CN219359283U - Multi-degree-of-freedom four-axis adjusting clamp for machining aviation parts - Google Patents
Multi-degree-of-freedom four-axis adjusting clamp for machining aviation parts Download PDFInfo
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- CN219359283U CN219359283U CN202320570753.0U CN202320570753U CN219359283U CN 219359283 U CN219359283 U CN 219359283U CN 202320570753 U CN202320570753 U CN 202320570753U CN 219359283 U CN219359283 U CN 219359283U
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- rotating shaft
- axis adjusting
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model discloses a multi-degree-of-freedom four-axis adjusting clamp for machining aviation parts, which relates to the technical field of machining of aviation parts and comprises a mounting plate and a circular plate, wherein the circular plate is positioned above the mounting plate, a mounting hole is formed in the mounting plate, a four-axis adjusting clamp body is mounted on the upper surface of the circular plate, a first angle adjusting mechanism is arranged below the circular plate, and a second angle adjusting mechanism is arranged above the mounting plate. The four-axis adjusting clamp body is used for fixing and rotating the aviation part, the first angle adjusting mechanism can enable the aviation part to swing along the left-right direction according to processing requirements, the second angle adjusting mechanism can enable the aviation part to swing along the front-back direction according to the processing requirements, and therefore free adjustment of multiple angles can be carried out on the aviation part, and further processing efficiency of the aviation part can be greatly improved.
Description
Technical Field
The utility model relates to the technical field of aviation part machining, in particular to a multi-degree-of-freedom four-axis adjusting clamp for aviation part machining.
Background
Along with the continuous development of aviation industry, the trend of diversification appears in aviation part, and more accurate complicacy, clamping location, processing, detection etc. all need special machine, and in the in-process to aviation part processing manufacturing, in order to make the better by processing of part, on the basis of X, Y, Z axle in the past, increase the swivel to form the mode of four axles, realize the diversification of anchor clamps, so that adjust the processing to aviation part.
Most of the existing four-axis adjusting clamps cannot freely adjust a plurality of angles of the aviation part according to processing requirements, so that the processing efficiency of the aviation part can be greatly affected; therefore, the multi-degree-of-freedom four-axis adjusting clamp for machining the aviation parts solves the problems.
Disclosure of Invention
The utility model aims to make up the defects of the prior art and provides a multi-degree-of-freedom four-axis adjusting clamp for machining aviation parts.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides a four-axis adjustment anchor clamps of multi freedom of aviation part processing, includes mounting panel and circular plate, the circular plate is located the top of mounting panel, the mounting hole has been seted up to the inside of mounting panel, four-axis adjustment anchor clamps body are installed to the upper surface mounting of circular plate, the below of circular plate is provided with first angle adjustment mechanism, the top of mounting panel is provided with second angle adjustment mechanism.
Further, the first angle adjusting mechanism comprises a rotating plate and a first rotating shaft, the outer surface of the first rotating shaft is rotationally connected with a first U-shaped plate, and the bottom surface of the first U-shaped plate is fixedly connected with the upper surface of the rotating plate.
Further, a motor is arranged on the outer surface of the first U-shaped plate, and the output end of the motor is fixedly connected with one end of the first rotating shaft.
Further, the outer surface of the first rotating shaft is fixedly connected with a first rotating block, and the upper surface of the first rotating block is fixedly connected with the bottom surface of the circular plate.
Further, the second angle adjustment mechanism comprises a second rotating shaft, the outer surface of the second rotating shaft is fixedly connected with the inner wall of the rotating plate, the outer surface of the second rotating shaft is rotationally connected with two supporting plates, and the bottom surfaces of the two supporting plates are fixedly connected with the upper surface of the mounting plate.
Further, the second angle adjusting mechanism further comprises two third rotating shafts, the outer surfaces of the two third rotating shafts are rotationally connected with second U-shaped plates, and one far away surfaces of the two second U-shaped plates are fixedly connected with one close to one surfaces of the rotating plates and the mounting plates respectively.
