CN219292934U - Aviation blade air film hole processing machine tool - Google Patents
Aviation blade air film hole processing machine tool Download PDFInfo
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- CN219292934U CN219292934U CN202223092367.XU CN202223092367U CN219292934U CN 219292934 U CN219292934 U CN 219292934U CN 202223092367 U CN202223092367 U CN 202223092367U CN 219292934 U CN219292934 U CN 219292934U
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Abstract
The utility model provides an aviation blade air film hole machining tool, relates to the technical field of machining equipment, and solves the technical problem of low machining efficiency of the tool. The aviation blade air film hole machining machine tool comprises a machine body, an upright post arranged on the machine body, double-processing stations arranged on the machine body side by side, seven linear motion numerical control shafts X1, Y, Z, W1, X2, Y, Z and W2 which are arranged on the upright post and respectively correspond to the double-processing stations, three rotary motion numerical control shafts A, C and A, C2 which are arranged on the machine body and respectively correspond to the double-processing stations, and an air film hole machining unit arranged on the two linear motion numerical control shafts W1 and W2. The machining tool for the ten-axis double-station aviation blade air film holes is used for machining the aviation blade air film holes, is provided with two machining stations, can be used for machining two aviation blades at the same time, and is compact in structure and low in cost.
Description
Technical Field
The utility model relates to the technical field of processing equipment, in particular to an aviation blade air film hole processing machine tool.
Background
Aero-engine blades are key functional components of high performance aero-engines, and their high temperature resistance directly determines the performance of the aero-engine. In order to improve the high temperature resistance of the aero-engine blade, air film holes are usually processed on the aero-engine blade. The existence of the air film hole enables the aeroengine to flow out of the air film hole and attach the air film hole to the surface of the blade when the aeroengine works, so that an air film cooling heat insulation layer is formed, and the high temperature resistance of the aeroengine blade can be remarkably improved. In order to realize high-precision machining of the air film holes of the aviation blades, high-efficiency and precision machining of the parts is finished by technical means such as electric spark, electrochemistry, laser machining and the like at present, wherein an electric spark small hole machining technology is the most mature and stable machining means.
The applicant found that the prior art has at least the following technical problems:
at present, an electric spark processing small hole machine for an air film hole of an aviation blade is commonly used, one machine tool can only process one part at the same time, the processing efficiency is low, and how to improve the processing efficiency of the small hole machine is a technical problem to be solved urgently.
Disclosure of Invention
The utility model aims to provide a ten-axis numerical control double-station aviation blade air film hole processing machine tool, which aims to solve the technical problem of low machine tool processing efficiency in the prior art.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
the utility model provides an aviation blade air film hole processing machine tool which comprises a machine body, an upright post arranged on the machine body, double-processing stations arranged on the machine body side by side, seven linear motion numerical control shafts, namely an X1 shaft, a Y shaft, a Z1 shaft, a W1 shaft, an X2 shaft, a Y shaft, a Z2 shaft and a W2 shaft, which are respectively corresponding to the double-processing stations, and an air film hole processing unit, which is arranged on the upright post, respectively corresponds to an A shaft, a C1 shaft, an A shaft and a C2 shaft of the double-processing stations, and is arranged on the machine body.
As a further improvement of the utility model, the Y-axis linear motion numerical control shaft comprises two Y-axis guide rail assemblies and two Y-axis servo drive assemblies, the Y-axis servo drive assemblies are arranged on the upright posts positioned at the outer sides of the double machining positions, and the Y-axis servo drive assemblies are in transmission connection with the X1-axis linear motion numerical control shaft and the X2-axis linear motion numerical control shaft so as to drive the Y-axis servo drive assemblies to perform linear motion along the directions of the Y-axis guide rail assemblies.
As a further improvement of the utility model, the X1 axis linear motion numerical control shaft comprises an X1 axis guide rail assembly and an X1 axis servo drive assembly, the X2 axis linear motion numerical control shaft comprises an X2 axis guide rail assembly and an X2 axis servo drive assembly, and the X1 axis guide rail assembly and the X2 axis guide rail assembly are arranged in parallel up and down and are all arranged on a sliding rail; the initial end of the sliding rail is arranged on the Y-axis guide rail assembly on one side in a sliding way, and the tail end of the sliding rail is arranged on the Y-axis guide rail assembly on the other side in a sliding way; the X1-axis servo driving assembly is in transmission connection with the Z1-axis linear motion numerical control shaft so as to drive the X1-axis servo driving assembly to perform linear motion along the X1-axis guide rail assembly; the X2-axis servo driving assembly is in transmission connection with the Z2-axis linear motion numerical control shaft so as to drive the X2-axis servo driving assembly to perform linear motion along the X2-axis guide rail direction.
