CN211683682U - Aircraft parts machining mould fixing device - Google Patents
Aircraft parts machining mould fixing device Download PDFInfo
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- CN211683682U CN211683682U CN201922486763.2U CN201922486763U CN211683682U CN 211683682 U CN211683682 U CN 211683682U CN 201922486763 U CN201922486763 U CN 201922486763U CN 211683682 U CN211683682 U CN 211683682U
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Abstract
The utility model provides an aircraft parts machining mould fixing device, belongs to the fixed technical field of aircraft mould, including fixed clamp splice, stationary mast, step-up voltage board, enhancement lacing wire, fixed riser, activity spreader, activity ejector pad, its characterized in that: the fixed clamping block is characterized in that a fixed stand column is fixedly connected to the middle of the upper top end surface of the fixed clamping block, a pressure rising and reducing plate is inserted into the middle of the side top end surface of the fixed stand column, a reinforcing lacing wire is fixedly connected to the rear portion of the lower top end surface of the pressure rising and reducing plate, a fixed vertical plate is fixedly connected to the middle of the front edge of the upper top end surface of the fixed clamping block, a movable cross post is inserted into the middle of the rear top end surface of the fixed vertical plate, a movable pushing block is inserted into the front edge of the side top end surface of the movable cross post, a worker can push the mold tightly to the middle to prevent the mold from moving when the mold is compressed.
Description
The technical field is as follows:
the utility model belongs to the technical field of the fixed apparatus of aircraft mould, concretely relates to aircraft parts machining mould fixing device.
Background art:
in long-term work practice, when a worker fixes a die on a workbench for use, the existing fixer only compresses the die to move left and right and back easily during processing, and the dies with different heights need to be fixed by replacing the fixers with different heights, so that the worker is inconvenient to operate and use and the work efficiency is reduced.
The utility model has the following contents:
the utility model aims at: when fixing the mould on the workstation for solving the staff and using, the staff can push tightly the mould to centre department and prevent to remove when compressing tightly the mould to the staff can be at any time quick regulation clamp plate height, makes things convenient for the staff to operate and use and improves work efficiency, and its technical scheme is as follows:
the utility model provides an aircraft parts machining mould fixing device, it includes fixed clamp splice 1, fixed column 2, lift clamp plate 3, strengthens lacing wire 4, fixed riser 5, activity spreader 6, activity ejector pad 7, its characterized in that: the middle of the upper top end surface of the fixed clamping block 1 is fixedly connected with a fixed upright post 2, the middle of the side top end surface of the fixed upright post 2 is inserted with a pressure rising and reducing plate 3, the rear part of the lower top end surface of the pressure rising and reducing plate 3 is fixedly connected with a reinforcing lacing wire 4, the middle of the front edge of the upper top end surface of the fixed clamping block 1 is fixedly connected with a fixed vertical plate 5, the middle of the rear top end surface of the fixed vertical plate 5 is inserted with a movable cross post 6, the front edge of the side top end surface of the movable cross post 6 is inserted with a movable push block 7, the fixed upright post 2 comprises a support post 2-1, an external thread 2-2 and a nut 2-3, the top end surface of the support post 2-1 is provided with an external thread 2-2, the top end surface of the support post 2-1 is inserted with two nuts 2-3, and the, the movable transverse column 6 comprises an insert column 6-1, a clamping ring 6-2, a threaded column 6-3 and a nut 2-3, the clamping ring 6-2 is inserted in the center of the front top end surface of the insert column 6-1, the clamping ring 6-2 and the insert column 6-1 are connected with each other through a bearing, the threaded column 6-3 is fixedly connected in the center of the front top end surface of the clamping ring 6-2, the nut 2-3 is inserted in the top end surface of the threaded column 6-3, the insert column 6-1 is inserted in the fixed vertical plate 5, the movable push block 7 comprises an insert block 7-1, a through hole 7-2 and an insertion hole 7-3, the through hole 7-2 is arranged in the middle of the rear end surface of the insert block 7-1, the insertion hole 7-3 is arranged in the middle of the rear top end surface of the through hole 7-2, the jack 7-3 is inserted in the side surface of the threaded column 6-3, the front top end surface of the insertion block 7-1 is in an arc shape, the pressure rising and reducing plate 3 is in a Z shape, and the middle of the rear edge of the top end surface of the pressure rising and reducing plate 3 is inserted in the side surface of the support column 2-1.
