CN223369141U - Aviation tire sidewall processing jig - Google Patents
Aviation tire sidewall processing jigInfo
- Publication number
- CN223369141U CN223369141U CN202422283779.4U CN202422283779U CN223369141U CN 223369141 U CN223369141 U CN 223369141U CN 202422283779 U CN202422283779 U CN 202422283779U CN 223369141 U CN223369141 U CN 223369141U
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- CN
- China
- Prior art keywords
- fixedly arranged
- driving motor
- transverse frame
- side wall
- aviation
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Abstract
The utility model relates to the technical field of tire polishing equipment, in particular to an aviation tire sidewall processing jig which comprises a base, wherein an upright post is fixedly arranged on the left side of the top wall of the base, a fixed disc is rotationally arranged on the right side wall of the upright post, a connecting seat is fixedly arranged on the right side wall of the fixed disc, a first transverse frame and a second transverse frame are fixedly arranged on the right side wall of the connecting seat up and down, the first transverse frame is positioned on the upper side of the second transverse frame, the aviation tire can be more conveniently fixed and detached, the aviation tires with different sizes can be better processed through the arrangement of a moving assembly, an adjusting assembly and a polishing assembly, and the transmission effect of polished fragments affecting a screw rod can be well avoided through the movement of the moving post in a slide hole, so that the structure is more durable.
Description
Technical Field
The utility model relates to the technical field of tire polishing equipment, in particular to an aviation tire sidewall processing jig.
Background
In the prior art, chinese patent application publication No. CN218746605U, for example, discloses a device for processing the sidewall of an aviation tire, belonging to the technical field of tire polishing devices. The aviation tire sidewall processing equipment comprises a base box table, wherein a bidirectional threaded rod is rotationally connected between inner walls of two sides of the base box table, two transmission blocks are slidably connected to the upper inner wall of the base box table, mounting plates are fixedly connected to the upper outer surfaces of the two transmission blocks, polishing heads are rotationally connected to the outer surfaces of one sides of each mounting plate, the bidirectional threaded rod is rotated to drive the two transmission blocks to be close to each other, the two mounting plates drive the two polishing heads to be attached to two sides of an aviation tire, the aviation tire polishing work with different widths is adapted, lifting plates are driven to move up and down through rotation of lifting threaded rods, so that the portions of the tire to be polished are aligned with the two polishing heads, the aviation tire polishing work with different diameters is adapted, the aviation tire manufacturing polishing equipment with different sizes is not required, and the production cost is saved.
However, when the above-mentioned open structure is in use, the disassembly of the aircraft tire is inconvenient, so time is wasted, and impurities are accumulated easily at the threaded rod to influence mechanical transmission.
Disclosure of utility model
(One) solving the technical problems
Aiming at the defects of the prior art, the utility model provides an aviation tire sidewall processing jig.
(II) technical scheme
The aviation tire sidewall machining jig comprises a base, wherein an upright post is fixedly arranged on the left side of the top wall of the base, a first fixed disk is rotatably arranged on the right side wall of the upright post, a connecting seat is fixedly arranged on the right side wall of the first fixed disk, a first transverse frame and a second transverse frame are fixedly arranged on the right side wall of the connecting seat up and down, the first transverse frame is positioned on the upper side of the second transverse frame, a first hydraulic cylinder is fixedly arranged on the top wall of the first transverse frame, an output end of the first hydraulic cylinder penetrates through the first transverse frame and is rotatably provided with a second fixed disk, a second driving motor is fixedly arranged on the lower side wall of the second transverse frame and is rotatably provided with a third fixed disk corresponding to the first driving motor, an output end of the second driving motor is connected with the third fixed disk, a positioning component is further arranged on the third fixed disk, a moving component is arranged on the rear side of the base, and an adjusting component is arranged on the moving component.
In order to facilitate the transverse adjustment of the position of the polishing assembly, the improvement of the utility model comprises a driving motor III, a moving column, a screw rod, a vertical beam and a cross beam, wherein a sliding hole is formed in the rear side of the base, the screw rod is rotatably arranged in the sliding hole, the moving column is slidably arranged in the sliding hole, the moving column is in threaded connection with the screw rod, the driving motor III is fixedly arranged at the position of the front side wall of the base corresponding to the screw rod, the three output end of the driving motor is connected with the screw rod, the vertical beam is fixedly arranged on the right side of the top wall of the moving column, and the cross beam is fixedly arranged on the top wall of the vertical beam.
In order to facilitate longitudinal adjustment of the position of the polishing component, the improvement of the utility model comprises that the adjusting component comprises a second hydraulic cylinder, the left side of the top wall of the cross beam is fixedly provided with the second hydraulic cylinder, the output end of the second hydraulic cylinder is fixedly provided with a U-shaped frame, and the U-shaped frame is provided with the polishing component.
