CN220497816U - Simple aviation aluminum alloy part punching device - Google Patents
Simple aviation aluminum alloy part punching device Download PDFInfo
- Publication number
- CN220497816U CN220497816U CN202322148022.XU CN202322148022U CN220497816U CN 220497816 U CN220497816 U CN 220497816U CN 202322148022 U CN202322148022 U CN 202322148022U CN 220497816 U CN220497816 U CN 220497816U
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- China
- Prior art keywords
- motor
- aluminum alloy
- drill bit
- fixedly connected
- telescopic rod
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 43
- 238000004080 punching Methods 0.000 title claims abstract description 29
- 230000033001 locomotion Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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- Processing Of Stones Or Stones Resemblance Materials (AREA)
Abstract
The utility model relates to the technical field of punching devices and discloses a simple aviation aluminum alloy part punching device which comprises a base, a workbench and a drill bit, wherein one end of the base is provided with a support column, the top of the support column is provided with a first air cylinder, the output end of the first air cylinder is provided with a first telescopic rod, one end of the first telescopic rod is provided with a fixed plate, one end of the fixed plate is provided with a first motor, the output end of the first motor is provided with a threaded rod, one end of the threaded rod is in threaded connection with a moving block, the bottom of the moving block is provided with a second air cylinder, the drill bit is arranged below the second air cylinder, the top of the base is provided with the workbench, the four corners of the base is provided with a second motor, one end of the second motor is provided with a pressing block, and the drill bit can perform punching operation at any position of an aluminum alloy through the arrangement of the first air cylinder and the first motor.
Description
Technical Field
The utility model relates to the technical field of punching devices, in particular to a simple aviation aluminum alloy part punching device.
Background
Because aluminum alloy has very high room temperature intensity, good corrosion resistance and high toughness, so the aluminum alloy is widely applied to the aviation field, the aluminum alloy needs to be processed before being applied to the aviation field, wherein the punching operation is necessary for the aluminum alloy, the standard head of the existing punching device is basically fixed at one position, the punching position can not be freely adjusted, and people are required to adjust the position of the aluminum alloy, so that the punching position is not accurate enough, and the working efficiency is low.
The utility model discloses an aluminium alloy plate processing perforating device like chinese patent publication No. CN113894322a, the publication day of authority is 2022, 1 month 7, mainly relates to panel processing perforating equipment field, an aluminium alloy plate processing perforating device, including the workstation, be equipped with transmission on the workstation, workstation top surface one side rotates the installation telescopic link through the bearing frame that has locking device, telescopic link periphery suit first adapter sleeve, the diaphragm is installed on the telescopic link top, the driving motor is all installed to diaphragm bottom surface both sides, but in actual use, the above-mentioned device can carry out porous operation simultaneously to a panel through setting up a plurality of drill bits, but fixed when the drill bit position of its setting, consequently can't carry out the operation of punching to each position of aluminium alloy, and although the device is with aluminium alloy place on the conveyer belt, lets aluminium alloy can remove, has increased the punching position, but the conveyer belt can only carry out the motion of single direction, so still can't let the drill bit just need the position of people to adjust aluminium alloy when punching in arbitrary position of aluminium alloy, so that the work efficiency of punching is not very low yet accurate.
Disclosure of Invention
The utility model aims to provide a simple aviation aluminum alloy part punching device, which solves the problem that the punching position of the existing punching device cannot be adjusted randomly.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a simple and easy aviation aluminum alloy spare perforating device, includes base, workstation and drill bit, base one end is provided with the support column, the support column top is provided with first cylinder, first cylinder output is provided with first telescopic link, first telescopic link one end is provided with the fixed plate, fixed plate one end is provided with first motor, first motor output is provided with the threaded rod, threaded rod one end threaded connection has the movable block, the movable block bottom is provided with the second cylinder, second cylinder below is provided with the drill bit, the base top is provided with the workstation, the base is located four corners departments of workstation and is provided with the second motor, second motor one end is provided with the briquetting.
Preferably, the output end of the second cylinder is fixedly connected with a second telescopic rod, and the drill bit is arranged below the second telescopic rod.
Preferably, the bottom of the second telescopic rod is fixedly connected with a third motor, and the output end of the third motor is fixedly connected with the drill bit.
Preferably, the output end of the second motor is fixedly connected with a third cylinder, the output end of the third cylinder is fixedly connected with a third telescopic rod, the top of the third telescopic rod is fixedly connected with a connecting arm, and one end of the connecting arm is fixedly connected with a pressing block.
Preferably, a sliding groove is formed in the top of the fixed plate, a sliding block is arranged on the top of the moving block, and the sliding groove is in sliding connection with the sliding block.
Preferably, one end of the threaded rod far away from the first motor is rotationally connected with the fixed plate.