The utility model has the advantages that: when fixing the mould on the workstation for solving the staff and using, the staff can push tightly the mould to centre department when compressing tightly the mould and prevent to remove to the staff can be at any time quick regulation clamp plate height, makes things convenient for the staff to operate and use and improves work efficiency.
Description of the drawings:
fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic structural view of the fixing column 2 of the present invention;
fig. 3 is a schematic structural view of the movable horizontal column 6 of the present invention;
fig. 4 is a schematic structural view of the movable push block 7 of the present invention.
The specific implementation mode is as follows:
refer to fig. 1 fig. 2 fig. 3 fig. 4 an aircraft parts machining mould fixing device, it includes fixed clamp splice 1, fixed stand 2, lift clamp plate 3, strengthens lacing wire 4, fixed riser 5, activity spreader 6, activity ejector pad 7, its characterized in that: the middle of the upper top end surface of the fixed clamping block 1 is fixedly connected with a fixed upright post 2, the middle of the side top end surface of the fixed upright post 2 is inserted with a pressure rising and reducing plate 3, the rear part of the lower top end surface of the pressure rising and reducing plate 3 is fixedly connected with a reinforcing lacing wire 4, the middle of the front edge of the upper top end surface of the fixed clamping block 1 is fixedly connected with a fixed vertical plate 5, the middle of the rear top end surface of the fixed vertical plate 5 is inserted with a movable cross post 6, the front edge of the side top end surface of the movable cross post 6 is inserted with a movable push block 7, the fixed upright post 2 comprises a support post 2-1, an external thread 2-2 and a nut 2-3, the top end surface of the support post 2-1 is provided with an external thread 2-2, the top end surface of the support post 2-1 is inserted with two nuts 2-3, and the, the movable transverse column 6 comprises an insert column 6-1, a clamping ring 6-2, a threaded column 6-3 and a nut 2-3, the clamping ring 6-2 is inserted in the center of the front top end surface of the insert column 6-1, the clamping ring 6-2 and the insert column 6-1 are connected with each other through a bearing, the threaded column 6-3 is fixedly connected in the center of the front top end surface of the clamping ring 6-2, the nut 2-3 is inserted in the top end surface of the threaded column 6-3, the insert column 6-1 is inserted in the fixed vertical plate 5, the movable push block 7 comprises an insert block 7-1, a through hole 7-2 and an insertion hole 7-3, the through hole 7-2 is arranged in the middle of the rear end surface of the insert block 7-1, the insertion hole 7-3 is arranged in the middle of the rear top end surface of the through hole 7-2, the jack 7-3 is inserted in the side surface of the threaded column 6-3, the front top end surface of the insertion block 7-1 is in an arc shape, the pressure rising and reducing plate 3 is in a Z shape, and the middle of the rear edge of the top end surface of the pressure rising and reducing plate 3 is inserted in the side surface of the support column 2-1.
When in use, firstly, the fixed clamping block 1 is inserted into a groove of a processing platform and is fixed on a working platform by using a bolt, then a nut 2-3 is inserted into a support 2-1 on the fixed upright post 2, then the lifting pressure plate 3 is inserted onto the support 2-1 and the height is adjusted, after the adjustment is finished, the nut 2-3 is rotated and clamped on the lower surface of the lifting pressure plate 3, then another nut is inserted into the support 2-1 and clamps the lifting pressure plate 3, then the jack 7-3 on the movable push block 7 is inserted onto the threaded post 6-3 on the movable sliding post 6, then the nut 2-3 is inserted into the through hole 7-2 and is inserted onto the threaded post 6-3 and simultaneously clamps the insert block 7-1 on the front surface of the clamp ring 6-2, then the insert post 6-1 is rotated to move on the fixed upright plate 5, meanwhile, the inserting column 6-1 rotates on the clamping ring 6-2, and finally the inserting block 7-1 clamps the die.