Further, the outer surfaces of the two third rotating shafts are fixedly connected with second rotating blocks, one of the outer surfaces of the second rotating blocks is provided with an electric telescopic rod, and the telescopic end of the electric telescopic rod is fixedly connected with the outer surface of the other second rotating block.
Compared with the prior art, the multi-degree-of-freedom four-axis adjusting clamp for machining the aviation part has the following beneficial effects:
1. according to the utility model, through the cooperation among the four-axis adjusting clamp body, the first angle adjusting mechanism and the second angle adjusting mechanism, the aviation part can be fixed and rotated by utilizing the four-axis adjusting clamp body, the aviation part can swing in the left-right direction by utilizing the first angle adjusting mechanism according to the processing requirement, and the aviation part can swing in the front-back direction by utilizing the second angle adjusting mechanism according to the processing requirement, so that the aviation part can be freely adjusted in multiple angles, and the processing efficiency of the aviation part can be greatly improved.
2. The utility model can be convenient for installing the device at a specified position by using the screw through the matching between the installation plate and the installation.
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is a side view of the present utility model;
FIG. 3 is a schematic view of the connection of a first rotating shaft and a first U-shaped plate according to the present utility model;
FIG. 4 is a schematic diagram showing the connection of a second rotating shaft and a support plate according to the present utility model;
fig. 5 is a schematic diagram of the connection of the second rotating block and the electric telescopic rod according to the present utility model.
In the figure: 1. a mounting plate; 2. a circular plate; 3. a first angle adjustment mechanism; 301. a rotating plate; 302. a first rotation shaft; 303. a first U-shaped plate; 304. a motor; 305. a first rotating block; 4. a second angle adjustment mechanism; 401. a second rotation shaft; 402. a support plate; 403. a third rotation shaft; 404. a second U-shaped plate; 405. a second rotating block; 406. an electric telescopic rod; 5. four-axis adjustment anchor clamps body.
Detailed Description
The principles and features of the present utility model are described below with reference to the drawings, the examples are illustrated for the purpose of illustrating the utility model and are not to be construed as limiting the scope of the utility model.
The embodiment provides a multi freedom four-axis adjustment anchor clamps of aviation part processing, the device is used for processing aviation part, through the first angle adjustment mechanism 3 and the second angle adjustment mechanism 4 that set up, can carry out the free regulation of a plurality of angles to aviation part according to the processing demand to can greatly improve aviation part's machining efficiency.
Referring to fig. 1 to 5, a multi-degree-of-freedom four-axis adjusting clamp for machining aviation parts comprises a mounting plate 1 and a circular plate 2, wherein the circular plate 2 is located above the mounting plate 1, a mounting hole is formed in the mounting plate 1, a four-axis adjusting clamp body 5 is mounted on the upper surface of the circular plate 2, a first angle adjusting mechanism 3 is arranged below the circular plate 2, and a second angle adjusting mechanism 4 is arranged above the mounting plate 1.
The four-axis adjusting fixture body 5 is a rotary fixture, is mainly used for carrying out multi-face cutting processing on a workpiece, meets the use requirement of a product, can be convenient to use a screw to install the device at a specified position through the cooperation between the mounting plate 1 and the installation, can enable an aviation part to swing along the left-right direction according to the processing requirement through setting the first angle adjusting mechanism 3, can enable the aviation part to swing along the front-back direction according to the processing requirement through setting the second angle adjusting mechanism 4, and therefore can carry out free adjustment of a plurality of angles on the aviation part, and further can greatly improve the processing efficiency of the aviation part.