Compared with the prior art, the utility model has the beneficial effects that:
according to the utility model, the first telescopic rod is driven to stretch out and draw back through the first air cylinder, so that the drill bit can move in the left-right direction, the first motor drives the threaded rod to rotate, at the moment, the moving block can move back and forth on the threaded rod, so that the drill bit is driven to move in the front-back direction, the drill bit can move freely in the front-back direction, the left-right direction, the drill bit can perform punching operation at any position of aluminum alloy, in addition, the position of the pressing block can be adjusted through the arrangement of the second motor, so that the drill bit can punch holes at the position where the aluminum alloy is pressed by the pressing block, and the drill bit has no dead angle in punching of the aluminum alloy, so that the drill bit is very practical.
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is a schematic view of a partial enlarged structure at A in FIG. 1;
fig. 3 is a schematic view of a partial enlarged structure at B in fig. 1.
In the figure: 1. a base; 2. a work table; 3. a drill bit; 4. a support column; 5. a first cylinder; 6. a first telescopic rod; 7. a fixing plate; 8. a first motor; 9. a threaded rod; 10. a moving block; 11. a second cylinder; 12. a second motor; 13. briquetting; 14. a second telescopic rod; 15. a third motor; 16. a third cylinder; 17. a third telescopic rod; 18. a connecting arm; 19. a chute; 20. a sliding block.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and fully with reference to the accompanying drawings, in which some, but not all embodiments of the utility model are shown.
Referring to fig. 1-3, the present utility model provides a technical solution: a simple aviation aluminum alloy part punching device comprises a base 1, a workbench 2 and a drill bit 3, wherein one end of the base 1 is provided with a support column 4, the top of the support column 4 is provided with a first air cylinder 5, the output end of the first air cylinder 5 is provided with a first telescopic rod 6, one end of the first telescopic rod 6 is provided with a fixed plate 7, one end of the fixed plate 7 is provided with a first motor 8, the output end of the first motor 8 is provided with a threaded rod 9, one end of the threaded rod 9 is in threaded connection with a movable block 10, the bottom of the movable block 10 is provided with a second air cylinder 11, the drill bit 3 is arranged below the second air cylinder 11, the top of the base 1 is provided with the workbench 2, the four corners of the base 1, which are positioned at the workbench 2, are provided with second motors 12, one end of the second motors 12 is provided with a pressing block 13,
in this embodiment, firstly, an aluminum alloy is placed on the workbench 2, then the second motor 12 is started to enable the pressing block 13 to move above the aluminum alloy, then the aluminum alloy is pressed, then the first cylinder 5 is started, at this time, the first telescopic rod 6 starts to stretch, so as to drive the drill bit 3 to move in the left-right direction, then the first motor 8 is started, so as to enable the threaded rod 9 to start rotating, at this time, the moving block 10 in threaded connection with the threaded rod 9 starts to move back and forth on the threaded rod 9, so as to drive the drill bit 3 to move in the front-back direction,
then, the second air cylinder 11 is started to enable the drill bit 3 to move downwards, the drill bit 3 is driven by the third motor 15 to punch the aluminum alloy, the drill bit 3 can move freely in the front-back left-right direction through the design, the drill bit 3 can punch any position of the aluminum alloy, when the position of the aluminum alloy to be punched is just pressed by the pressing block 13, the pressing block 13 can be lifted firstly, then the second motor 12 is started to enable the pressing block 13 to move to other positions, and therefore the drill bit 3 can punch the aluminum alloy, and the drill bit 3 has no dead angle in punching on the aluminum alloy through the design.
As shown in fig. 1, the output end of the second cylinder 11 is fixedly connected with a second telescopic rod 14, and the drill bit 3 is disposed below the second telescopic rod 14, in this embodiment, when the second cylinder 11 is opened, the second telescopic rod 14 stretches, so as to drive the drill bit 3 to move downward, so that the drill bit 3 can successfully punch the aluminum alloy.
As shown in fig. 1, the bottom of the second telescopic rod 14 is fixedly connected with a third motor 15, and the output end of the third motor 15 is fixedly connected with the drill bit 3, in this embodiment, since the drill bit 3 needs a driving force when punching, the drill bit 3 has a driving force when punching through the design of the third motor 15.
As shown in fig. 1-2, the output end of the second motor 12 is fixedly connected with a third air cylinder 16, the output end of the third air cylinder 16 is fixedly connected with a third telescopic rod 17, the top of the third telescopic rod 17 is fixedly connected with a connecting arm 18, one end of the connecting arm 18 is fixedly connected with the pressing block 13, in this embodiment, since a driving force is required for pressing down and lifting the pressing block 13, the pressing down and lifting of the pressing block 13 have a driving force through the design of the third motor 15 and the third telescopic rod 17, and in addition, since the motor is located outside the workbench 2, in order to enable the pressing block 13 to move above the workbench 2, the pressing block 13 can smoothly move above the workbench 2 through the design of the connecting arm 18.
