CN221134115U - Aviation aluminum alloy vibration drilling machining center - Google Patents
Aviation aluminum alloy vibration drilling machining center Download PDFInfo
- Publication number
- CN221134115U CN221134115U CN202322716831.6U CN202322716831U CN221134115U CN 221134115 U CN221134115 U CN 221134115U CN 202322716831 U CN202322716831 U CN 202322716831U CN 221134115 U CN221134115 U CN 221134115U
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- CN
- China
- Prior art keywords
- aluminum alloy
- machining center
- drilling machining
- workbench
- fixedly arranged
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 48
- 238000005553 drilling Methods 0.000 title claims abstract description 39
- 229910045601 alloy Inorganic materials 0.000 claims description 7
- 239000000956 alloy Substances 0.000 claims description 7
- 229910001095 light aluminium alloy Inorganic materials 0.000 claims description 7
- 230000007246 mechanism Effects 0.000 claims description 6
- 238000009434 installation Methods 0.000 claims 2
- 230000000694 effects Effects 0.000 abstract description 6
- 238000003754 machining Methods 0.000 abstract description 6
- 230000009471 action Effects 0.000 description 5
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000006227 byproduct Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/10—Greenhouse gas [GHG] capture, material saving, heat recovery or other energy efficient measures, e.g. motor control, characterised by manufacturing processes, e.g. for rolling metal or metal working
Landscapes
- Drilling And Boring (AREA)
Abstract
The utility model relates to the technical field of electric tools and discloses an aviation aluminum alloy vibration drilling machining center which comprises a workbench, wherein through grooves are formed in the inner bottom of the workbench, a sliding plate is arranged on the inner wall of the workbench in a sliding mode, a plurality of second rotating seats are fixedly arranged on the upper surface of the sliding plate, the inner walls of the second rotating seats are rotatably connected with L-shaped plates, connecting blocks are fixedly arranged on the positions, close to two sides, of the workbench, a support frame is fixedly connected with the connecting blocks together, support plates are fixedly arranged on two sides of the support frame, and two hydraulic cylinders are fixedly arranged on the upper surfaces of the support plates on two sides of the support frame. According to the utility model, the vibration drilling machining center for the aviation aluminum alloy has the effect of quick and automatic feeding, and meanwhile, the vibration drilling machining center for the aviation aluminum alloy also has the effect of clamping and fixing the aluminum alloy, so that the aluminum alloy is more stable in machining, and the cutting accuracy of the aluminum alloy is greatly improved.
Description
Technical Field
The utility model relates to the technical field of drilling processing, in particular to an aviation aluminum alloy vibration drilling processing center.
Background
Aviation aluminum alloy is a byproduct of the development of the aviation industry in China. As the name suggests, the aviation aluminum alloy is applied to aviation industry at the earliest, and the texture of the aviation aluminum alloy is far from that of the common aluminum alloy, and the aviation aluminum alloy has the characteristics of high strength, high pressure resistance, oxidation resistance and the like.
At present, most aviation aluminum alloy vibration drilling machining centers need to be manually assisted in feeding when being machined, so that the machining efficiency of aluminum alloy is greatly reduced, and the development of later enterprises is not facilitated. Accordingly, a person skilled in the art provides an aviation aluminum alloy vibration drilling machining center to solve the problems set forth in the background art.
Disclosure of utility model
The utility model aims to solve the defects in the prior art, and provides an aviation aluminum alloy vibration drilling machining center which has the effect of quick and automatic feeding, and simultaneously has the effect of clamping and fixing aluminum alloy, so that the aluminum alloy is more stable in machining, and the cutting accuracy of the aluminum alloy is greatly improved.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
The aviation aluminum alloy vibration drilling machining center comprises a workbench, wherein a through groove is formed in the inner bottom of the workbench, a sliding plate is arranged on the inner wall of the workbench in a sliding mode, a plurality of second rotating seats are fixedly arranged on the upper surface of the sliding plate, and the inner walls of the second rotating seats are rotatably connected with L-shaped plates;
The workbench is close to both sides department and all fixedly is provided with the connecting block, and is a plurality of the joint block is fixedly connected with support frame jointly, the support frame both sides are all fixedly provided with the backup pad, both sides the backup pad upper surface is all fixedly provided with two hydraulic cylinder, and is a plurality of adjacent pairwise one set of hydraulic cylinder, every group hydraulic cylinder one end is fixedly connected with push pedal.
