CN217749638U - High-reliability multi-wire cutting device for aviation die - Google Patents
High-reliability multi-wire cutting device for aviation die Download PDFInfo
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- CN217749638U CN217749638U CN202221534690.5U CN202221534690U CN217749638U CN 217749638 U CN217749638 U CN 217749638U CN 202221534690 U CN202221534690 U CN 202221534690U CN 217749638 U CN217749638 U CN 217749638U
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Abstract
The utility model discloses a multi-thread cutting device of high reliability aeromould, including the installation base, installation base top surface is provided with the workstation, the workstation top surface is connected with two-way winding mechanism and guiding mechanism through first adjustment mechanism and second adjustment mechanism respectively, just first adjustment mechanism and second adjustment mechanism symmetry respectively set up in the workstation top surface, first adjustment mechanism is connected through drive mechanism with the second adjustment mechanism input, is located leftwards first adjustment mechanism input is provided with actuating mechanism, just actuating mechanism sets up in installation base front surface left side, adopts driving motor as driven maincenter to and through the drive of each sprocket and chain to adjust through the mode unification of screw thread for the accuracy of regulation is more accurate, and the while operation is convenient, the effectual problem of avoiding adjusting cycle length.
Description
Technical Field
The utility model relates to a high reliability aeronautical mold multi-wire cutting device belongs to multi-wire cutting technical field.
Background
The multi-wire cutting is a novel cutting machining method for simultaneously cutting raw materials into a plurality of workpieces through high-speed reciprocating motion of metal wires, can effectively improve the production and machining efficiency, saves the raw materials, and has an application number: 202020942209.0 mentions, when using, the cutting line is around the guide roll on the guide assembly and is on two-way rolling axle, every guide assembly can be alone along spout back-and-forth movement, drive the cutting line back-and-forth movement regulation, adjust distance and direction between the different cutting lines, and then realize the regulation to the work piece size and the shape that need cut out, can cut the work piece of different thickness size and shape of department simultaneously, and the machining efficiency is improved, but the part of regulation need pass through artifical manual regulation, cause the accurate value of regulation to reduce, and the problem of the time length of regulation.
SUMMERY OF THE UTILITY MODEL
The utility model discloses the technical problem who solves overcomes current defect, provides a high reliability aeronautical mold multi-wire cutting device, can effectively solve the problem in the background art.
In order to achieve the above object, the utility model provides a following technical scheme: including the installation base, installation base top surface is provided with the workstation, the workstation top surface is connected with two-way winding mechanism and guiding mechanism through first adjustment mechanism and second adjustment mechanism respectively, just first adjustment mechanism and second adjustment mechanism symmetry respectively set up in the workstation top surface, first adjustment mechanism is connected through drive mechanism with the second adjustment mechanism input, is located the left first adjustment mechanism input is provided with actuating mechanism, just actuating mechanism sets up in installation base front surface left side.
Furthermore, a processing table is arranged between every two adjacent second adjusting mechanisms and arranged in the middle of the top surface of the workbench.
Furthermore, first adjustment mechanism includes first adjustment tank, a first accommodate the lead screw and a regulating block, the workstation top surface is located to first adjustment tank symmetry digging, first adjustment tank inner chamber rear surface is connected with a first accommodate the lead screw through the bearing, a first accommodate the lead screw outer wall has a first regulating block through threaded connection to be the symmetry setting.
Furthermore, the second adjusting mechanism comprises a second adjusting groove, a second adjusting screw rod and a second adjusting block, the second adjusting groove is symmetrically dug on two sides of the top surface of the workbench, the rear surface of the inner cavity of the second adjusting groove is connected with the second adjusting screw rod through a bearing, and the outer wall of the second adjusting screw rod is connected with the second adjusting block through threads and symmetrically arranged.
Further, drive mechanism is including driving the sprocket and driving the chain, first accommodate the lead screw all extends to the workstation front surface with second accommodate the lead screw input, drive the sprocket and overlap respectively and locate first accommodate the lead screw and the input of second accommodate the lead screw, adjacent drive and be connected through driving the chain between the sprocket.
Further, actuating mechanism includes driving motor, drive shaft, driving sprocket and drive chain, driving motor passes through the mounting panel and sets up in installation base front surface left side, the driving motor output is provided with the drive shaft, drive shaft outer wall cover is equipped with driving sprocket, just driving sprocket is located the left equally to overlap and is located first accommodate the lead screw input, adjacent two be connected through drive chain between the driving sprocket.
Further, the size of the first adjusting screw rod positioned on the left side is longer than the size of the first adjusting screw rod and the size of the second adjusting screw rod positioned on the right side.
The utility model has the advantages that:
the first adjustment mechanism that sets up rather than the inside part that includes, with the cooperation of assisting mutually of the second adjustment mechanism, drive mechanism and the actuating mechanism that set up, adopt driving motor as driven maincenter to and the drive through each sprocket and chain, and adjust in unison through the mode of screw thread, make the accuracy more accurate of regulation, the simple operation simultaneously, the effectual problem of avoiding the cycle length.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention.