As a further improvement of the utility model, the Z1 axis linear motion numerical control shaft comprises a Z1 axis adapter plate and a Z1 axis servo drive assembly, wherein the Z1 axis servo drive assembly is in sliding connection with the X1 axis guide rail assembly through the Z1 axis adapter plate, and the X1 axis servo drive assembly is in transmission connection with the Z1 axis adapter plate; the Z2 axis linear motion numerical control shaft comprises a Z2 axis adapter plate and a Z2 axis servo drive assembly, the Z2 axis servo drive assembly is in sliding connection with the X2 axis guide rail assembly through the Z2 axis adapter plate, and the X2 axis servo drive assembly is in transmission connection with the Z2 axis adapter plate; the W1 axis linear motion numerical control shaft is arranged on the Z1 axis servo driving assembly; the W2 axis linear motion numerical control shaft is arranged on the Z2 axis servo driving assembly.
As a further improvement of the utility model, the W1 axis linear motion numerical control shaft comprises a W1 axis driving assembly, and the W2 axis linear motion numerical control shaft comprises a W2 axis driving assembly; the number of the air film hole processing units is two, and the air film hole processing units are respectively arranged on the W1 shaft driving assembly and the W2 shaft driving assembly.
As a further improvement of the utility model, the A-axis rotary motion numerical control shaft is a numerical control shaft capable of rotating around the X1 axis or the X2 axis, and the C1-axis rotary motion numerical control shaft and the C2-axis rotary motion numerical control shaft are arranged on the A-axis rotary motion numerical control shaft.
As a further improvement of the present utility model, the C1 axis rotational movement numerical control axis includes a C1 axis rotatable about itself; the C2 axis rotary motion numerical control shaft comprises a C2 axis capable of rotating around the C2 axis.
As a further improvement of the utility model, the air film hole processing unit corresponding to the first processing station comprises a first rotating shaft, a first electrode wire and a first guide, wherein the first rotating shaft and the first guide are both arranged on the Z1-axis servo driving assembly, and the first electrode wire is fixed on the first rotating shaft; the air film hole machining unit corresponding to the second machining station comprises a second rotating shaft, a second electrode wire and a second guide, wherein the second rotating shaft and the second guide are both installed on the Z2-axis servo driving assembly, and the second electrode wire is fixed on the second rotating shaft.
As a further improvement of the utility model, the machine tool also comprises a water tank arranged on the machine tool body and positioned below the double machining positions.
As a further improvement of the utility model, the Y-axis guide rail assembly, the X1-axis guide rail assembly and the X2-axis guide rail assembly all comprise sliding rails, and the sliding rails are I-shaped sliding rails.
Compared with the prior art, the utility model has the following beneficial effects:
the utility model provides an aviation blade air film hole processing machine tool, which is a ten-axis double-station aviation blade air film hole processing machine tool, and comprises seven linear motion numerical control shafts X1, X2, Y, Z1, Z2, W1 and W2, and A, C and C2 three rotary motion numerical control shafts, wherein one machine tool is provided with two processing stations, can process two aviation blades at the same time, greatly improves the processing efficiency, and has the advantages of low cost, compact structure and the like compared with two single-station small hole machines; the three rotating shafts A, C and C2 are assembled together, the rotating angles of the workpiece around the X axis are uniformly controlled by the A axis, the rotating shafts C1 and C2 respectively control the indexing angles of the blade parts clamped on the rotating shafts along the respective axes, and the double-station indexing processing requirement of the same type of parts can be realized; the Z1 axis is arranged on the X1 axis through the W1 axis; the W2 axis is arranged on the Z2 axis, and the Z2 axis is arranged on the X2 axis; the X1 axis and the X2 axis are jointly arranged on the Y axis, so that the synchronous machining requirement of holes of the same type on two aviation blades is met.