Preferably, the utility model further comprises a sliding rail and a limiting beam, wherein the limiting beam is fixedly arranged on the bottom wall of the U-shaped frame, the sliding rail is fixedly arranged at the position, corresponding to the limiting beam, of the top wall of the cross beam, and the sliding rail is in sliding connection with the limiting beam.
In order to facilitate machining of the side of the aviation tire, the improvement of the utility model is that the grinding assembly comprises a driving motor IV and a grinding wheel, the grinding wheel is rotationally arranged in the U-shaped frame, the driving motor IV is fixedly arranged on the outer wall of one side of the U-shaped frame, and the output end of the driving motor IV is connected with the grinding wheel.
In order to facilitate positioning of the aircraft tire, the improved positioning assembly comprises positioning columns, and a plurality of groups of positioning columns are fixedly arranged on the three top walls of the fixed disc.
Preferably, the improvement of the utility model further comprises a positioning groove, wherein a plurality of groups of positioning grooves are formed in the lower side wall of the second fixed disc, and the positioning columns are matched with the positioning grooves.
(III) beneficial effects
Compared with the prior art, the utility model provides an aviation tire sidewall processing jig, which has the following beneficial effects:
This aircraft tire side wall processing tool, can be more convenient fix and dismantle aircraft tire, through the setting of moving subassembly, adjusting part and polishing subassembly, the aircraft tire of equidimension not that can be better is processed, through moving the post and moving in the slide opening, the piece that has avoided polishing that can be fine influences the transmission effect of screw rod, makes this structure more durable.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic view of the structure of FIG. 1 according to another embodiment of the present utility model;
FIG. 3 is a schematic view of the structure of FIG. 2 from another perspective in accordance with the present utility model;
Fig. 4 is a schematic cross-sectional view of a partial structure of the present utility model.
The device comprises a base, a column, a fixed plate I, a driving motor I, a connecting seat I, a driving motor 5, a connecting seat I, a vertical frame I, a transverse frame II, a hydraulic cylinder I, a fixing plate II, a driving motor II, a fixing plate III, a fixing column 13, a positioning column 14, a driving motor III, a driving column 15, a moving column 16, a vertical beam 17, a cross beam 18, a hydraulic cylinder II, a driving motor 19, a U-shaped frame 20, a driving motor IV, a grinding wheel 21, a sliding rail 22, a limiting beam 23, a limiting beam 24 and a screw.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-4, an aircraft tire sidewall processing jig comprises a base 1, a column 2 is fixedly arranged on the left side of the top wall of the base 1, a fixed disk I3 is rotatably arranged on the right side wall of the column 2, a connecting seat 5 is fixedly arranged on the right side wall of the fixed disk I3, a transverse frame I7 and a transverse frame II 8 are fixedly arranged on the right side wall of the connecting seat 5 up and down, the transverse frame I7 is positioned on the upper side of the transverse frame II 8, a hydraulic cylinder I9 is fixedly arranged on the top wall of the transverse frame I7, the output end of the hydraulic cylinder I9 penetrates through the transverse frame I7 and is rotatably provided with a fixed disk II 10, a driving motor II 11 is fixedly arranged on the lower side wall of the transverse frame II 8 corresponding to the hydraulic cylinder I9, a fixed disk III 12 is rotatably arranged on the upper side wall of the transverse frame II 8 corresponding to the driving motor II 11, the output end of the driving motor II 11 is connected with the fixed disk III 12, a positioning component is further arranged on the fixed disk III 12, a moving component is arranged on the rear side of the base 1, the movable component is provided with an adjusting component, the adjusting component is provided with a polishing component, the aircraft tire is placed between the third fixed disk 12 and the second fixed disk 10, the first hydraulic cylinder 9 controls the second fixed disk 10 to descend and the third fixed disk 12 to mutually cooperate to clamp and fix the aircraft tire, the aircraft tire is positioned through the fixing component, the second driving motor 11 drives the aircraft tire to rotate, the aircraft tire side is polished through the polishing component, the transverse position of the polishing component can be adjusted through the movable component, the longitudinal position of the polishing component can be adjusted through the adjusting component, thereby the aircraft tire side with different sizes can be polished, the first driving motor 4 rotates the first fixed disk 3, thereby the connecting seat 5 and the vertical frame 6 can be rotated, the direction of the aircraft tire can be further adjusted, thereby can process the opposite side, this structure can be more convenient fix and dismantle aircraft tire, through the setting of moving assembly, adjusting part and polishing assembly, can be better process the aircraft tire of equidimension not, move in the sliding hole through the movable column 15, the piece that has avoided polishing that can be fine influences the transmission effect of screw rod 24, makes this structure more durable.