The first angle adjustment mechanism 3 comprises a rotating plate 301 and a first rotating shaft 302, the outer surface of the first rotating shaft 302 is rotationally connected with a first U-shaped plate 303, the bottom surface of the first U-shaped plate 303 is fixedly connected with the upper surface of the rotating plate 301, a motor 304 is mounted on the outer surface of the first U-shaped plate 303, the output end of the motor 304 is fixedly connected with one end of the first rotating shaft 302, a first rotating block 305 is fixedly connected with the outer surface of the first rotating shaft 302, the upper surface of the first rotating block 305 is fixedly connected with the bottom surface of the circular plate 2, the motor 304 and the motor 304 can drive the first rotating shaft 302 to rotate, and the first rotating shaft 302 can drive the first rotating block 305, the circular plate 2, the four-axis adjustment fixture body 5 and aviation parts to swing along the left-right direction.
The second angle adjusting mechanism 4 comprises a second rotating shaft 401, the outer surface of the second rotating shaft 401 is fixedly connected with the inner wall of the rotating plate 301, two supporting plates 402 are rotatably connected to the outer surface of the second rotating shaft 401, the bottom surfaces of the two supporting plates 402 are fixedly connected with the upper surface of the mounting plate 1, the two supporting plates 402 are symmetrical with respect to the center point of the second rotating shaft 401, and the second rotating shaft 401 is located at the center of the rotating plate 301.
The second angle adjustment mechanism 4 still includes two third axis of rotation 403, the surface of two third axis of rotation 403 is all rotated and is connected with second U-shaped plate 404, the one side that two second U-shaped plates 404 kept away from each other is respectively with the one side fixed connection that rotating plate 301 and mounting panel 1 are close to each other, the surface of two third axis of rotation 403 is all fixedly connected with second rotating block 405, the electric telescopic handle 406 is installed to the surface mounting of one of them second rotating block 405, the flexible end of electric telescopic handle 406 and the surface fixed connection of another second rotating block 405, when the angle to the aviation part is adjusted, starter motor 304, motor 304 can drive first axis of rotation 302 rotation, first axis of rotation 302 rotation can drive first rotating block 305, circular plate 2, four-axis adjustment anchor clamps body 5 and aviation part swing along the left and right directions, start electric telescopic handle 406, second rotating block 405 and the second U-shaped plate 404 of top reciprocate, thereby can drive rotating plate 301 and second axis of rotation 401, in the rotating plate 301 pivoted in-process, second rotating block 405 and corresponding rotation axis of rotation 405 and three axis of rotation can drive the rotation of the corresponding circular plate 301 and the rotation of more than the rotation axis of rotation of a plurality of parts, thereby can carry out the angle adjustment of rotation of the aviation part 2, and the aviation part can be adjusted along the direction of rotation, and the aviation part is further adjusted.
Working principle: when the device is used, the device can be firstly arranged at a designated position through the mounting hole, then the aviation part can be fixed and rotated through the four-axis adjusting clamp body 5, when the angle of the aviation part is required to be adjusted, the motor 304 is started, the motor 304 can drive the first rotating shaft 302 to rotate, the first rotating shaft 302 can drive the first rotating block 305, the circular plate 2, the four-axis adjusting clamp body 5 and the aviation part to swing along the left-right direction, the electric telescopic rod 406 is started, the electric telescopic rod 406 can drive the second rotating block 405 above and the second U-shaped plate 404 above to move up and down, so that the rotating plate 301 and the second rotating shaft 401 can be driven to rotate, the second rotating block 405 and the third rotating shaft 403 can be correspondingly rotated in the rotating process of the rotating plate 301, the rotating plate 301 can drive the circular plate 2, the four-axis adjusting clamp body 5, the aviation part and the like to swing along the front-back direction, and the free adjustment of a plurality of angles can be carried out on the aviation part, and the processing efficiency of the aviation part can be greatly improved.
The foregoing description of the preferred embodiments of the utility model is not intended to limit the utility model to the precise form disclosed, and any such modifications, equivalents, and alternatives falling within the spirit and scope of the utility model are intended to be included within the scope of the utility model.
Claims (7)
1. The utility model provides a multi freedom four-axis adjustment anchor clamps of aviation part processing, includes mounting panel (1) and circular plate (2), its characterized in that: the circular plate (2) is located the top of mounting panel (1), the mounting hole has been seted up to the inside of mounting panel (1), the upper surface mounting of circular plate (2) has four-axis adjustment anchor clamps body (5), the below of circular plate (2) is provided with first angle adjustment mechanism (3), the top of mounting panel (1) is provided with second angle adjustment mechanism (4).
