CN204524873U - A kind of tool mechanism of medium-sized aviation arc plate Multi-axis Machining - Google Patents
A kind of tool mechanism of medium-sized aviation arc plate Multi-axis Machining Download PDFInfo
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- CN204524873U CN204524873U CN201420850584.7U CN201420850584U CN204524873U CN 204524873 U CN204524873 U CN 204524873U CN 201420850584 U CN201420850584 U CN 201420850584U CN 204524873 U CN204524873 U CN 204524873U
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- frame
- oblique pull
- arc plate
- bottom bracing
- fixedly connected
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Abstract
The purpose of this utility model is to provide a kind of tool mechanism of medium-sized aviation arc plate Multi-axis Machining.The technical solution of the utility model is: be made up of middle oblique pull frame, limit oblique pull frame, diagonal brace frame, middle support frame, bottom bracing frame, bearing diagonal framework, middle support frame and oblique pull crossbeam.This mechanism is by arc plate as in frock, and being distributed in arc panel area has screwed hole for clamping, is compressed by arc plate with pad and bolt, after installing, go up horizontal Machining centers together, make datum plate and bed surface sturdy, briquetting compression tooling, realizes the Multi-axis Machining of arc plate by the method.This mechanism designs for the Multi-axis Machining of medium-sized avigation piece, in the processing of polyhedron (as cambered surface), utilizes this frock can realize the Multi-axis Machining of arc plate, also can reduce the distortion that arc plate work in-process causes, greatly enhance productivity.Whole frock is that assembly welding forms, and bottom surface is by six pieces of coplanar reference blocks, and side milling becomes cambered surface that arc plate can be fitted, and is convenient to clamping, realizes the processing of multiaxis cambered surface.
Description
Technical field
The utility model relates to machinery manufacturing technology field, particularly relates to a kind of tool mechanism of medium-sized aviation arc plate Multi-axis Machining.
Background technology
To produce and in manufacturing industry, the processing of arc plate is the central important link of production in modern aerospace.Processing in the past for arc plate is all adopt single process technique, proceeds to next process, so, waste a large amount of time costs and human cost after namely completing a procedure.This tool mechanism is by arc plate as in frock, and frock being distributed in arc panel area has screwed hole for clamping, is compressed by arc plate with pad and bolt, after installing, go up horizontal Machining centers together, make datum plate and bed surface sturdy, briquetting compression tooling, realizes the Multi-axis Machining of arc plate by the method.This mechanism designs for the Multi-axis Machining of medium-sized avigation piece, in the processing of polyhedron (as cambered surface), utilizes this frock can realize the Multi-axis Machining of arc plate, also can reduce the distortion that arc plate work in-process causes, greatly enhance productivity.Whole frock is formed by each part assembly welding, and bottom surface is by six pieces of coplanar reference blocks, and side milling becomes cambered surface that arc plate can be fitted, and is convenient to clamping, thus realizes the processing of multiaxis cambered surface.
Utility model content
The purpose of this utility model is to provide a kind of tool mechanism of medium-sized aviation arc plate Multi-axis Machining.
The technical solution of the utility model is: a kind of tool mechanism of medium-sized aviation arc plate Multi-axis Machining, it is characterized in that: by oblique pull frame in several, several limit oblique pull framves, several diagonal brace frames, middle support frame, bottom bracing frame, several bearing diagonal frameworks, support frame and several oblique pull crossbeams composition in several, any described middle oblique pull chord position is in the side of bottom bracing frame, described middle oblique pull frame with bottom bracing frame for being fixedly connected with, the parallel side being arranged in oblique pull frame of oblique pull frame, any described limit, described limit oblique pull frame with bottom bracing frame for being fixedly connected with, any described bearing diagonal framework is positioned at one end of bottom bracing frame, described bearing diagonal framework and bottom bracing frame are for being fixedly connected with, any described middle support frame is positioned at the top of bottom bracing frame, described middle support frame and bottom bracing frame are for being fixedly connected with, any described diagonal brace frame is positioned at the top of bottom bracing frame, described diagonal brace frame and bearing diagonal framework with middle support frame for being fixedly connected with, described middle support frame is positioned at the top of bottom bracing frame, described middle support frame and middle support frame are for being fixedly connected with, any described oblique pull crossbeam is positioned at one end of bottom bracing frame, described oblique pull crossbeam and diagonal brace frame are for being fixedly connected with, described oblique pull crossbeam is also provided with radian reference block, described radian reference block is positioned at the side of oblique pull crossbeam, described radian reference block and oblique pull crossbeam are for being fixedly connected with, described diagonal brace frame is also provided with fixed block, oblique pull fixed cross beam and the main fixed cross beam of oblique pull, described fixed block is positioned at the top of diagonal brace frame, described fixed block and diagonal brace frame are for being fixedly connected with, the parallel side being positioned at fixed block of described oblique pull fixed cross beam, described oblique pull fixed cross beam and diagonal brace frame are for being fixedly connected with, the parallel opposite side being positioned at fixed block of the main fixed cross beam of described oblique pull, the main fixed cross beam of described oblique pull and diagonal brace frame are for being fixedly connected with, described middle support frame is also provided with middle reference block, described middle reference block is arranged in the top of support frame, described middle reference block and middle support frame are for being fixedly connected with, described bottom bracing frame is also provided with fixed head, described fixed head is positioned at the side of bottom bracing frame, described fixed head and bottom bracing frame are for being fixedly connected with.
