A thin-wall aviation aluminum alloy tube hole opening device

Through the gear system driven by the servo motor and the sliding column sliding rod mechanism, a hole opening device suitable for thin-wall aerospace aluminum alloy pipes is designed, which solves the problem of limited application scope of traditional devices and achieves a hole opening effect with high flexibility and stability.

CN222740447UActive Publication Date: 2025-04-11SUZHOU ZHIAO MASCH TECH CO LTD
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Patent Information

Application Number
CN202420324455.8
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-02-22
Publication Date
2025-04-11
Estimated Expiration
2034-02-22

AI Technical Summary

Technical Problem

The traditional thin-wall aerospace aluminum alloy pipe opening device cannot be suitable for a variety of aluminum alloy pipes of different sizes, which limits its application range.

Method used

A thin-wall aerospace aluminum alloy pipe opening device is designed, and the sliding column and sliding rod are driven to slide in the limit groove through the servo motor drive connection rod and gear system, achieving flexible adaptation to aluminum alloy pipes with different inner diameters, and preventing shaking through the cylinder support pipe body.

Benefits of technology

The device can adapt to a variety of aluminum alloy tubes, improves the application range and flexibility of the hole opening device, and stabilizes the hole opening process through the support device.

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Abstract

The utility model relates to the technical field of hole-opening devices, and discloses a hole-opening device for thin-walled aviation aluminum alloy tubes, including a hole-opening platform, an installation cavity is opened inside the hole-opening platform, a first servo motor is fixedly connected to the middle of the bottom surface of the installation cavity, and a rotating rod is fixedly connected to the output end of the first servo motor. In the utility model, when the hole-opening device for thin-walled aviation aluminum alloy tubes is used, the aluminum alloy tube is placed in a storage slot, and the second servo motor is started to drive the connecting rod to rotate while driving the driving gear to rotate, and the driving gear and the driven gear are meshed with each other, thereby driving the driven gear to rotate together, and the driven gear is rotated to drive multiple sliding columns to slide in the limit groove, so that the sliding rod is extended and retracted in the limit plate, and can flexibly adapt to aluminum alloy tubes of different inner diameters, which means that the same hole-opening device can be used to process aluminum alloy tubes of various sizes.
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Description

Technical Field

[0001] The utility model relates to the technical field of hole-opening devices, in particular to a hole-opening device for a thin-wall aviation aluminum alloy tube. Background Art

[0002] As we all know, thin-walled aviation aluminum alloy tube is a tubular component made of lightweight, high-strength aluminum alloy material. It has a small wall thickness and a large inner diameter, is light in weight and high in strength, and is commonly used in aerospace, automobile, shipbuilding and other fields. Thin-walled aviation aluminum alloy tube has excellent corrosion resistance and can be used for a long time in harsh environments without damage. Thin-walled aviation aluminum alloy tube usually needs to be processed by drilling holes to meet the connection requirements of different system pipes and accessories. The drilling device is a mechanical equipment specially used for drilling holes in thin-walled pipes.

[0003] However, traditional thin-wall aviation aluminum alloy tube hole opening devices are usually designed for aluminum alloy tubes of specific sizes and cannot be applied to aluminum alloy tubes of various sizes. This limits its scope of application and requires additional tools and devices to handle pipes of different sizes. Therefore, technical improvements are urgently needed. Utility Model Content

[0004] The purpose of the utility model is to solve the shortcomings existing in the prior art, and a thin-wall aviation aluminum alloy tube hole opening device is proposed. When the thin-wall aviation aluminum alloy tube hole opening device is used, the aluminum alloy tube is placed in a storage groove, and the second servo motor is started to drive the connecting rod to rotate while driving the driving gear to rotate, and the driving gear and the driven gear are meshed with each other, thereby driving the driven gear to rotate together, and the rotation of the driven gear drives multiple sliding columns to slide in the limit groove, so that the sliding rod can be extended and retracted in the limit plate, which can flexibly adapt to aluminum alloy tubes with different inner diameters. This means that the same hole opening device can be used to process aluminum alloy tubes of various sizes, thereby improving the application range and flexibility of the device. The support pad is driven to move by starting the cylinder, so as to support one side of the aluminum alloy tube to prevent shaking during the hole opening process.

