CN216180378U - Aircraft parts processing turning device - Google Patents
Aircraft parts processing turning device Download PDFInfo
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- CN216180378U CN216180378U CN202122366566.4U CN202122366566U CN216180378U CN 216180378 U CN216180378 U CN 216180378U CN 202122366566 U CN202122366566 U CN 202122366566U CN 216180378 U CN216180378 U CN 216180378U
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- plate
- workstation
- bottom plate
- turning device
- thread bush
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Abstract
The utility model relates to the technical field of machining and discloses an aircraft part machining turnover device which comprises a bottom plate and a workbench, wherein guide plates are fixedly arranged on the front side and the rear side of the top of the bottom plate, threaded columns are movably arranged in the two guide plates, threaded sleeves are connected to the surfaces of the two threaded columns in a threaded mode, and rotating plates are fixedly connected to the front side and the rear side of the bottom of the workbench. This aircraft spare part processing turning device, under the initial condition, the thread bush is located the rightmost end of screw thread post, the workstation is in the horizontality this moment, when needs overturn to table surface, it rotates to drive the screw thread post through the rotating electrical machines, make the thread bush slowly move to the left side under the effect of screw thread, the rotor plate rotates at the top of thread bush, it rotates to the right side to drive the workstation, the L shaped plate rotates left side on the diaphragm, the workstation ninety degrees that overturns just when the thread bush moves to the leftmost side, thereby make the device be convenient for overturn to the mesa of workstation.
Description
Technical Field
The utility model relates to the technical field of machining, in particular to an aircraft part machining turnover device.
Background
In the production manufacturing process of aircraft, need use some machining's workstation to process spare part, the mesa of some traditional workstations is most relatively more fixed, and sets up for the level for spare part can only be kept flat and process on the mesa, because the mesa is relatively fixed unable upset, consequently inconvenient edgewise processes spare part, can't satisfy the demand of multi-angle processing, we have proposed an aircraft spare part processing turning device for this reason.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Aiming at the defects of the prior art, the utility model provides the aircraft part processing and overturning device which has the advantages of overturning the table top of the workbench and facilitating the processing of the aircraft parts from the side surface, and solves the problems in the background art.
(II) technical scheme
The utility model provides the following technical scheme: the utility model provides an aircraft parts processing turning device, includes bottom plate and workstation, the side is all fixed to be equipped with the deflector, two around the bottom plate top the equal activity in inside of deflector is equipped with the screw thread post, two the surperficial threaded connection of screw thread post has the thread bush, the equal fixedly connected with rotor plate in side around the workstation bottom, the bottom of rotor plate is articulated with the top of thread bush, one side fixedly connected with diaphragm at bottom plate top, the side all articulates around the diaphragm has the L shaped plate, the one side of keeping away from the diaphragm of L shaped plate is articulated with the side of workstation, the top fixed mounting of bottom plate has the rotating electrical machines.
Furthermore, the inside of deflector is seted up flutedly, the screw thread post is connected with the inside rotation of recess, and the screw thread post can make the screw thread cover remove about the inside of recess through the effect of screw when the inside of recess rotates, can lead to spacingly through the removal of recess to the screw thread cover.
Further, the bottom plate is fixedly provided with a vertical plate, one end of the threaded column penetrates through the vertical plate and is rotatably connected with the inside of the vertical plate, the end of the threaded column can be limited through the action of the vertical plate, and the threaded column can be rotated inside the vertical plate.
Further, the fixed belt pulley that is equipped with of output of rotating electrical machines, the belt pulley passes the one end of riser through belt and two screw thread posts and is connected, can drive two screw thread posts through the belt and rotate simultaneously when rotating electrical machines rotates.
Furthermore, one side of riser is fixed and is equipped with the spacing ring, one side of spacing ring is equipped with cushion rubber, through cushion rubber's effect, when the thread bush to the left side removal and with the spacing ring contact, cushions the protection to the left side of thread bush.
Compared with the prior art, the utility model provides an aircraft part processing and overturning device, which has the following beneficial effects:
1. this aircraft spare part processing turning device, under the initial condition, the thread bush is located the rightmost end of screw thread post, the workstation is in the horizontality this moment, when needs overturn to table surface, it rotates to drive the screw thread post through the rotating electrical machines, make the thread bush slowly move to the left side under the effect of screw thread, the rotor plate rotates at the top of thread bush, it rotates to the right side to drive the workstation, the L shaped plate rotates left side on the diaphragm, the workstation ninety degrees that overturns just when the thread bush moves to the leftmost side, thereby make the device be convenient for overturn to the mesa of workstation.
2. This aircraft parts processing turning device, then through being provided with the spacing ring, the spacing ring is provided with cushion rubber with the junction of riser, is convenient for carry out spacing buffering to the left side of thread bush through spacing ring and cushion rubber's effect, can contact with the spacing ring and produce the extrusion to it when the thread bush moves the left side of screw thread post for cushion rubber takes place to deform, carries out the buffer protection to the left side of thread bush under cushion rubber's spring action.
Drawings
FIG. 1 is a cross-sectional view of the structure of the present invention;
FIG. 2 is a top view of the base plate structure of the present invention;
FIG. 3 is a schematic view of the structure of the working table of the present invention;
FIG. 4 is an enlarged view of the structure of FIG. 1A according to the present invention.