Further, described in several number of oblique pull frame be 2.
Further, the number of several limit oblique pull framves described is 2.
Further again, the angle of described limit oblique pull frame and bearing diagonal framework is 26 °.
Further, the number of several diagonal brace frames described is 4.
Further again, the angle of described diagonal brace frame and bearing diagonal framework is 90 °.
Further, the number of several bearing diagonal frameworks described is 2.
Further again, the angle of described bearing diagonal framework and bottom bracing frame is 109 °.
Further, described in several number of support frame be 2.
Further, the number of several oblique pull crossbeams described is 4.
The beneficial effects of the utility model are: this tool mechanism by arc plate as in frock, frock is distributed in arc panel area and has screwed hole for clamping, with pad and bolt, arc plate is compressed, after installing, go up horizontal Machining centers together, make datum plate and bed surface sturdy, briquetting compression tooling, realizes the Multi-axis Machining of arc plate by the method.This mechanism designs for the Multi-axis Machining of medium-sized avigation piece, in the processing of polyhedron (as cambered surface), utilizes this frock can realize the Multi-axis Machining of arc plate, also can reduce the distortion that arc plate work in-process causes, greatly enhance productivity.Whole frock is formed by each part assembly welding, and bottom surface is by six pieces of coplanar reference blocks, and side milling becomes cambered surface that arc plate can be fitted, and is convenient to clamping, thus realizes the processing of multiaxis cambered surface.
Accompanying drawing explanation
Fig. 1 is front view of the present utility model.
Fig. 2 is top view of the present utility model.
Fig. 3 is side view of the present utility model.
Fig. 4 is secondary side view of the present utility model.
Wherein: 1, radian reference block 2, middle oblique pull frame 3, limit oblique pull frame
4, diagonal brace frame 5, middle support frame 6, bottom bracing frame
7, bearing diagonal framework 8, middle support frame 9, oblique pull crossbeam
10, middle reference block 11, fixed head 12, fixed block
13, oblique pull fixed cross beam 14, the main fixed cross beam of oblique pull
Detailed description of the invention
Below in conjunction with accompanying drawing, brief description is made to detailed description of the invention of the present utility model.