Drawings
In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly described, it being obvious that the drawings in the following description are only some embodiments of the utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic diagram of the layout of each axis of an aviation blade air film hole processing machine tool;
fig. 2 is a schematic structural diagram of an aviation blade air film hole processing machine tool.
In the figure, 1, a lathe bed; 2. a water tank; 3. a three-axis turntable; 4. aviation blade II; 5. a second guide; 6. a second wire electrode; 7. a column; 8. a second Y-axis guide rail assembly; 9. a second rotation shaft; 10. an X2 axis servo drive assembly; 11. w2 axle drive assembly; 12. a ram; 13. z2 axis servo drive assembly; 14. z2 axis adapter plate; 15. y-axis servo drive assembly; 16. z1 axis servo drive assembly; 17. z1 axis adapter plate; 18. an X1 axis guide rail assembly; 19. w1 axis drive assembly; 20. x1 axis servo drive assembly; 21. a first rotation shaft; 22. an X2 axis guide rail assembly; 23. a first Y-axis guide rail assembly; 24. a first wire electrode; 25. a first guide; 26. aviation blade I.
Detailed Description
In order to make the objects, technical solutions and advantages of the present utility model more apparent, the technical solutions of the present utility model will be described in detail below. It will be apparent that the described embodiments are only some, but not all, embodiments of the utility model. All other embodiments, based on the examples herein, which are within the scope of the utility model as defined by the claims, will be within the scope of the utility model as defined by the claims.
As shown in fig. 1, the utility model provides an aviation blade air film hole processing machine tool, which comprises a machine body 1, an upright post 7 arranged on the machine body 1, double-processing stations arranged on the machine body 1 side by side, seven linear motion numerical control shafts of an X1 shaft, a Y shaft, a Z1 shaft, a W1 shaft, an X2 shaft, a Y shaft, a Z2 shaft and a W2 shaft which are respectively corresponding to the double-processing stations and three rotary motion numerical control shafts of an A shaft, a C1 shaft, an A shaft and a C2 shaft which are respectively corresponding to the double-processing stations and an air film hole processing unit arranged on the W1 shaft linear motion numerical control shaft and the W2 shaft linear motion numerical control shaft.
Specifically, the numerical control axis of linear motion of the X1 axis, that is, the X1 axis, is the left-right length direction of the lathe bed 1; the X2 axis linear motion numerical control axis is the length direction of the machine tool body 1 from left to right, and is arranged from left to right with the X1 axis, the Y axis linear motion numerical control axis is the Y axis, is the width direction of the machine tool body 1 from front to back, the Z1 axis linear motion numerical control axis is the Z1 axis, is the height direction of the machine tool body 1 from top to bottom, the Z2 axis linear motion numerical control axis is the Z2 axis, is the height direction of the machine tool body 1 from top to bottom; the W1 axis linear motion numerical control axis is the W1 axis, and is the height direction of the lathe bed 1 up and down; the W2 axis linear motion numerical control axis is the W2 axis, and is the height direction of the lathe bed 1; the A-axis rotary motion numerical control axis is the A-axis, and is the rotary direction around the X1 axis or the X2 axis; the C1 axis rotary motion numerical control axis is the C1 axis, and is the rotary direction of the vertical line around the X1 axis; the C2 axis rotational movement numerical control axis, i.e., the C2 axis, is the rotational direction about the perpendicular to the X2 axis.
As an alternative implementation mode of the utility model, the Y-axis linear motion numerical control shaft comprises two Y-axis guide rail assemblies and two Y-axis servo drive assemblies 15, wherein the number of the Y-axis guide rail assemblies is two, namely a first Y-axis guide rail assembly 23 and a second Y-axis guide rail assembly 8, the number of the upright posts 7 is two, the upright posts 7 are respectively arranged at the left side and the right side of the machine body 1, the first Y-axis guide rail assembly 23 is arranged at the top of the left upright post 7, the second Y-axis guide rail assembly 8 is arranged at the top of the right upright post 7, and the Y-axis servo drive assemblies 15 are in transmission connection with the X1-axis linear motion numerical control shaft and the X2-axis linear motion numerical control shaft so as to drive the Y-axis guide rail assemblies to perform linear motion along the direction of the Y-axis guide rail assemblies.