[0005] In order to achieve the above purpose, the utility model provides the following technical solutions:

[0006] A thin-wall aviation aluminum alloy tube hole opening device, comprising a hole opening platform, a mounting cavity is formed inside the hole opening platform, a first servo motor is fixedly connected to the middle of the bottom surface of the mounting cavity, a rotating rod is fixedly connected to the output end of the first servo motor, the rotating rod passes through the mounting cavity to the outside of the hole opening platform and is fixedly connected to a rotating disk, a storage groove is formed at the edge of the upper surface of the rotating disk, and an aluminum alloy tube is placed inside the storage groove;

[0007] A limiting disk is fixedly connected to the edge of the upper surface of the rotating disk near the middle, a storage cavity is opened inside the rotating disk, a rotating column is rotatably connected to the middle of the bottom surface of the storage cavity, a second servo motor is fixedly connected to one side of the bottom surface of the storage cavity, a connecting rod is fixedly connected to the output end of the second servo motor, and a connecting seat is fixedly connected to one side of the upper surface of the opening table.

[0008] Through the above technical scheme, compared with the existing thin-wall aviation aluminum alloy tube hole opening device, when the thin-wall aviation aluminum alloy tube hole opening device is used, the third servo motor is started to drive the threaded rod to rotate and at the same time drive the threaded sleeve to move. The movement of the threaded sleeve drives the slider to slide in the slide groove, thereby limiting the threaded sleeve to move up and down, so that the hole opening position can be adjusted as required, and the hole opening head is driven to move by starting the electric telescopic rod and the fourth servo motor to open the hole, and the practical performance is high.

[0009] Furthermore, the upper ends of the connecting rod and the rotating column penetrate the storage cavity and are rotatably connected to the inner top surface of the limiting plate, the upper ends of the connecting rod and the outer wall of the rotating column are respectively fixedly connected to the driving gear and the driven gear, the surface of the driven gear is provided with a plurality of limiting grooves, the interiors of the limiting grooves are slidably connected to the sliding columns, and the interiors of the limiting plate are slidably connected to a plurality of sliding rods;

[0010] Through the above technical solution, the sliding column moves to drive the sliding rod to extend and retract on the limit plate, which is convenient for limiting the aluminum alloy tubes with different inner diameters.

[0011] Furthermore, the upper ends of the sliding columns are fixedly connected to the lower ends of the sliding rods, the outer walls of the sliding rods on one side away from the center of the driven gears are fixedly connected to sponge pads, and the driving gears and the driven gears are meshed with each other;

[0012] Through the above technical solution, the sponge pad is used to increase the friction force of the aluminum alloy tube in the process of limiting the position of the aluminum alloy tube while preventing damage to the inner wall of the aluminum alloy tube.

[0013] Furthermore, an annular groove is provided at the edge of the upper surface of the perforated platform near the middle, and support columns are fixedly connected to both sides of the upper surface of the rotating disk, and the support columns are slidably connected inside the annular groove;

[0014] Through the above technical solution, the support column is slidably connected inside the annular groove, which facilitates improving the stability of the rotation of the rotating disk.

[0015] Furthermore, a lifting cavity is provided inside the connecting seat, a third servo motor is fixedly connected to the bottom surface of the lifting cavity, a threaded rod is fixedly connected to the output end of the third servo motor, a threaded sleeve is sleeved on the lower end of the threaded rod, a slider is fixedly connected to one side of the outer wall of the threaded sleeve, a sliding groove is provided in the middle of the outer wall of one side of the connecting seat, and the slider is slidably connected inside the sliding groove;

[0016] Through the above technical solution, the slider is slidably connected inside the slide groove, which makes it easy to limit the threaded sleeve, so as to cooperate with the threaded rod to move up and down.

[0017] Furthermore, an electric telescopic rod is fixedly connected to the middle of the outer wall of one side of the slider, an output end of the electric telescopic rod is fixedly connected to a fourth servo motor, and an output end of the fourth servo motor is fixedly connected to a perforated head;

[0018] Through the above technical solution, the hole opening head can be driven to move by starting the fourth servo motor and the electric telescopic rod.

[0019] Furthermore, a cylinder is fixedly connected to the upper end of the outer wall of one side of the perforating platform, and a support pad is fixedly connected to the output end of the cylinder;

[0020] Through the above technical solution, the outer wall of one side of the aluminum alloy tube is supported by the support pad to prevent shaking during the hole opening process.

[0021] Furthermore, a PLC control panel is provided on an outer wall of the hole-opening platform away from the connecting seat;

[0022] Through the above technical solution, the first servo motor, the second servo motor, the third servo motor, the fourth servo motor, the electric telescopic rod and the cylinder are electrically connected through the PLC control panel to control their switching.