Of course, the above description is not intended to limit the present invention, and the present invention is not limited to the above examples, and the changes, modifications, additions or substitutions made by those skilled in the art within the scope of the present invention should also belong to the protection scope of the present invention.
Claims (5)
1. The utility model provides an aircraft parts machining mould fixing device, includes fixed clamp splice (1), fixed post (2), lift clamp plate (3), strengthens lacing wire (4), fixed riser (5), activity spreader (6), activity ejector pad (7), its characterized in that: the movable clamping block is characterized in that a fixed stand column (2) is fixedly connected to the middle of the upper top end surface of the fixed clamping block (1), a pressure rising and reducing plate (3) is inserted into the middle of the side top end surface of the fixed stand column (2), a reinforcing lacing wire (4) is fixedly connected to the rear portion of the lower top end surface of the pressure rising and reducing plate (3), a fixed vertical plate (5) is fixedly connected to the middle of the front edge of the upper top end surface of the fixed clamping block (1), a movable cross column (6) is inserted into the middle of the rear top end surface of the fixed vertical plate (5), and a movable push block (7) is inserted into the front edge of the side top end surface of the movable.
2. An aircraft parts machining die holding apparatus as claimed in claim 1, wherein: the fixed upright post (2) comprises a support post (2-1), external threads (2-2) and nuts (2-3), the external threads (2-2) are arranged on the top end surface of the side of the support post (2-1), the two nuts (2-3) are inserted into the top end surface of the side of the support post (2-1), and the external threads (2-2) are matched with the nuts (2-3).
3. An aircraft parts machining die holding apparatus as claimed in claim 2, wherein: the movable transverse column (6) comprises an inserting column (6-1), a clamping ring (6-2), a threaded column (6-3) and a nut (2-3), the clamping ring (6-2) is inserted in the center of a circle of a front top end surface of the inserting column (6-1), the clamping ring (6-2) and the inserting column (6-1) are connected with each other through a bearing, the threaded column (6-3) is fixedly connected to the center of a circle of the front top end surface of the clamping ring (6-2), the nut (2-3) is inserted in the side top end surface of the threaded column (6-3), and the inserting column (6-1) is inserted in the fixed vertical plate (5).
4. An aircraft parts machining die holding apparatus as claimed in claim 3, wherein: the movable push block (7) comprises an insert block (7-1), a through hole (7-2) and an insertion hole (7-3), the through hole (7-2) is formed in the middle of the rear edge of the top end surface of the insert block (7-1), the insertion hole (7-3) is formed in the middle of the top end surface of the rear portion inside the through hole (7-2), the insertion hole (7-3) is inserted in the side surface of the threaded column (6-3), and the front top end surface of the insert block (7-1) is in an arc shape.
5. An aircraft parts machining die holding apparatus as claimed in claim 2, wherein: the pressure rising and reducing plate (3) is Z-shaped, and the middle of the rear edge of the upper top end surface of the pressure rising and reducing plate (3) is inserted into the side surface of the strut (2-1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922486763.2U CN211683682U (en) | 2019-12-30 | 2019-12-30 | Aircraft parts machining mould fixing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922486763.2U CN211683682U (en) | 2019-12-30 | 2019-12-30 | Aircraft parts machining mould fixing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211683682U true CN211683682U (en) | 2020-10-16 |
Family
ID=72798039
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922486763.2U Active CN211683682U (en) | 2019-12-30 | 2019-12-30 | Aircraft parts machining mould fixing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211683682U (en) |
-
2019
- 2019-12-30 CN CN201922486763.2U patent/CN211683682U/en active Active
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