A kind of tool mechanism of medium-sized aviation arc plate Multi-axis Machining as shown in Figure 1, it is characterized in that: by oblique pull frame 2 in several, several limit oblique pull framves 3, several diagonal brace frames 4, middle support frame 5, bottom bracing frame 6, several bearing diagonal frameworks 7, in several, support frame 8 and several oblique pull crossbeams 9 form, any described middle oblique pull frame 2 is positioned at the side of bottom bracing frame 6, described middle oblique pull frame 2 with bottom bracing frame 6 for being fixedly connected with, the parallel side being arranged in oblique pull frame 2 of oblique pull frame 3, any described limit, described limit oblique pull frame 3 with bottom bracing frame 6 for being fixedly connected with, any described bearing diagonal framework 7 is positioned at one end of bottom bracing frame 6, described bearing diagonal framework 7 and bottom bracing frame 6 are for being fixedly connected with, any described middle support frame 8 is positioned at the top of bottom bracing frame 6, described middle support frame 8 and bottom bracing frame 6 are for being fixedly connected with, any described diagonal brace frame 4 is positioned at the top of bottom bracing frame 6, described diagonal brace frame 4 and bearing diagonal framework 7 with middle support frame 8 for being fixedly connected with, described middle support frame 5 is positioned at the top of bottom bracing frame 6, described middle support frame 5 and middle support frame 8 are for being fixedly connected with, any described oblique pull crossbeam 9 is positioned at one end of bottom bracing frame 6, described oblique pull crossbeam 9 and diagonal brace frame 4 are for being fixedly connected with, described oblique pull crossbeam 9 is also provided with radian reference block 1, described radian reference block 1 is positioned at the side of oblique pull crossbeam 9, described radian reference block 1 and oblique pull crossbeam 9 are for being fixedly connected with, described diagonal brace frame 4 is also provided with fixed block 12, oblique pull fixed cross beam 13 and the main fixed cross beam 14 of oblique pull, described fixed block 12 is positioned at the top of diagonal brace frame 4, described fixed block 12 and diagonal brace frame 4 are for being fixedly connected with, the parallel side being positioned at fixed block 12 of described oblique pull fixed cross beam 13, described oblique pull fixed cross beam 13 and diagonal brace frame 4 are for being fixedly connected with, the parallel opposite side being positioned at fixed block 12 of the main fixed cross beam of described oblique pull 14, the main fixed cross beam 14 of described oblique pull with diagonal brace frame 4 for being fixedly connected with, described middle support frame 5 is also provided with middle reference block 10, described middle reference block 10 is arranged in the top of support frame 5, described middle reference block 10 and middle support frame 5 are for being fixedly connected with, described bottom bracing frame 6 is also provided with fixed head 11, described fixed head 11 is positioned at the side of bottom bracing frame 6, described fixed head 11 and bottom bracing frame 6 are for being fixedly connected with.Described in several number of oblique pull frame 2 be 2.The number of several limit oblique pull framves 3 described is 2.The number of several diagonal brace frames 4 described is 4.The number of several bearing diagonal frameworks 7 described is 2.Described in several number of support frame 8 be 2.The number of several oblique pull crossbeams 9 described is 4.Described limit oblique pull frame 3 is 26 ° with the angle of bearing diagonal framework 7.Described diagonal brace frame 4 is 90 ° with the angle of bearing diagonal framework 7.Described bearing diagonal framework 7 is 109 ° with the angle of bottom bracing frame 6.
Working method: this tool mechanism main composition is made up of two middle oblique pull framves, two limit oblique pull framves, 3, four diagonal brace frames 4, middle support frame 5, bottom bracing frame 6, two bearing diagonal frameworks 7, two middle support frames 8 and four oblique pull crossbeams 9, by arc plate as in frock, frock is distributed in arc panel area and has screwed hole for clamping, with pad and bolt, arc plate is compressed, after installing, go up horizontal Machining centers together, make datum plate and bed surface sturdy, briquetting compression tooling, realizes the Multi-axis Machining of arc plate by the method.This mechanism designs for the Multi-axis Machining of medium-sized avigation piece, in the processing of polyhedron (as cambered surface), utilizes this frock can realize the Multi-axis Machining of arc plate, also can reduce the distortion that arc plate work in-process causes, greatly enhance productivity.Whole frock is formed by each part assembly welding, and bottom surface is by six pieces of coplanar reference blocks, and side milling becomes cambered surface that arc plate can be fitted, and is convenient to clamping, thus realizes the processing of multiaxis cambered surface.
Above an embodiment of the present utility model has been described in detail, but described content being only preferred embodiment of the present utility model, can not being considered to for limiting practical range of the present utility model.All equalizations done according to the utility model application range change and improve, and all should still belong within patent covering scope of the present utility model.