[0023] The utility model has the following beneficial effects:

[0024] 1. The utility model proposes a thin-wall aviation aluminum alloy tube hole-opening device. Compared with the existing thin-wall aviation aluminum alloy tube hole-opening device, when the thin-wall aviation aluminum alloy tube hole-opening device is used, the aluminum alloy tube is placed in a storage groove, and the second servo motor is started to drive the connecting rod to rotate while driving the driving gear to rotate, and the driving gear is meshed with the driven gear to drive the driven gear to rotate together, and the driven gear is driven to rotate to drive multiple sliding columns to slide in the limit groove, so that the sliding rod can be extended and retracted in the limit plate, which can flexibly adapt to aluminum alloy tubes with different inner diameters. This means that the same hole-opening device can be used to process aluminum alloy tubes of various sizes, thereby improving the application range and flexibility of the device. The cylinder is started to drive the support pad to move, so as to support one side of the aluminum alloy tube to prevent shaking during the hole-opening process.

[0025] 2. The utility model proposes a thin-wall aviation aluminum alloy tube hole-opening device. Compared with the existing thin-wall aviation aluminum alloy tube hole-opening device, when the thin-wall aviation aluminum alloy tube hole-opening device is used, the third servo motor is started to drive the threaded rod to rotate and the threaded sleeve to move at the same time. The movement of the threaded sleeve drives the slider to slide in the slide groove, thereby limiting the threaded sleeve to move up and down, so that the hole-opening position can be adjusted as required. By starting the electric telescopic rod and the fourth servo motor, the hole-opening head is driven to move to open the hole, and the practical performance is high. BRIEF DESCRIPTION OF THE DRAWINGS

[0026] Figure 1 This is an axonometric view of a thin-wall aviation aluminum alloy tube hole opening device proposed by the utility model;

[0027] Figure 2 This is an axial section view of a thin-wall aviation aluminum alloy tube hole opening device proposed by the utility model;

[0028] Figure 3 This is an axonometric schematic diagram of a driving gear in a thin-wall aviation aluminum alloy tube hole-opening device proposed by the utility model;

[0029] Figure 4 This is an axonometric schematic diagram of a thin-wall aviation aluminum alloy tube hole opening device proposed by the utility model;

[0030] Figure 5 for Figure 2 Enlarged view of point A in the middle.

[0031] 1. Drilling table; 2. Installation cavity; 3. First servo motor; 4. Rotating rod; 5. Rotating disk; 6. Storage slot; 7. Aluminum alloy tube; 8. Storage cavity; 9. Rotating column; 10. Second servo motor; 11. Connecting rod; 12. Driving gear; 13. Driven gear; 14. Limiting disk; 15. Limiting slot; 16. Sliding column; 17. Sliding rod; 18. Sponge pad; 19. Connecting seat; 20. Lifting cavity; 21. Third servo motor; 22. Threaded rod; 23. Threaded sleeve; 24. Sliding block; 25. Electric telescopic rod; 26. Fourth servo motor; 27. Drilling head; 28. Slide slot; 29. ​​Cylinder; 30. Support pad; 31. PLC control panel; 32. Annular groove; 33. Support column. DETAILED DESCRIPTION

[0032] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0033] Reference Figure 1-5 The utility model provides an embodiment: a thin-wall aviation aluminum alloy tube hole opening device, comprising a hole opening platform 1, a mounting cavity 2 is opened inside the hole opening platform 1, a first servo motor 3 is fixedly connected to the middle of the bottom surface of the mounting cavity 2, a rotating rod 4 is fixedly connected to the output end of the first servo motor 3, the rotating rod 4 passes through the mounting cavity 2 to the outside of the hole opening platform 1 and is fixedly connected to a rotating disk 5, a storage groove 6 is opened at the edge of the upper surface of the rotating disk 5, and an aluminum alloy tube 7 is placed inside the storage groove 6;

[0034] A limiting disk 14 is fixedly connected to the edge of the upper surface of the rotating disk 5 near the middle, a storage cavity 8 is opened inside the rotating disk 5, a rotating column 9 is rotatably connected to the middle of the bottom surface of the storage cavity 8, a second servo motor 10 is fixedly connected to one side of the bottom surface of the storage cavity 8, a connecting rod 11 is fixedly connected to the output end of the second servo motor 10, and a connecting seat 19 is fixedly connected to one side of the upper surface of the hole-opening platform 1.

