CN219665421U - Triaxial five aircraft nose cnc engraving and milling machine - Google Patents
Triaxial five aircraft nose cnc engraving and milling machine Download PDFInfo
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- CN219665421U CN219665421U CN202321337414.4U CN202321337414U CN219665421U CN 219665421 U CN219665421 U CN 219665421U CN 202321337414 U CN202321337414 U CN 202321337414U CN 219665421 U CN219665421 U CN 219665421U
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- 238000003801 milling Methods 0.000 title claims abstract description 17
- 238000001179 sorption measurement Methods 0.000 claims description 19
- 238000012545 processing Methods 0.000 abstract description 16
- 238000004519 manufacturing process Methods 0.000 abstract description 8
- 238000013461 design Methods 0.000 abstract description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 235000012431 wafers Nutrition 0.000 description 2
- 229910000926 A-3 tool steel Inorganic materials 0.000 description 1
- 239000004593 Epoxy Substances 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000003698 laser cutting Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052755 nonmetal Inorganic materials 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
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Abstract
The utility model discloses a triaxial five-machine head engraving and milling machine which comprises a machine base, a portal frame and a machine head structure, wherein the machine base is provided with a machine head; the portal frame comprises a vertical supporting rod and a cross beam, and the cross beam slides up and down relative to the vertical supporting rod through a cross beam driving device; five nose structures are distributed on the cross beam at equal intervals, limiting plates are arranged between adjacent nose structures, and each nose structure moves in the range of the two limiting plates of the cross beam through an independent nose driving device; the machine base is provided with a workbench corresponding to the machine head structure, and the workbench slides relative to the machine base through a chute; the workbench pipeline is connected with a vacuum device. Set up a plurality of aircraft nose structures that go on in step, be equipped with corresponding workstation to realize that multiplex spare is processing simultaneously, improved the efficiency of processing, accomplished output index in time, saved the cost of labor, reasonable in design, low in manufacturing cost.
Description
Technical Field
The utility model relates to the technical field of engraving and milling machines, in particular to a triaxial five-machine head engraving and milling machine.
Background
The engraving and milling machine is one of numerical control machine tools, and can perform non-contact cutting and punching on metal or nonmetal plates and pipes, and is particularly suitable for laser cutting and processing of stainless steel plates, iron plates, silicon wafers, ceramic wafers, titanium alloys, epoxy, A3 steel, diamond and other materials. At present, one machine of the engraving and milling machine can only process one product with two specifications at the same time, and the production efficiency is extremely low; for enterprises for mass production of mechanical parts, the processing production of the mass mechanical parts is completed in time in order to improve the production efficiency. Therefore, it is necessary to provide a three-axis five-station engraving and milling machine.
Disclosure of Invention
In view of the above, the utility model provides a triaxial five-machine head engraving and milling machine.
In order to achieve the above purpose, the present utility model adopts the following technical scheme: comprises a machine base, a portal frame and a machine head structure; the portal frame comprises a vertical supporting rod and a cross beam, and the cross beam slides up and down relative to the vertical supporting rod through a cross beam driving device; five nose structures are distributed on the cross beam at equal intervals, limiting plates are arranged between adjacent nose structures, and each nose structure moves in the range of the two limiting plates of the cross beam through an independent nose driving device; the machine base is provided with a workbench corresponding to the machine head structure, and the workbench slides relative to the machine base through a second sliding block; the workbench pipeline is connected with a vacuum device. Set up a plurality of aircraft nose structures that go on in step, be equipped with corresponding workstation to realize that multiplex spare is processing simultaneously, improved the efficiency of processing, accomplished output index in time, saved the cost of labor, reasonable in design, low in manufacturing cost.
In a further technical scheme, the beam driving device comprises a first sliding rail arranged on the vertical supporting rod, and the beam corresponds to a first sliding block arranged on the first sliding rail. The beam is enabled to slide up and down relative to the vertical supporting rod through the beam driving device, and further five machine head structures also slide up and down along with the beam.
In a further technical scheme, the top end of the vertical supporting rod is provided with a limiting part for limiting the first sliding block. The excessive movement of the cross beam is avoided, so that the cross beam and the vertical supporting rod are separated from each other, and the processing of the workpiece is affected.
In a further technical scheme, the workbench comprises a bottom layer platform and an adsorption platform, wherein the adsorption platform is rotatably arranged above the bottom layer platform through a rotary structure; the machine base is provided with a chute corresponding to the second sliding block. The rotation of the adsorption platform is realized through the rotary structure, so that the direction of a workpiece is changed, and the workpiece is conveniently machined in a limited range by the machine head structure.
In a further technical scheme, the adsorption platform is provided with a plurality of adsorption holes which are regularly arranged. The workpiece placed on the workbench can be adsorbed in vacuum through the adsorption hole, so that the workpiece is not easy to run, the operation is convenient to carry out, and the operation error is effectively avoided.
