed surface of third gear (12) is connected with connecting block (15), the top fixedly connected with slide bar (16) of connecting block (15), the equal fixedly connected with limiting plate (17) in upper and lower both ends of slide bar (16), the surface sliding connection of slide bar (16) has welding head (23).
2. An aerospace tube welding apparatus according to claim 1, wherein: the outer surface cover of slide bar (16) is equipped with slider (19), the surface cover of slide bar (16) is equipped with reset spring one (18), the bottom fixed connection of reset spring one (18) is at the upper surface of slider (19), the other end fixedly connected with protecting crust one (21) of slider (19), logical groove has been seted up to the bottom of protecting crust one (21), logical inslot fixedly connected with reset spring two (24), the bottom fixedly connected with gleitbretter (25) of reset spring two (24), the bottom fixed connection pillar (26) of gleitbretter (25), the bottom fixedly connected with protecting crust two (27) of pillar (26), the bottom rotation of protecting crust two (27) is connected with pivot (29).
3. An aerospace tube welding apparatus according to claim 1, wherein: the surface of the first limiting block (2) is provided with a groove (4), the surface of the second limiting block (3) close to the first limiting block (2) is provided with a first through hole (5) and a circular groove (6), and the first through hole (5) is located on one side of the circular groove (6).
4. An aerospace tube welding apparatus according to claim 3, wherein: the inner wall of circular slot (6) rotates and is connected with first bearing (11), the inner wall of first bearing (11) rotates and is connected with bearing rod (10), one end fixed connection of bearing rod (10) is in one side of second gear (9), the inner wall of through-hole one (5) rotates and is connected at the surface of second bearing (14).
5. An aerospace tube welding apparatus according to claim 2, wherein: a sliding groove (20) is formed in one side surface of the sliding block (19), the inner wall of the sliding groove (20) is slidably connected to the outer surface of the sliding rod (16), and the top end of the first return spring (18) is fixedly connected to the lower surface of the limiting plate (17).
6. An aerospace tube welding apparatus according to claim 2, wherein: one side of the first protective shell (21) is fixedly connected with a connecting rod (22), and the bottom end of the connecting rod (22) is fixedly connected with the top end of a welding head (23).
7. An aerospace tube welding apparatus according to claim 2, wherein: the inner wall of the second protective shell (27) is fixedly connected with a connecting shaft (28), two ends of the rotating shaft (29) are provided with a second through hole (30), and the outer surface of the connecting shaft (28) is rotationally connected to the inner wall of the second through hole (30).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321389515.6U CN220259941U (en) | 2023-06-02 | 2023-06-02 | Aviation pipe fitting welding set |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321389515.6U CN220259941U (en) | 2023-06-02 | 2023-06-02 | Aviation pipe fitting welding set |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220259941U true CN220259941U (en) | 2023-12-29 |
Family
ID=89315609
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321389515.6U Active CN220259941U (en) | 2023-06-02 | 2023-06-02 | Aviation pipe fitting welding set |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220259941U (en) |
-
2023
- 2023-06-02 CN CN202321389515.6U patent/CN220259941U/en active Active
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| GR01 | Patent grant | ||
| GR01 | Patent grant |