Specifically, the X1 axis linear motion numerical control axis and the X2 axis linear motion numerical control axis reciprocate along the first Y axis guide rail assembly 23 and the second Y axis guide rail assembly 8 under the drive of the Y axis servo drive assembly 15.
As shown in fig. 2, the X1 axis linear motion numerical control axis comprises an X1 axis guide rail assembly 18 and an X1 axis servo drive assembly 20, the X2 axis linear motion numerical control axis comprises an X2 axis guide rail assembly 22 and an X2 axis servo drive assembly 10, and the X1 axis guide rail assembly 18 and the X2 axis guide rail assembly 22 are arranged in parallel up and down and are all mounted on the slide rail 12; the initial end of the sliding rail 12 is arranged on the Y-axis guide rail assembly at one side, namely the first Y-axis guide rail assembly 23, and the tail end of the sliding rail 12 is arranged on the Y-axis guide rail assembly at the other side, namely the second Y-axis guide rail assembly 8; the X1 axis servo driving assembly 20 is in transmission connection with the Z1 axis linear motion numerical control shaft so as to drive the X1 axis guide rail assembly to perform linear motion along the direction of the X1 axis guide rail assembly 18; the X2-axis servo driving assembly 10 is in transmission connection with the Z2 linear motion numerical control shaft so as to drive the X2-axis servo driving assembly to perform linear motion along the X2-axis guide rail direction 22.
As shown in fig. 2, the Z1 axis linear motion numerical control axis comprises a Z1 axis adapter plate 17 and a Z1 axis servo drive assembly 16, the Z1 axis servo drive assembly 16 is slidably connected with an X1 axis guide rail assembly 18 through the Z1 axis adapter plate 17, and the X1 axis servo drive assembly 20 is in transmission connection with the Z1 axis adapter plate 17; the Z2 axis linear motion numerical control shaft comprises a Z2 axis adapter plate 14 and a Z2 axis servo drive assembly 13, the Z2 axis servo drive assembly 13 is in sliding connection with an X2 axis guide rail assembly 22 through the Z2 axis adapter plate 14, and the X2 axis servo drive assembly 10 is in transmission connection with the Z2 axis adapter plate 14; the W1 axis linear motion numerical control shaft is arranged on the Z1 axis servo driving assembly 16; the W2 axis linear motion numerical control shaft is arranged on the Z2 axis servo driving assembly 13. Aviation blade I26 installs and carries out the air film hole processing on the C1 axle, aviation blade II4 installs and carries out the air film hole processing on the C2 axle.
As shown in fig. 2, the W1 axis linear motion numerical control axis includes a W1 axis drive assembly 19, and the W2 axis linear motion numerical control axis includes a W2 axis drive assembly 11; the number of the air film hole processing units is two, and the air film hole processing units are respectively arranged on the W1 shaft driving assembly 19 and the W2 shaft driving assembly 11.
As shown in fig. 2, the a-axis rotary motion numerical control shaft comprises a numerical control shaft capable of rotating around the X1 axis or the X2 axis, the C1 rotary motion numerical control shaft and the C2 rotary motion numerical control shaft are mounted on the a-axis rotary motion numerical control shaft, and further, the a-axis rotary motion numerical control shaft, the C1 rotary motion numerical control shaft and the C2 rotary motion numerical control shaft jointly form a three-axis turntable 3.
As shown in fig. 2, the C1 rotary motion numerical control shaft includes a C1 shaft rotatable around itself; the C2 rotary motion numerical control shaft includes a C2 shaft capable of rotating around itself.
As shown in fig. 2, the air film hole processing unit corresponding to the first processing station comprises a first rotating shaft 21, a first electrode wire 24 and a first guide 25, wherein the first rotating shaft 21 and the first guide 25 are both arranged on the Z1 servo driving assembly 16, and the first electrode wire 24 is fixed on the first rotating shaft 21; the air film hole processing unit corresponding to the second processing station comprises a second rotating shaft 9, a second electrode wire 6 and a second guide 5, wherein the second rotating shaft 9 and the second guide 5 are both arranged on a Z2 servo driving assembly 13, and the second electrode wire 6 is fixed on the second rotating shaft 9.
As shown in fig. 2, the machine tool further comprises a water tank 2 arranged on the machine tool body 1 and positioned below the double machining positions.
The Y-axis guide rail assembly, the X1-axis guide rail assembly and the X2-axis guide rail assembly all comprise sliding rails which are I-shaped sliding rails.