As shown in fig. 1 and 3, the top of the fixed plate 7 is provided with a sliding groove 19, the top of the moving block 10 is provided with a sliding block 20, the sliding groove 19 is slidably connected with the sliding block 20, in this embodiment, since the moving block 10 is moved by the rotation of the threaded rod 9, in order to prevent the moving block 10 from swinging along with the rotation of the threaded rod 9, the sliding block 20 and the sliding groove 19 are provided, so that the movement of the moving block 10 is more stable.
As shown in fig. 1, one end of the threaded rod 9 far away from the first motor 8 is rotationally connected with the fixed plate 7, in this embodiment, in order to prevent the threaded rod 9 from being suspended at one end far away from the first motor 8, which results in tilting of the drill bit 3, one end of the threaded rod 9 far away from the first motor 8 needs to be connected with the fixed plate 7, so that the threaded rod 9 can normally rotate, and thus the threaded rod 9 is rotationally connected with the fixed plate 7.
Working principle: when the aluminum alloy drilling machine is used, firstly, aluminum alloy is placed on the workbench 2, then the second motor 12 is started to enable the pressing block 13 to move to the upper side of the aluminum alloy, then the third air cylinder 16 is started to enable the third telescopic rod 17 to shrink, so that the pressing block 13 can press the aluminum alloy, then the first air cylinder 5 is started, at the moment, the first telescopic rod 6 starts to stretch, so that the drill bit 3 is driven to move in the left-right direction, then the first motor 8 is started to enable the threaded rod 9 to start rotating, at the moment, the moving block 10 in threaded connection with the threaded rod 9 starts to move back and forth on the threaded rod 9, so that the drill bit 3 is driven to move downwards by the second air cylinder 11, and the drill bit 3 is driven to punch the aluminum alloy under the driving of the third motor 15.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes and modifications may be made therein without departing from the principles of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a simple and easy aviation aluminum alloy spare perforating device, includes base (1), workstation (2) and drill bit (3), its characterized in that: base (1) one end is provided with support column (4), support column (4) top is provided with first cylinder (5), first cylinder (5) output is provided with first telescopic link (6), first telescopic link (6) one end is provided with fixed plate (7), fixed plate (7) one end is provided with first motor (8), first motor (8) output is provided with threaded rod (9), threaded rod (9) one end threaded connection has movable block (10), movable block (10) bottom is provided with second cylinder (11), second cylinder (11) below is provided with drill bit (3), base (1) top is provided with workstation (2), base (1) are located four corners departments of workstation (2) and are provided with second motor (12), second motor (12) one end is provided with briquetting (13).
2. The simple aviation aluminum alloy part punching device according to claim 1, wherein: the output end of the second air cylinder (11) is fixedly connected with a second telescopic rod (14), and the drill bit (3) is arranged below the second telescopic rod (14).
3. The simple aviation aluminum alloy part punching device according to claim 2, wherein: the bottom of the second telescopic rod (14) is fixedly connected with a third motor (15), and the output end of the third motor (15) is fixedly connected with the drill bit (3).
4. The simple aviation aluminum alloy part punching device according to claim 1, wherein: the output end of the second motor (12) is fixedly connected with a third air cylinder (16), the output end of the third air cylinder (16) is fixedly connected with a third telescopic rod (17), the top of the third telescopic rod (17) is fixedly connected with a connecting arm (18), and one end of the connecting arm (18) is fixedly connected with the pressing block (13).
5. The simple aviation aluminum alloy part punching device according to claim 1, wherein: the top of the fixed plate (7) is provided with a sliding groove (19), the top of the moving block (10) is provided with a sliding block (20), and the sliding groove (19) is in sliding connection with the sliding block (20).
6. The simple aviation aluminum alloy part punching device according to claim 5, wherein: one end of the threaded rod (9) far away from the first motor (8) is rotationally connected with the fixed plate (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322148022.XU CN220497816U (en) | 2023-08-10 | 2023-08-10 | Simple aviation aluminum alloy part punching device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322148022.XU CN220497816U (en) | 2023-08-10 | 2023-08-10 | Simple aviation aluminum alloy part punching device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220497816U true CN220497816U (en) | 2024-02-20 |
Family
ID=89879123
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322148022.XU Active CN220497816U (en) | 2023-08-10 | 2023-08-10 | Simple aviation aluminum alloy part punching device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220497816U (en) |
-
2023
- 2023-08-10 CN CN202322148022.XU patent/CN220497816U/en active Active
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