The machine head driving device in the further technical scheme comprises a fixed plate and a second sliding rail; the fixed plate is fixed with the aircraft nose structure each other, and the second slide rail sets up in the crossbeam, and the recess that corresponds with the second slide rail is seted up to the fixed plate. The machine head driving device controls the machine head structure to slide relative to the cross beam, so that the transverse work of the machine head structure is facilitated.
In a further technical scheme, the vertical supporting rods are provided with three vertical supporting rods which are respectively arranged at the two ends and the middle of the cross beam. The beam is supported from three different positions, so that the excessive load of the beam is avoided, and the up-and-down sliding stability of the beam is ensured.
Compared with the prior art, the utility model has the following beneficial technical effects: set up a plurality of aircraft nose structures that go on in step, be equipped with corresponding workstation to realize that multiplex spare is processing simultaneously, improved the efficiency of processing, accomplished output index in time, saved the cost of labor, reasonable in design, low in manufacturing cost.
Drawings
In order to more clearly illustrate the embodiments of the present utility model or the technical solutions in the prior art, the drawings that are required to be used in the embodiments or the description of the prior art will be briefly described below, and it is obvious that the drawings in the following description are only embodiments of the present utility model, and that other drawings can be obtained according to the provided drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic structural view of the present utility model.
Fig. 2 is an enlarged view at a.
Detailed Description
The utility model will now be described in further detail with reference to the accompanying drawings. The drawings are simplified schematic representations which merely illustrate the basic structure of the utility model and therefore show only the structures which are relevant to the utility model. In the description of the present utility model, it should be understood that the terms "longitudinal," "radial," "length," "width," "thickness," "upper," "lower," "left," "right," "front," "rear," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like indicate orientations or positional relationships based on the orientation or positional relationships shown in the drawings, are merely for convenience in describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present utility model. In the description of the present utility model, unless otherwise indicated, the meaning of "a plurality" is two or more.
In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be either fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
Referring to fig. 1-2, a three-axis five-machine-head engraving and milling machine comprises a machine base 1, a portal frame 2 and a machine head structure 3; the portal frame 2 comprises a vertical supporting rod 21 and a cross beam 22, and the cross beam 22 slides up and down relative to the vertical supporting rod 21 through a cross beam driving device 4; five nose structures 3 are equidistantly distributed on the cross beam 22, limiting plates 5 are arranged between every two adjacent nose structures 3, and each nose structure 3 moves in the range of the two limiting plates 5 of the cross beam 22 through an independent nose driving device 9; the machine base 1 is provided with a workbench 6 corresponding to the machine head structure 3, and the workbench 6 slides relative to the machine base 1 through a chute 611; the workbench 6 is connected with a vacuum device 7 in a pipeline way. Set up a plurality of aircraft nose structures that go on in step, be equipped with corresponding workstation to realize that multiplex spare is processing simultaneously, improved the efficiency of processing, accomplished output index in time, saved the cost of labor, reasonable in design, low in manufacturing cost.
The beam driving device 4 includes a first sliding rail 41 disposed on the vertical supporting rod 21, and a first sliding block 42 disposed on the beam 22, so as to avoid excessive sliding of the beam 22, and make the beam 22 separate from the limitation of the vertical supporting rod 21, and a limiting portion 8 for limiting the first sliding block 42 is disposed at the top end of the vertical supporting rod 21, so as to affect the processing of the workpiece; further, since the five nose structures 3 are mounted on the cross beam 22, the supporting force of the cross beam 22 is limited, so that the excessive load of the cross beam 22 is avoided, three vertical supporting rods 21 are arranged at the two ends and the middle of the cross beam 22 respectively, and the cross beam 22 is supported from three different positions; in order to ensure smooth sliding of the cross beam 22, the three vertical support rods 21 are provided with first slide rails 41, so that stable up-and-down sliding of the cross beam 22 is ensured.
The workbench 6 comprises a bottom layer platform 61 and an adsorption platform 62, and the adsorption platform 62 is rotatably arranged above the bottom layer platform 61 through a rotating structure; further, the machine base 1 is provided with a second sliding block 11 corresponding to the chute 611; the workbench 6 slides with the chute 611 through the second sliding block 11, so that the workpiece can reciprocate in the Y-axis direction; considering that the transverse movement range of the machine head structure 3 is limited, the rotation of the adsorption platform 62 is realized through the rotary structure so as to change the direction of the workpiece, and the machine head structure 3 can conveniently process the workpiece in a limited range.
Further, the adsorption platform 62 is provided with a plurality of regularly arranged adsorption holes 621, and the adsorption platform 62 is connected with the vacuum device 7 through a pipeline. The workpiece placed on the workbench 6 can be adsorbed in vacuum through the adsorption holes 621, so that the workpiece is not easy to run, the operation is convenient to carry out, and the operation error is effectively avoided.