Claims (10)
1. the tool mechanism of one kind medium-sized aviation arc plate Multi-axis Machining, it is characterized in that: by oblique pull frame in several, several limit oblique pull framves, several diagonal brace frames, middle support frame, bottom bracing frame, several bearing diagonal frameworks, support frame and several oblique pull crossbeams composition in several, any described middle oblique pull chord position is in the side of bottom bracing frame, described middle oblique pull frame with bottom bracing frame for being fixedly connected with, the parallel side being arranged in oblique pull frame of oblique pull frame, any described limit, described limit oblique pull frame with bottom bracing frame for being fixedly connected with, any described bearing diagonal framework is positioned at one end of bottom bracing frame, described bearing diagonal framework and bottom bracing frame are for being fixedly connected with, any described middle support frame is positioned at the top of bottom bracing frame, described middle support frame and bottom bracing frame are for being fixedly connected with, any described diagonal brace frame is positioned at the top of bottom bracing frame, described diagonal brace frame and bearing diagonal framework with middle support frame for being fixedly connected with, described middle support frame is positioned at the top of bottom bracing frame, described middle support frame and middle support frame are for being fixedly connected with, any described oblique pull crossbeam is positioned at one end of bottom bracing frame, described oblique pull crossbeam and diagonal brace frame are for being fixedly connected with, described oblique pull crossbeam is also provided with radian reference block, described radian reference block is positioned at the side of oblique pull crossbeam, described radian reference block and oblique pull crossbeam are for being fixedly connected with, described diagonal brace frame is also provided with fixed block, oblique pull fixed cross beam and the main fixed cross beam of oblique pull, described fixed block is positioned at the top of diagonal brace frame, described fixed block and diagonal brace frame are for being fixedly connected with, the parallel side being positioned at fixed block of described oblique pull fixed cross beam, described oblique pull fixed cross beam and diagonal brace frame are for being fixedly connected with, the parallel opposite side being positioned at fixed block of the main fixed cross beam of described oblique pull, the main fixed cross beam of described oblique pull and diagonal brace frame are for being fixedly connected with, described middle support frame is also provided with middle reference block, described middle reference block is arranged in the top of support frame, described middle reference block and middle support frame are for being fixedly connected with, described bottom bracing frame is also provided with fixed head, described fixed head is positioned at the side of bottom bracing frame, described fixed head and bottom bracing frame are for being fixedly connected with.
2. the tool mechanism of a kind of medium-sized aviation arc plate Multi-axis Machining according to claim 1, is characterized in that: described in several number of oblique pull frame be 2.
3. the tool mechanism of a kind of medium-sized aviation arc plate Multi-axis Machining according to claim 1, is characterized in that: the number of several limit oblique pull framves described is 2.
4. the tool mechanism of a kind of medium-sized aviation arc plate Multi-axis Machining according to claim 1, is characterized in that: the angle of described limit oblique pull frame and bearing diagonal framework is 26 °.
5. the tool mechanism of a kind of medium-sized aviation arc plate Multi-axis Machining according to claim 1, is characterized in that: the number of several diagonal brace frames described is 4.
6. the tool mechanism of a kind of medium-sized aviation arc plate Multi-axis Machining according to claim 1, is characterized in that: the angle of described diagonal brace frame and bearing diagonal framework is 90 °.
7. the tool mechanism of a kind of medium-sized aviation arc plate Multi-axis Machining according to claim 1, is characterized in that: the number of several bearing diagonal frameworks described is 2.
8. the tool mechanism of a kind of medium-sized aviation arc plate Multi-axis Machining according to claim 1, is characterized in that: the angle of described bearing diagonal framework and bottom bracing frame is 109 °.
9. the tool mechanism of a kind of medium-sized aviation arc plate Multi-axis Machining according to claim 1, is characterized in that: described in several number of support frame be 2.
10. the tool mechanism of a kind of medium-sized aviation arc plate Multi-axis Machining according to claim 1, is characterized in that: the number of several oblique pull crossbeams described is 4.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420850584.7U CN204524873U (en) | 2014-12-29 | 2014-12-29 | A kind of tool mechanism of medium-sized aviation arc plate Multi-axis Machining |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420850584.7U CN204524873U (en) | 2014-12-29 | 2014-12-29 | A kind of tool mechanism of medium-sized aviation arc plate Multi-axis Machining |
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| Publication Number | Publication Date |
|---|---|
| CN204524873U true CN204524873U (en) | 2015-08-05 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420850584.7U Expired - Fee Related CN204524873U (en) | 2014-12-29 | 2014-12-29 | A kind of tool mechanism of medium-sized aviation arc plate Multi-axis Machining |
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| Country | Link |
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| CN (1) | CN204524873U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104526410A (en) * | 2014-12-29 | 2015-04-22 | 天津市华天世纪机械有限公司 | Tool mechanism for conducting multi-axis machining on middle-sized aviation arc plates |
-
2014
- 2014-12-29 CN CN201420850584.7U patent/CN204524873U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104526410A (en) * | 2014-12-29 | 2015-04-22 | 天津市华天世纪机械有限公司 | Tool mechanism for conducting multi-axis machining on middle-sized aviation arc plates |
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| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150805 Termination date: 20161229 |
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| CF01 | Termination of patent right due to non-payment of annual fee |