Wherein: 1. a base plate; 2. a guide plate; 3. a groove; 4. a threaded post; 5. a threaded sleeve; 6. a work table; 7. a rotating plate; 8. a transverse plate; 9. an L-shaped plate; 10. a rotating electric machine; 11. a vertical plate; 12. a limiting ring; 13. and (3) buffer rubber.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-4, an aircraft part processing and turning device comprises a bottom plate 1 and a workbench 6, wherein guide plates 2 are fixedly arranged on the front side and the rear side of the top of the bottom plate 1, threaded columns 4 are movably arranged inside the two guide plates 2, grooves 3 are formed inside the guide plates 2, the threaded columns 4 are rotatably connected with the insides of the grooves 3, the grooves 3 are strip-shaped grooves, the threaded columns 4 can rotate inside the grooves 3, threaded sleeves 5 are connected with the surfaces of the two threaded columns 4 in a threaded manner, rotating plates 7 are fixedly connected with the front side and the rear side of the bottom of the workbench 6, the bottom of the rotating plate 7 is hinged with the top of the threaded sleeves 5, a transverse plate 8 is fixedly connected with one side of the top of the bottom plate 1, an L-shaped plate 9 is hinged with the front side and the rear side of the transverse plate 8, one side of the L-shaped plate 9, which is far away from the transverse plate 8, is hinged with the side of the workbench 6, and a rotating motor 10 is fixedly arranged on the top of the bottom plate 1, the rotary motor 10 is a servo motor, and can drive the two threaded columns 4 to rotate simultaneously by controlling the forward and reverse rotation of the servo motor, so as to drive the workbench 6 to overturn or fall back to the horizontal state.
Fixed riser 11 that is equipped with on bottom plate 1, the one end of screw thread post 4 is passed riser 11 and is connected with the inside rotation of riser 11, the fixed belt pulley that is equipped with of output of rotating electrical machines 10, the belt pulley passes through the belt and is connected with the one end that two screw thread posts 4 passed riser 11, the one end that screw thread post 4 passed riser 11 is provided with the belt lace wheel, connect through the belt between belt pulley and the belt lace wheel, the belt pulley that drives earlier when making rotating electrical machines 10 rotate rotates, rethread belt drives two belt lace wheel rotations, and then can drive two screw thread posts 4 simultaneously and rotate.
A limiting ring 12 is fixedly arranged on one side of the vertical plate 11, buffer rubber 13 is arranged on one side of the limiting ring 12, the buffer rubber 13 is located between the limiting ring 12 and the vertical plate 11, and the left side of the threaded sleeve 5 is conveniently buffered and protected through the effect of the buffer rubber.
When using, when needs overturn 6 faces of workstation, drive screw thread post 4 through rotating electrical machines 10 and rotate, make the thread bush 5 slowly move to the left side under the effect of screw thread, rotor plate 7 rotates at the top of thread bush 5, drive workstation 6 and rotate to the right side, L shaped plate 9 rotates to the left side on diaphragm 8, workstation 6 overturns ninety degrees just when thread bush 5 moves to the leftmost side, thereby make the device be convenient for overturn 6's mesa, when needs workstation 6 is in the horizontality, only need control rotating electrical machines 10 antiport can.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides an aircraft spare part processing turning device, includes bottom plate (1) and workstation (6), its characterized in that: the utility model discloses a novel rotary table, including bottom plate (1), bottom plate (1) top, bottom plate (1) front and back side all fixed deflector (2), two the equal activity in inside of deflector (2) is equipped with threaded column (4), two the surperficial threaded connection of threaded column (4) has thread bush (5), the equal fixedly connected with rotor plate (7) in side around workstation (6) bottom, the bottom of rotor plate (7) is articulated with the top of thread bush (5), one side fixedly connected with diaphragm (8) at bottom plate (1) top, the side all articulates around diaphragm (8) has L shaped plate (9), the one side of keeping away from diaphragm (8) of L shaped plate (9) is articulated with the side of workstation (6), the top fixed mounting of bottom plate (1) has rotating electrical machines (10).
2. The aircraft component processing turning device of claim 1, wherein: the guide plate (2) is internally provided with a groove (3), and the threaded column (4) is rotatably connected with the inside of the groove (3).
3. The aircraft component processing turning device of claim 1, wherein: the bottom plate (1) is fixedly provided with a vertical plate (11), and one end of the threaded column (4) penetrates through the vertical plate (11) and is rotatably connected with the inside of the vertical plate (11).
4. The aircraft component processing turning device of claim 3, wherein: the output end of the rotating motor (10) is fixedly provided with a belt pulley, and the belt pulley is connected with one end of the two threaded columns (4) penetrating through the vertical plate (11) through a belt.
5. The aircraft component processing turning device of claim 3, wherein: a limiting ring (12) is fixedly arranged on one side of the vertical plate (11), and buffer rubber (13) is arranged on one side of the limiting ring (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122366566.4U CN216180378U (en) | 2021-09-29 | 2021-09-29 | Aircraft parts processing turning device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122366566.4U CN216180378U (en) | 2021-09-29 | 2021-09-29 | Aircraft parts processing turning device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216180378U true CN216180378U (en) | 2022-04-05 |
Family
ID=80927103
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122366566.4U Active CN216180378U (en) | 2021-09-29 | 2021-09-29 | Aircraft parts processing turning device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216180378U (en) |
-
2021
- 2021-09-29 CN CN202122366566.4U patent/CN216180378U/en active Active
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