Through above-mentioned technical scheme, mutually supporting through the second rotates between seat and the L template, is convenient for promote aviation aluminum alloy and removes forward, mutually supporting through between hydraulic cylinder and the push pedal, under the both sides electromagnet magnetic force effect, can make the push pedal centre gripping more fastening.
Further, a fixed plate is fixedly arranged on the lower end surface of the workbench, a motor is fixedly arranged on one side wall of the fixed plate, and the output end of the motor is fixedly connected with a rotating rod;
Through above-mentioned technical scheme, rotate the dwang through motor drive.
Further, the lower end surface of the sliding plate is fixedly connected with a first rotating seat, a side wall of the first rotating seat is rotationally connected with a connecting rod, and the connecting rod is rotationally connected with the rotating rod;
Through above-mentioned technical scheme, utilize mutually supporting between first rotating seat, connecting rod and the dwang, can make the sliding plate slide on the workstation.
Further, the upper end face of the supporting frame is fixedly provided with a mounting frame and a limiting frame, the upper end face of the mounting frame is fixedly provided with an electric telescopic rod, and the output end of the electric telescopic rod is fixedly connected with a drilling mechanism;
Through above-mentioned technical scheme, mutually support between electric telescopic handle and the drilling mechanism, be convenient for process aluminum alloy.
Further, electromagnets are fixedly embedded in the opposite sides of the two pushing plates;
Through the technical scheme, mutual suction between the pushing plates at two sides is facilitated.
Further, connecting frames are fixedly arranged on the other side walls of the two pushing plates, and rollers are rotatably connected to the inner walls of the two connecting frames;
through above-mentioned technical scheme, be convenient for support the push pedal.
Further, springs are fixedly connected between the L-shaped plates and the sliding plates;
Through above-mentioned technical scheme, be convenient for reset the pivoted L template.
Further, the first rotating seat slides on the inner wall of the through groove;
through the technical scheme, the sliding plate can be driven to move through the first rotating seat.
The utility model has the following beneficial effects:
1. Compared with the existing aviation aluminum alloy vibration drilling machining center, the aviation aluminum alloy vibration drilling machining center provided by the utility model has the advantages that when the aviation aluminum alloy vibration drilling machining center is used, under the driving action of a motor, the sliding plate slides on the workbench through the mutual matching among the rotating rod, the connecting rod and the rotating seat, the aluminum alloy on the support frame can be pushed forward through the matching among the second rotating seat, the L-shaped plate and the spring, and the aluminum alloy can be automatically fed and transmitted under the matching action of the limiting frame, so that the machining efficiency of the aluminum alloy is greatly improved.
2. Compared with the existing aviation aluminum alloy vibration drilling machining center, the aviation aluminum alloy vibration drilling machining center provided by the utility model has the advantages that when in use, the aviation aluminum alloy vibration drilling machining center can clamp and fix the aluminum alloy plate under the magnetic force action of the electromagnets at the two sides through the pushing of the pushing plates of the hydraulic cylinders at the two sides, so that the aviation aluminum alloy is prevented from shaking easily during drilling, and the accuracy of aluminum alloy machining is higher.
Drawings
FIG. 1 is a front view of an aviation aluminum alloy vibration drilling machining center provided by the utility model;
FIG. 2 is a top cross-sectional view of an aircraft aluminum alloy vibratory drilling machining center according to the present utility model;
FIG. 3 is a schematic view of a part of an aviation aluminum alloy vibration drilling machining center;
FIG. 4 is an enlarged view of FIG. 1 at A;
fig. 5 is an enlarged view at B in fig. 2.