The utility model provides an aviation blade air film hole processing machine tool, which is a ten-axis double-station aviation blade air film hole processing machine tool, and comprises seven linear motion numerical control shafts X1, X2, Y, Z1, Z2, W1 and W2, and A, C and C2 three rotary motion numerical control shafts, wherein one machine tool is provided with two processing stations, can process two aviation blades at the same time, greatly improves the processing efficiency, and has the advantages of low cost, compact structure and the like compared with two single-station small hole machines; the three rotating shafts A, C and C2 are assembled together, the rotating angles of the workpiece around the X axis are uniformly controlled by the A axis, the rotating shafts C1 and C2 respectively control the indexing angles of the blade parts clamped on the rotating shafts along the respective axes, and the double-station indexing processing requirement of the same type of parts can be realized; the Z1 axis is arranged on the X1 axis through the W1 axis; the W2 axis is arranged on the Z2 axis, and the Z2 axis is arranged on the X2 axis; the X1 axis and the X2 axis are jointly arranged on the Y axis, so that the synchronous machining requirement of holes of the same type on two aviation blades is met.
Here, first, the "inward" is a direction toward the center of the accommodating space, and the "outward" is a direction away from the center of the accommodating space.
In the description of the present utility model, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in fig. 1 are merely for convenience in describing the present utility model and simplifying the description, and do not indicate or imply that the device or element being referred to must have a specific orientation, be configured and operated in a specific orientation, and therefore should not be construed as limiting the present utility model.
Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include at least one such feature. In the description of the present utility model, the meaning of "plurality" means at least two, for example, two, three, etc., unless specifically defined otherwise.
In the present utility model, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly, through intermediaries, or both, may be in communication with each other or in interaction with each other, unless expressly defined otherwise. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art according to the specific circumstances.
In the present utility model, unless expressly stated or limited otherwise, a first feature "up" or "down" a second feature may be the first and second features in direct contact, or the first and second features in indirect contact via an intervening medium. Moreover, a first feature being "above," "over" and "on" a second feature may be a first feature being directly above or obliquely above the second feature, or simply indicating that the first feature is level higher than the second feature. The first feature being "under", "below" and "beneath" the second feature may be the first feature being directly under or obliquely below the second feature, or simply indicating that the first feature is less level than the second feature.
In the description of the present specification, a description referring to terms "one embodiment," "some embodiments," "examples," "specific examples," or "some examples," etc., means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the present utility model. In this specification, schematic representations of the above terms are not necessarily directed to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, the different embodiments or examples described in this specification and the features of the different embodiments or examples may be combined and combined by those skilled in the art without contradiction.
The foregoing is merely illustrative of the present utility model, and the present utility model is not limited thereto, and any person skilled in the art will readily recognize that variations or substitutions are within the scope of the present utility model. Therefore, the protection scope of the present utility model shall be subject to the protection scope of the claims.
Claims (9)
1. The aviation blade air film hole machining machine tool is characterized by comprising a machine body, an upright post arranged on the machine body, double-processing stations arranged on the machine body side by side, seven linear motion numerical control shafts, namely an X1 shaft, a Y shaft, a Z1 shaft, a W1 shaft, an X2 shaft, a Y shaft, a Z2 shaft and a W2 shaft, which are respectively corresponding to the double-processing stations, and an air film hole machining unit, which is arranged on the upright post, is respectively corresponding to the three rotary motion numerical control shafts of an A shaft, a C1 shaft, an A shaft and a C2 shaft of the double-processing stations, and is arranged on the linear motion numerical control shafts of the W1 shaft and the linear motion numerical control shafts of the W2 shaft; the air film hole machining unit corresponding to the first machining station comprises a first rotating shaft, a first electrode wire and a first guide, wherein the first rotating shaft and the first guide are both arranged on the Z1-axis servo driving assembly, and the first electrode wire is fixed on the first rotating shaft; the air film hole machining unit corresponding to the second machining station comprises a second rotating shaft, a second electrode wire and a second guide, wherein the second rotating shaft and the second guide are both installed on the Z2-axis servo driving assembly, and the second electrode wire is fixed on the second rotating shaft.