[0035] Compared with the existing thin-wall aviation aluminum alloy tube hole opening device, when the thin-wall aviation aluminum alloy tube hole opening device is used, the third servo motor 21 is started to drive the threaded rod 22 to rotate and at the same time drive the threaded sleeve 23 to move. The movement of the threaded sleeve 23 drives the slider 24 to slide in the slide groove 28, thereby limiting the threaded sleeve 23 to make it move up and down, so that the hole opening position can be adjusted as required, and the electric telescopic rod 25 and the fourth servo motor 26 are started to facilitate the movement of the hole opening head 27 to open the hole, and the practical performance is relatively high.

[0036] The upper ends of the connecting rod 11 and the rotating column 9 both penetrate the storage cavity 8 and are rotatably connected to the inner top surface of the limiting disk 14. The upper ends of the connecting rod 11 and the outer walls of the rotating column 9 are respectively fixedly connected to the driving gear 12 and the driven gear 13. The surface of the driven gear 13 is provided with a plurality of limiting grooves 15. The interior of the limiting grooves 15 is slidably connected with sliding columns 16. The interior of the limiting disk 14 is slidably connected with a plurality of sliding rods 17. The movement of the sliding columns 16 drives the sliding rods 17 to extend and retract on the limiting disk 14, which is convenient for limiting the aluminum alloy tubes 7 with different inner diameters. The upper ends of the sliding columns 16 are fixedly connected to the lower ends of the sliding rods 17, and the sliding rods 17 are away from the driven gear 13. The outer wall on one side of the center is fixedly connected with a sponge pad 18, and the driving gear 12 and the driven gear 13 are meshed with each other. The sponge pad 18 is convenient for increasing the friction force of the aluminum alloy tube 7 in the process of limiting the position, while preventing damage to the inner wall of the aluminum alloy tube 7. An annular groove 32 is provided at the edge near the middle of the upper surface of the hole-opening platform 1, and support columns 33 are fixedly connected on both sides of the upper surface of the rotating disk 5. The support columns 33 are slidably connected inside the annular groove 32. The support columns 33 are slidably connected inside the annular groove 32 to improve the rotation stability of the rotating disk 5. A lifting cavity 20 is provided inside the connecting seat 19, and the bottom surface of the lifting cavity 20 is fixedly connected with the first Three servo motors 21, the output end of the third servo motor 21 is fixedly connected to a threaded rod 22, the lower end of the threaded rod 22 is sleeved with a threaded sleeve 23, one side of the outer wall of the threaded sleeve 23 is fixedly connected to a slider 24, a middle part of the outer wall of one side of the connecting seat 19 is provided with a slide groove 28, the slider 24 is slidably connected inside the slide groove 28, and the slider 24 is slidably connected inside the slide groove 28, so as to facilitate the threaded sleeve 23 to be limited, so as to cooperate with the threaded rod 22 to move up and down, the middle part of the outer wall of one side of the slider 24 is fixedly connected to an electric telescopic rod 25, and the output end of the electric telescopic rod 25 is fixedly connected to a fourth servo motor 26, and the output end of the fourth servo motor 26 is fixedly connected A hole punching head 27 is connected, and the hole punching head 27 can be driven to move by starting the fourth servo motor 26 and the electric telescopic rod 25. A cylinder 29 is fixedly connected to the upper end of the outer wall on one side of the hole punching platform 1, and a support pad 30 is fixedly connected to the output end of the cylinder 29. The support pad 30 is used to support the outer wall of one side of the aluminum alloy tube 7 to prevent shaking during the hole punching process. A plc control panel 31 is provided on the outer wall of the hole punching platform 1 on the side away from the connecting seat 19, and the plc control panel 31 is electrically connected to the first servo motor 3, the second servo motor 10, the third servo motor 21, the fourth servo motor 26, the electric telescopic rod 25 and the cylinder 29 to control their switches.

[0037] Working principle: When in use, the aluminum alloy tube 7 is placed in the storage slot 6, and the second servo motor 10 is started to drive the connecting rod 11 to rotate and the driving gear 12 to rotate at the same time. The driving gear 12 is meshed with the driven gear 13, thereby driving the driven gear 13 to rotate together. The driven gear 13 rotates to drive multiple sliding columns 16 to slide in the limit groove 15, so that the sliding rod 17 can be extended and retracted in the limit plate 14, which can flexibly adapt to aluminum alloy tubes 7 of different inner diameters. This means that the same hole opening device can be used to process aluminum alloy tubes 7 of various sizes, providing The application scope and flexibility of the device are improved. By starting the cylinder 29 to drive the support pad 30 to move, one side of the aluminum alloy tube 7 is supported to prevent shaking during the hole opening process. By starting the third servo motor 21 to drive the threaded rod 22 to rotate, the threaded sleeve 23 is driven to move. Due to the movement of the threaded sleeve 23, the slider 24 is driven to slide in the slide groove 28, so that the threaded sleeve 23 is limited to move up and down, so that the hole opening position can be adjusted as needed. By starting the electric telescopic rod 25 and the fourth servo motor 26, the hole opening head 27 is driven to move to open the hole.