Legend description:
1. A work table; 2. a sliding plate; 3. a through groove; 4. an electric telescopic rod; 5. a drilling mechanism; 6. a mounting frame; 7. a support frame; 8. a connecting block; 9. a connecting rod; 10. a first rotating seat; 11. a rotating lever; 12. a fixing plate; 13. a motor; 14. an electromagnet; 15. a limit frame; 16. a support plate; 17. a hydraulic cylinder; 18. a second rotating seat; 19. an L-shaped plate; 20. a spring; 21. a connecting frame; 22. a roller; 23. a push plate.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-5, one embodiment provided by the present utility model is: the utility model provides an aviation aluminum alloy vibration drilling machining center, includes workstation 1, and logical groove 3 has been seted up to workstation 1 inner bottom, and workstation 1 inner wall slides and is provided with slide plate 2, and slide plate 2 upper surface is fixed to be provided with a plurality of second and rotates seat 18, and a plurality of second rotate seat 18 inner walls rotate and are connected with L template 19, through the cooperation between second rotate seat 18 and the L template 19, is convenient for promote aviation aluminum alloy and moves forward;
The workstation 1 is close to both sides department and all fixedly provided with connecting block 8, the common fixedly connected with support frame 7 of a plurality of connecting blocks 8, the support frame 7 both sides are all fixedly provided with backup pad 16, the equal fixedly provided with of both sides backup pad 16 upper surface two hydraulic cylinder 17, a plurality of hydraulic cylinder 17 are adjacent two by two a set of, every group hydraulic cylinder 17 one end all fixedly connected with push pedal 23, mutually support through between hydraulic cylinder 17 and the push pedal 23, under the magnetic force effect of both sides electromagnet 14, can make the push pedal 23 centre gripping more fastening.
The fixed plate 12 that is provided with of terminal surface under the workstation 1, fixed plate 12 side wall fixedly is provided with motor 13, the output fixedly connected with dwang 11 of motor 13 drives dwang 11 through motor 13 and rotates, the first rotating seat 10 of terminal surface fixedly connected with under the slide plate 2, a side wall rotation of first rotating seat 10 is connected with connecting rod 9, rotate between connecting rod 9 and the dwang 11 and be connected with, utilize first rotating seat 10, mutually support between connecting rod 9 and the dwang 11, can make slide plate 2 slide on workstation 1, support frame 7 up end fixedly is provided with mounting bracket 6 and spacing frame 15, mounting bracket 6 up end fixedly is provided with electric telescopic handle 4, electric telescopic handle 4's output fixedly connected with drilling mechanism 5, mutually support between electric telescopic handle 4 and the drilling mechanism 5, be convenient for process the aluminum alloy, two push pedal 23 relative one side are all fixedly embedded and are equipped with electromagnet 14, be convenient for make mutual suction between two push pedal 23 another lateral wall all fixedly provided with link 21, two link 21 inner wall all rotate and are connected with gyro wheel 22, be convenient for support push pedal 23 and a plurality of slide plate 2L and a plurality of slide plate 2 are connected with through the spring that slide plate 20, slide plate 2 is convenient for carry out the slide plate 2, slide plate 2 is moved in order to make slide plate 2 through the fixed connection between the slide plate 3, slide plate 2 is convenient for slide plate 2, slide plate 2 is moved through the first rotating plate 20.
Working principle: when the aluminum alloy drilling machine is used, firstly, aviation aluminum alloy is placed in a limiting frame 15, a rotating rod 11 is driven by a motor 13, a sliding plate 2 periodically reciprocates under the action of a connecting rod 9 and a first rotating seat 10, the aluminum alloy can be moved forwards by utilizing the cooperation among a second rotating seat 18, an L-shaped plate 19 and a spring 20, and the aluminum alloy can be firmly fixed under the action of magnetic force of an electromagnet 14 by the cooperation among a hydraulic cylinder 17 and a push plate 23, so that the aluminum alloy drilling machine is more stable.