2. The four-axis adjusting clamp for machining aviation parts with multiple degrees of freedom according to claim 1, wherein: the first angle adjusting mechanism (3) comprises a rotating plate (301) and a first rotating shaft (302), wherein a first U-shaped plate (303) is rotatably connected to the outer surface of the first rotating shaft (302), and the bottom surface of the first U-shaped plate (303) is fixedly connected with the upper surface of the rotating plate (301).
3. The four-axis adjusting clamp for machining aviation parts with multiple degrees of freedom according to claim 2, wherein: the motor (304) is installed on the outer surface of the first U-shaped plate (303), and the output end of the motor (304) is fixedly connected with one end of the first rotating shaft (302).
4. The four-axis adjusting clamp for machining aviation parts with multiple degrees of freedom according to claim 2, wherein: the outer surface of the first rotating shaft (302) is fixedly connected with a first rotating block (305), and the upper surface of the first rotating block (305) is fixedly connected with the bottom surface of the circular plate (2).
5. The four-axis adjusting clamp for machining aviation parts with multiple degrees of freedom according to claim 2, wherein: the second angle adjusting mechanism (4) comprises a second rotating shaft (401), the outer surface of the second rotating shaft (401) is fixedly connected with the inner wall of the rotating plate (301), the outer surface of the second rotating shaft (401) is rotationally connected with two supporting plates (402), and the bottom surfaces of the two supporting plates (402) are fixedly connected with the upper surface of the mounting plate (1).
6. The four-axis adjusting clamp for machining aviation parts with multiple degrees of freedom according to claim 2, wherein: the second angle adjusting mechanism (4) further comprises two third rotating shafts (403), the outer surfaces of the two third rotating shafts (403) are rotationally connected with second U-shaped plates (404), and one faces, away from each other, of the two second U-shaped plates (404) are fixedly connected with one faces, close to each other, of the rotating plates (301) and the mounting plates (1) respectively.
7. The four-axis adjusting clamp with multiple degrees of freedom for machining aviation parts according to claim 6, wherein: the outer surfaces of the two third rotating shafts (403) are fixedly connected with second rotating blocks (405), one of the outer surfaces of the second rotating blocks (405) is provided with an electric telescopic rod (406), and the telescopic end of the electric telescopic rod (406) is fixedly connected with the outer surface of the other second rotating block (405).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320570753.0U CN219359283U (en) | 2023-03-22 | 2023-03-22 | Multi-degree-of-freedom four-axis adjusting clamp for machining aviation parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320570753.0U CN219359283U (en) | 2023-03-22 | 2023-03-22 | Multi-degree-of-freedom four-axis adjusting clamp for machining aviation parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219359283U true CN219359283U (en) | 2023-07-18 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320570753.0U Active CN219359283U (en) | 2023-03-22 | 2023-03-22 | Multi-degree-of-freedom four-axis adjusting clamp for machining aviation parts |
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| Country | Link |
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| CN (1) | CN219359283U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117400171A (en) * | 2023-10-16 | 2024-01-16 | 湖南中联重科智能高空作业机械有限公司 | Angle steel installation accessories |
| CN121061779A (en) * | 2025-11-06 | 2025-12-05 | 成都飞机工业(集团)有限责任公司 | U-shaped multi-degree-of-freedom clamping device and application method thereof |
-
2023
- 2023-03-22 CN CN202320570753.0U patent/CN219359283U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117400171A (en) * | 2023-10-16 | 2024-01-16 | 湖南中联重科智能高空作业机械有限公司 | Angle steel installation accessories |
| CN121061779A (en) * | 2025-11-06 | 2025-12-05 | 成都飞机工业(集团)有限责任公司 | U-shaped multi-degree-of-freedom clamping device and application method thereof |
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