The machine head driving device 9 comprises a fixed plate 91 and a second sliding rail 92; the fixing plate 91 is fixed with the machine head structure 3, the second sliding rail 92 is arranged on the cross beam 22, and the fixing plate 91 is provided with a groove corresponding to the second sliding rail (92). The head structure 3 is controlled to slide relative to the cross beam 22 through the head driving device 9, so that the head structure 3 can conveniently perform transverse work.
The vertical support rods 21, the cross beams 22 and various sliding structural grooves are made of stainless steel materials, and have the characteristics of difficult corrosion, difficult deformation, strong rigidity, easy processing and low cost; the driving components of the beam driving device 4, the machine head driving device 9, the second sliding block 11 and the sliding groove 611 are driving air cylinders or electric cylinders.
The working principle of the utility model is further described below:
the five workpieces are respectively adsorbed on the five adsorption platforms 62, and the five work tables 6 are simultaneously moved into the working range corresponding to the machine head structure 3 through the second sliding block 11 and the sliding groove 611, namely, the Y-axis direction movement; inputting various parameters in a control system, calibrating zero points, simultaneously and automatically moving the five machine head structures 3 to the same direction, namely X-axis direction movement, on the cross beam 22 through the machine head driving device 9, and when the engraving depth of a workpiece needs to be deepened, driving the five machine head structures 3 to move downwards relative to the vertical supporting rod 21, namely Z-axis direction movement by the cross beam 22, and accurately processing the workpiece from three directions, so as to avoid processing errors; meanwhile, the adsorption platform 62 can rotate through the rotary structure so as to change the direction of the workpiece, and the machine head structure 3 is convenient for processing the workpiece in a limited range.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present utility model. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the utility model. Thus, the present utility model is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (7)
1. A triaxial five aircraft nose cnc engraving and milling machine, its characterized in that: comprises a machine base (1), a portal frame (2) and a machine head structure (3); the portal frame (2) comprises a vertical supporting rod (21) and a cross beam (22), and the cross beam (22) slides up and down relative to the vertical supporting rod (21) through a cross beam driving device (4); five nose structures (3) are equidistantly distributed on the cross beam (22), limiting plates (5) are arranged between adjacent nose structures (3), and each nose structure (3) moves in the range of the two limiting plates (5) of the cross beam (22) through an independent nose driving device (9); the machine base (1) is provided with a workbench (6) corresponding to the machine head structure (3), and the workbench (6) slides relative to the machine base (1) through a chute (611); the workbench (6) is connected with a vacuum device (7) through a pipeline.
2. A triaxial five-head engraving and milling machine as defined in claim 1, characterized in that: the beam driving device (4) comprises a first sliding rail (41) arranged on the vertical supporting rod (21), and the beam (22) corresponds to a first sliding block (42) arranged on the first sliding rail (41).
3. A triaxial five-head engraving and milling machine as defined in claim 2, characterized in that: the top end of the vertical supporting rod (21) is provided with a limiting part (8) for limiting the first sliding block (42).
4. A triaxial five-head engraving and milling machine as defined in claim 1, characterized in that: the workbench (6) comprises a bottom layer platform (61) and an adsorption platform (62), and the adsorption platform (62) is rotatably arranged above the bottom layer platform (61) through a rotary structure; the machine base (1) is provided with a second sliding block (11) corresponding to the sliding groove (611).
5. The three-axis five-head engraving and milling machine as recited in claim 4, wherein: the adsorption platform (62) is provided with a plurality of adsorption holes (621) which are regularly arranged.
6. A triaxial five-head engraving and milling machine as defined in claim 1, characterized in that: the machine head driving device (9) comprises a fixed plate (91) and a second sliding rail (92); the fixed plate (91) is fixed with the machine head structure (3) mutually, the second sliding rail (92) is arranged on the cross beam (22), and the fixed plate (91) is provided with a groove corresponding to the second sliding rail (92).
7. A triaxial five-head engraving and milling machine as defined in claim 1, characterized in that: the vertical support rods (21) are arranged at the two ends and the middle of the cross beam (22) respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321337414.4U CN219665421U (en) | 2023-05-30 | 2023-05-30 | Triaxial five aircraft nose cnc engraving and milling machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321337414.4U CN219665421U (en) | 2023-05-30 | 2023-05-30 | Triaxial five aircraft nose cnc engraving and milling machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219665421U true CN219665421U (en) | 2023-09-12 |
Family
ID=87897428
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321337414.4U Active CN219665421U (en) | 2023-05-30 | 2023-05-30 | Triaxial five aircraft nose cnc engraving and milling machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219665421U (en) |
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2023
- 2023-05-30 CN CN202321337414.4U patent/CN219665421U/en active Active
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