Finally, it should be noted that: the foregoing description of the preferred embodiments of the present utility model is not intended to be limiting, but rather, although the present utility model has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described, or equivalents may be substituted for elements thereof, and any modifications, equivalents, improvements or changes may be made without departing from the spirit and principles of the present utility model.
Claims (8)
1. Aviation aluminum alloy vibration drilling machining center, including workstation (1), its characterized in that: a through groove (3) is formed in the inner bottom of the workbench (1), a sliding plate (2) is arranged on the inner wall of the workbench (1) in a sliding mode, a plurality of second rotating seats (18) are fixedly arranged on the upper surface of the sliding plate (2), and L-shaped plates (19) are rotatably connected to the inner walls of the second rotating seats (18);
The workbench (1) is close to both sides department and all fixedly provided with connecting block (8), a plurality of connecting block (8) joint fixedly connected with support frame (7), support frame (7) both sides are all fixedly provided with backup pad (16), both sides backup pad (16) upper surface is all fixedly provided with two hydraulic cylinder (17), and is a plurality of adjacent two liang of hydraulic cylinder (17), every group hydraulic cylinder (17) one end is equal fixedly connected with push pedal (23).
2. The aircraft aluminum alloy vibratory drilling machining center of claim 1, wherein: the automatic rotary table is characterized in that a fixed plate (12) is fixedly arranged on the lower end face of the workbench (1), a motor (13) is fixedly arranged on one side wall of the fixed plate (12), and a rotary rod (11) is fixedly connected to the output end of the motor (13).
3. The aircraft aluminum alloy vibratory drilling machining center of claim 1, wherein: the sliding plate is characterized in that a first rotating seat (10) is fixedly connected to the lower end face of the sliding plate (2), a connecting rod (9) is rotatably connected to one side wall of the first rotating seat (10), and the connecting rod (9) is rotatably connected with a rotating rod (11).
4. The aircraft aluminum alloy vibratory drilling machining center of claim 1, wherein: the automatic drilling device is characterized in that an installation frame (6) and a limiting frame (15) are fixedly arranged on the upper end face of the support frame (7), an electric telescopic rod (4) is fixedly arranged on the upper end face of the installation frame (6), and a drilling mechanism (5) is fixedly connected to the output end of the electric telescopic rod (4).
5. The aircraft aluminum alloy vibratory drilling machining center of claim 1, wherein: electromagnets (14) are fixedly embedded on the opposite sides of the two pushing plates (23).
6. The aircraft aluminum alloy vibratory drilling machining center of claim 1, wherein: the other side walls of the two pushing plates (23) are fixedly provided with connecting frames (21), and the inner walls of the two connecting frames (21) are rotatably connected with rollers (22).
7. The aircraft aluminum alloy vibratory drilling machining center of claim 1, wherein: springs (20) are fixedly connected between the L-shaped plates (19) and the sliding plates (2).
8. An aeronautical aluminum alloy vibratory drilling machining center according to claim 3, wherein: the first rotating seat (10) slides on the inner wall of the through groove (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322716831.6U CN221134115U (en) | 2023-10-10 | 2023-10-10 | Aviation aluminum alloy vibration drilling machining center |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322716831.6U CN221134115U (en) | 2023-10-10 | 2023-10-10 | Aviation aluminum alloy vibration drilling machining center |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221134115U true CN221134115U (en) | 2024-06-14 |
Family
ID=91429705
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322716831.6U Active CN221134115U (en) | 2023-10-10 | 2023-10-10 | Aviation aluminum alloy vibration drilling machining center |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221134115U (en) |
-
2023
- 2023-10-10 CN CN202322716831.6U patent/CN221134115U/en active Active
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