[0038] Finally, it should be noted that the above is only a preferred embodiment of the present invention and is not intended to limit the present invention. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art can still modify the technical solutions described in the aforementioned embodiments or make equivalent substitutions for some of the technical features therein. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. A thin-wall aviation aluminum alloy tube hole-punching device, comprising a hole-punching station (1), characterized in that: The hole-opening platform (1) has an installation cavity (2) formed inside, a first servo motor (3) is fixedly connected to the middle of the bottom surface of the installation cavity (2), an output end of the first servo motor (3) is fixedly connected to a rotating rod (4), the rotating rod (4) passes through the installation cavity (2) to the outside of the hole-opening platform (1) and is fixedly connected to a rotating disk (5), a storage groove (6) is formed at the edge of the upper surface of the rotating disk (5), and an aluminum alloy tube (7) is placed inside the storage groove (6); A limit plate (14) is fixedly connected to the edge of the upper surface of the rotating disk (5) near the middle, a storage cavity (8) is provided inside the rotating disk (5), a rotating column (9) is rotatably connected to the middle of the bottom surface of the storage cavity (8), a second servo motor (10) is fixedly connected to one side of the bottom surface of the storage cavity (8), a connecting rod (11) is fixedly connected to the output end of the second servo motor (10), and a connecting seat (19) is fixedly connected to one side of the upper surface of the hole-opening platform (1); The upper ends of the connecting rod (11) and the rotating column (9) both penetrate the storage cavity (8) and are rotatably connected to the inner top surface of the limiting plate (14); the upper ends of the outer walls of the connecting rod (11) and the rotating column (9) are respectively fixedly connected to a driving gear (12) and a driven gear (13); a surface of the driven gear (13) is provided with a plurality of limiting grooves (15); the interiors of the limiting grooves (15) are slidably connected to sliding columns (16); the interiors of the limiting plate (14) are slidably connected to a plurality of sliding rods (17); The upper ends of the sliding columns (16) are fixedly connected to the lower ends of the sliding rods (17); a sponge pad (18) is fixedly connected to the outer wall of the sliding rods (17) at one side away from the center of the driven gear (13); and the driving gear (12) and the driven gear (13) are meshed with each other.

2. A thin-wall aviation aluminum alloy tube hole opening device according to claim 1, characterized in that: An annular groove (32) is provided at an edge near the middle of the upper surface of the hole-opening platform (1), and support columns (33) are fixedly connected to both sides of the upper surface of the rotating disk (5), and the support columns (33) are slidably connected inside the annular groove (32).

3. A thin-wall aviation aluminum alloy tube hole opening device according to claim 1, characterized in that: A lifting cavity (20) is provided inside the connecting seat (19), a third servo motor (21) is fixedly connected to the bottom surface of the lifting cavity (20), a threaded rod (22) is fixedly connected to the output end of the third servo motor (21), a threaded sleeve (23) is sleeved on the lower end of the rod body of the threaded rod (22), a slider (24) is fixedly connected to one side of the outer wall of the threaded sleeve (23), a sliding groove (28) is provided in the middle of the outer wall of one side of the connecting seat (19), and the slider (24) is slidably connected inside the sliding groove (28).

4. A thin-wall aviation aluminum alloy tube hole opening device according to claim 3, characterized in that: An electric telescopic rod (25) is fixedly connected to the middle of an outer wall of one side of the sliding block (24); an output end of the electric telescopic rod (25) is fixedly connected to a fourth servo motor (26); and an output end of the fourth servo motor (26) is fixedly connected to a perforated head (27).

5. A thin-wall aviation aluminum alloy tube hole opening device according to claim 1, characterized in that: The upper end of the outer wall of one side of the perforating platform (1) is fixedly connected to a cylinder (29), and the output end of the cylinder (29) is fixedly connected to a support pad (30).

6. A thin-wall aviation aluminum alloy tube hole opening device according to claim 1, characterized in that: A PLC control panel (31) is provided on an outer wall of the hole-opening platform (1) at a side away from the connecting seat (19).