Fig. 1 is a schematic view of the overall structure of the high-reliability aviation die multi-wire cutting device of the present invention;
FIG. 2 is a top view of a worktable of the high-reliability aviation die multi-wire cutting device of the present invention;
fig. 3 is an enlarged view of the driving mechanism of the high-reliability aviation die multi-wire cutting device of the invention;
reference numbers in the figures: 1. installing a base; 2. a work table; 3. a first adjustment mechanism; 4. a second adjustment mechanism; 5. a drive mechanism; 6. a drive mechanism; 7. a first adjustment groove; 8. a first adjusting screw rod; 9. a first regulating block; 10. a second adjustment groove; 11. a second adjusting screw rod; 12. a second regulating block; 13. driving the chain wheel; 14. driving the chain; 15. a drive motor; 16. a drive shaft; 17. a drive sprocket; 18. the chain is driven.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are presented herein only to illustrate and explain the present invention, and not to limit the present invention. In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
As shown in fig. 1-3, including installation base 1, installation base 1 top surface is provided with workstation 2, 2 top surfaces of workstation are connected with two-way winding mechanism and guiding mechanism through first adjustment mechanism 3 and second adjustment mechanism 4 respectively, just first adjustment mechanism 3 and second adjustment mechanism 4 symmetry respectively set up in 2 top surfaces of workstation, first adjustment mechanism 3 is connected through drive mechanism 5 with second adjustment mechanism 4 input, is located the left 3 input of first adjustment mechanism is provided with actuating mechanism 6, just actuating mechanism 6 sets up in installation base 1 front surface left side.
As shown in fig. 1, a processing table is arranged between two adjacent second adjusting mechanisms 4, and the processing table is arranged in the middle of the top surface of the workbench 2.
As shown in fig. 2, the first adjusting mechanism 3 includes a first adjusting groove 7, a first adjusting screw 8 and a first adjusting block 9, the first adjusting groove 7 is symmetrically dug on the top surface of the workbench 2, the rear surface of the inner cavity of the first adjusting groove 7 is connected with the first adjusting screw 8 through a bearing, the outer wall of the first adjusting screw 8 is connected with the first adjusting block 9 through a thread and is symmetrically arranged, and the outer wall of the first adjusting screw 8 drives the first adjusting block 9 and the bidirectional winding mechanism thereon to displace through the thread.
The second adjusting mechanism 4 comprises a second adjusting groove 10, a second adjusting screw rod 11 and a second adjusting block 12, the second adjusting groove 10 is symmetrically dug in two sides of the top surface of the workbench 2, the rear surface of the inner cavity of the second adjusting groove 10 is connected with the second adjusting screw rod 11 through a bearing, the outer wall of the second adjusting screw rod 11 is connected with the second adjusting block 12 through threads and symmetrically arranged, and the outer wall of the second adjusting screw rod 11 drives the second adjusting block 12 to move with a guide mechanism arranged on the second adjusting screw rod through threads.
The driving mechanism 5 comprises a driving chain wheel 13 and a driving chain 14, the input ends of the first adjusting screw rods 8 and the second adjusting screw rods 11 extend to the front surface of the workbench 2, the driving chain wheel 13 is respectively sleeved at the input ends of the first adjusting screw rods 8 and the second adjusting screw rods 11, the driving chain wheel 13 is adjacent to the driving chain wheel 13, the driving chain wheel 13 is connected with the driving chain 14, when the first adjusting screw rods 8 are driven, the driving chain wheel 13 on the outer wall of the first adjusting screw rods 8 on the left side is driven, the adjacent driving chain wheel 13 is driven to rotate through the driving chain 14, and therefore each first adjusting screw rod 8 and each second adjusting screw rod 11 rotate.
As shown in fig. 3, the driving mechanism 6 includes a driving motor 15, a driving shaft 16, a driving sprocket 17 and a driving chain 18, the driving motor 15 is disposed on the left side of the front surface of the mounting base 1 through a mounting plate, the driving shaft 16 is disposed at an output end of the driving motor 15, the driving sprocket 17 is sleeved on an outer wall of the driving shaft 16, the driving motor 15 drives the driving sprocket 17 to rotate through the driving shaft 16, the driving sprocket 17 is also sleeved on an input end of the first adjusting screw 8 located on the left side, adjacent driving sprockets 17 are driven by the driving chain 18, so that the driving sprocket 17 sleeved on the first adjusting screw 8 located on the left side rotates and drives the first adjusting screw 8 located on the left side to rotate, two adjacent driving sprockets 17 are connected through the driving chain 18, and the size of the first adjusting screw 8 located on the left side is longer than the sizes of the first adjusting screw 8 and the second adjusting screw 11 located on the right side.