2. The aviation blade air film hole processing machine tool according to claim 1, wherein the Y-axis linear motion numerical control shaft comprises two Y-axis guide rail assemblies and two Y-axis servo drive assemblies, the Y-axis servo drive assemblies are arranged on the upright posts positioned on the outer sides of the double processing positions, and the Y-axis servo drive assemblies are in transmission connection with the X1-axis linear motion numerical control shaft and the X2-axis linear motion numerical control shaft so as to drive the Y-axis servo drive assemblies to perform linear motion along the Y-axis guide rail assembly direction.
3. The aviation blade air film hole processing machine tool according to claim 2, wherein the X1 axis linear motion numerical control shaft comprises an X1 axis guide rail assembly and an X1 axis servo drive assembly, the X2 axis linear motion numerical control shaft comprises an X2 axis guide rail assembly and an X2 axis servo drive assembly, and the X1 axis guide rail assembly and the X2 axis guide rail assembly are arranged in parallel up and down and are all arranged on a sliding rail; the initial end of the sliding rail is arranged on the Y-axis guide rail assembly on one side in a sliding way, and the tail end of the sliding rail is arranged on the Y-axis guide rail assembly on the other side in a sliding way; the X1-axis servo driving assembly is in transmission connection with the Z1-axis linear motion numerical control shaft so as to drive the X1-axis servo driving assembly to perform linear motion along the X1-axis guide rail assembly; the X2-axis servo driving assembly is in transmission connection with the Z2-axis linear motion numerical control shaft so as to drive the X2-axis servo driving assembly to perform linear motion along the X2-axis guide rail direction.
4. The aviation blade air film hole processing machine tool according to claim 3, wherein the Z1 axis linear motion numerical control shaft comprises a Z1 axis adapter plate and a Z1 axis servo drive assembly, the Z1 axis servo drive assembly is in sliding connection with the X1 axis guide rail assembly through the Z1 axis adapter plate, and the X1 axis servo drive assembly is in transmission connection with the Z1 axis adapter plate; the Z2 axis linear motion numerical control shaft comprises a Z2 axis adapter plate and a Z2 axis servo drive assembly, the Z2 axis servo drive assembly is in sliding connection with the X2 axis guide rail assembly through the Z2 axis adapter plate, and the X2 axis servo drive assembly is in transmission connection with the Z2 axis adapter plate; the W1 axis linear motion numerical control shaft is arranged on the Z1 axis servo driving assembly; the W2 axis linear motion numerical control shaft is arranged on the Z2 axis servo driving assembly.
5. The aircraft blade air film hole machining tool of claim 4, wherein the W1 axis linear motion numerical control axis comprises a W1 axis drive assembly and the W2 axis linear motion numerical control axis comprises a W2 axis drive assembly; the number of the air film hole processing units is two, and the air film hole processing units are respectively arranged on the W1 shaft driving assembly and the W2 shaft driving assembly.
6. The aircraft blade air film hole machining tool of claim 1, wherein the a-axis rotational movement numerical control shaft is a numerical control shaft capable of rotating around an X1 axis or an X2 axis, and the C1-axis rotational movement numerical control shaft and the C2-axis rotational movement numerical control shaft are mounted on the a-axis rotational movement numerical control shaft.
7. The aircraft blade air film hole machining tool of claim 6 wherein said C1 axis rotational motion numerical control axis comprises a C1 axis rotatable about itself; the C2 axis rotary motion numerical control shaft comprises a C2 axis capable of rotating around the C2 axis.
8. The aircraft blade film hole machining tool of claim 1, further comprising a water trough disposed on the lathe bed below the double machining location.
9. The aircraft blade air film hole processing machine of claim 3, wherein the Y-axis guide rail assembly, the X1-axis guide rail assembly, and the X2-axis guide rail assembly each comprise a slide rail, the slide rail being an i-shaped slide rail.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223092367.XU CN219292934U (en) | 2022-11-06 | 2022-11-06 | Aviation blade air film hole processing machine tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223092367.XU CN219292934U (en) | 2022-11-06 | 2022-11-06 | Aviation blade air film hole processing machine tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219292934U true CN219292934U (en) | 2023-07-04 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223092367.XU Active CN219292934U (en) | 2022-11-06 | 2022-11-06 | Aviation blade air film hole processing machine tool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219292934U (en) |
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2022
- 2022-11-06 CN CN202223092367.XU patent/CN219292934U/en active Active
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