The utility model discloses the theory of operation: firstly, a driving motor 15 drives a driving chain wheel 17 to rotate through a driving shaft 16, adjacent driving chain wheels 17 are driven through a driving chain 18, the driving chain wheel 17 sleeved on a first adjusting screw 8 on the left side is driven to rotate and drives the first adjusting screw 8 on the left side to rotate, a driving chain wheel 13 on the outer wall of the first adjusting screw 8 on the left side is driven, adjacent driving chain wheels 13 are driven to rotate through a driving chain 14, each first adjusting screw 8 and a second adjusting screw 11 are driven to rotate, the first adjusting screw 8 drives a first adjusting block 9 and a bidirectional winding mechanism on the first adjusting screw to displace through threads, and the second adjusting screw 11 drives a second adjusting block 12 and a guide mechanism on the second adjusting screw to displace through threads.
The above is the preferred embodiment of the present invention, and the technical personnel in the field of the present invention can also change and modify the above embodiment, therefore, the present invention is not limited to the above specific embodiment, and any obvious improvement, replacement or modification made by the technical personnel in the field on the basis of the present invention all belong to the protection scope of the present invention.
Claims (7)
1. The utility model provides a high reliability aeronautical mold multi-wire cutting device, includes installation base (1), its characterized in that: installation base (1) top surface is provided with workstation (2), workstation (2) top surface is connected with two-way winding mechanism and guiding mechanism through first adjustment mechanism (3) and second adjustment mechanism (4) respectively, just first adjustment mechanism (3) and second adjustment mechanism (4) symmetry respectively set up in workstation (2) top surface, first adjustment mechanism (3) are connected through drive mechanism (5) with second adjustment mechanism (4) input, are located the left first adjustment mechanism (3) input is provided with actuating mechanism (6), just actuating mechanism (6) set up in installation base (1) front surface left side.
2. The high-reliability multi-wire cutting device for the aviation dies as claimed in claim 1, wherein: a processing table is arranged between every two adjacent second adjusting mechanisms (4), and the processing table is arranged in the middle of the top surface of the workbench (2).
3. The high-reliability multi-wire cutting device for the aviation dies as claimed in claim 2, wherein: first adjustment mechanism (3) include first adjustment tank (7), first accommodate the lead screw (8) and first regulating block (9), workstation (2) top surface is located to first adjustment tank (7) symmetry excavation, first adjustment tank (7) inner chamber rear surface is connected with first accommodate the lead screw (8) through the bearing, first accommodate the lead screw (8) outer wall has first regulating block (9) through threaded connection to be the symmetry setting.
4. The high-reliability multi-wire cutting device for the aviation dies as claimed in claim 3, wherein: second adjustment mechanism (4) include second adjustment tank (10), second accommodate the lead screw (11) and second regulating block (12), workstation (2) top surface both sides are located to second adjustment tank (10) symmetry digging, second adjustment tank (10) inner chamber rear surface is connected with second accommodate the lead screw (11) through the bearing, second accommodate the lead screw (11) outer wall has second regulating block (12) through threaded connection to be the symmetry setting.
5. The high-reliability multi-wire cutting device for the aviation dies as claimed in claim 4, wherein: drive mechanism (5) are including driving sprocket (13) and drive chain (14), first accommodate the lead screw (8) all extend to workstation (2) front surface with second accommodate the lead screw (11) input, drive sprocket (13) and overlap respectively and locate the input of first accommodate the lead screw (8) and second accommodate the lead screw (11), and is adjacent drive and be connected through driving chain (14) between sprocket (13).
6. The high-reliability multi-wire cutting device for the aviation dies as claimed in claim 5, wherein: actuating mechanism (6) include driving motor (15), drive shaft (16), driving sprocket (17) and drive chain (18), driving motor (15) set up in installation base (1) front surface left side through the mounting panel, driving motor (15) output is provided with drive shaft (16), drive shaft (16) outer wall cover is equipped with driving sprocket (17), just driving sprocket (17) are located the left equally to overlap driving sprocket (17) are located first accommodate the lead screw (8) input, adjacent two be connected through drive chain (18) between driving sprocket (17).
7. The high-reliability multi-wire cutting device for the aviation dies as claimed in claim 6, wherein: the first adjusting screw (8) on the left side is longer than the first adjusting screw (8) and the second adjusting screw (11) on the right side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221534690.5U CN217749638U (en) | 2022-06-16 | 2022-06-16 | High-reliability multi-wire cutting device for aviation die |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221534690.5U CN217749638U (en) | 2022-06-16 | 2022-06-16 | High-reliability multi-wire cutting device for aviation die |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217749638U true CN217749638U (en) | 2022-11-08 |
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ID=83895083
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221534690.5U Active CN217749638U (en) | 2022-06-16 | 2022-06-16 | High-reliability multi-wire cutting device for aviation die |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217749638U (en) |
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2022
- 2022-06-16 CN CN202221534690.5U patent/CN217749638U/en active Active
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