Referring to fig. 2-3, the above-mentioned moving assembly may be any one, and the present application provides an embodiment, where the moving assembly includes a third driving motor 14, a moving post 15, a screw 24, a vertical beam 16, and a cross beam 17, a sliding hole is provided at the rear side of the base 1, the screw 24 is rotatably provided in the sliding hole, the moving post 15 is slidably provided in the sliding hole, the moving post 15 is in threaded connection with the screw 24, the third driving motor 14 is fixedly provided at a position corresponding to the screw 24 on the front side wall of the base 1, an output end of the third driving motor 14 is connected with the screw 24, the vertical beam 16 is fixedly provided at the right side of the top wall of the moving post 15, the cross beam 17 is fixedly provided at the top wall of the vertical beam 16, the screw 24 is driven by the driving motor three 14 to rotate in the sliding hole, the moving post 15 is driven to move in the sliding hole, and the vertical beam 16 and the cross beam 17 are adjusted in lateral position.
Referring to fig. 2, the adjusting assembly may be any one of the above embodiments, and the application provides an embodiment, where the adjusting assembly includes a second hydraulic cylinder 18, the second hydraulic cylinder 18 is fixedly disposed on the left side of the top wall of the beam 17, a U-shaped frame 19 is fixedly disposed on an output end of the second hydraulic cylinder 18, a polishing assembly is disposed on the U-shaped frame 19, and the second hydraulic cylinder 18 can adjust a longitudinal position of the U-shaped frame 19.
Referring to fig. 2, further, the U-shaped frame 19 comprises a sliding rail 22 and a limiting beam 23, the limiting beam 23 is fixedly arranged on the bottom wall of the U-shaped frame 19, the sliding rail 22 is fixedly arranged on the top wall of the cross beam 17 and corresponds to the limiting beam 23, the sliding rail 22 is slidably connected with the limiting beam 23, and when the longitudinal position of the U-shaped frame 19 is adjusted, the U-shaped frame 19 can move more stably through the movement of the limiting beam 23 in the sliding rail 22.
Referring to fig. 2, the polishing assembly may be any one of the above embodiments, and the present application provides an embodiment, where the polishing assembly includes a driving motor four 20 and a polishing wheel 21, the polishing wheel 21 is rotatably disposed on the U-shaped frame 19, the driving motor four 20 is fixedly disposed on an outer wall of one side of the U-shaped frame 19, an output end of the driving motor four 20 is connected to the polishing wheel 21, the driving motor four 20 drives the polishing wheel 21 to rotate in the U-shaped frame 19, and polishing is performed on the side of the aircraft tire through the polishing wheel 21.
Referring to fig. 1, the positioning assembly may be any one of the above embodiments, and the application provides an embodiment, where the positioning assembly includes a positioning column 13, a plurality of groups of positioning columns 13 are fixedly disposed on a top wall of a third fixing plate 12, and an aircraft tire is placed on an upper side of the third fixing plate 12 and penetrates through screw holes on the aircraft tire through the positioning columns 13, so that the aircraft tire can be positioned.
Referring to fig. 4, further, the tire fixing device further comprises a positioning groove, a plurality of groups of positioning grooves are formed in the lower side wall of the second fixing plate 10, the positioning columns 13 are matched with the positioning grooves, the first hydraulic cylinder 9 controls the second fixing plate 10 to descend, and the positioning columns 13 enter the positioning grooves, so that the stability of rotation of the aviation tire can be improved.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein 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 (7)
1. A tire side wall machining jig for an aviation tire comprises a base (1) and is characterized in that an upright post (2) is fixedly arranged on the left side of the top wall of the base (1), a first fixing plate (3) is fixedly arranged on the right side wall of the upright post (2), a connecting seat (5) is fixedly arranged on the right side wall of the first fixing plate (3), a first transverse frame (7) and a second transverse frame (8) are fixedly arranged on the right side wall of the connecting seat (5) up and down, the first transverse frame (7) is located on the upper side of the second transverse frame (8), a first hydraulic cylinder (9) is fixedly arranged on the top wall of the first transverse frame (7), an output end of the first hydraulic cylinder (9) penetrates through the first transverse frame (7) and rotates to be provided with a second fixing plate (10), a second driving motor (11) is fixedly arranged on the lower side wall of the second transverse frame (8) corresponding to the first hydraulic cylinder (9), a third fixing plate (12) is fixedly arranged on the upper side wall of the second transverse frame (8) corresponding to the second driving motor (11), an output end of the second driving motor (11) is connected with the third fixing plate (12), a positioning component is further arranged on the third fixing plate (12), a moving component is arranged on the base (1), and an adjusting component is arranged on the rear side of the grinding component.
2. The fixture for machining the side walls of the aviation tires according to claim 1, wherein the moving assembly comprises a driving motor III (14), a moving column (15), a screw (24), a vertical beam (16) and a cross beam (17), a sliding hole is formed in the rear side of the base (1), the screw (24) is rotatably arranged in the sliding hole, the moving column (15) is slidably arranged in the sliding hole, the moving column (15) is in threaded connection with the screw (24), the driving motor III (14) is fixedly arranged at the position, corresponding to the screw (24), of the front side wall of the base (1), the output end of the driving motor III (14) is connected with the screw (24), the vertical beam (16) is fixedly arranged on the right side of the top wall of the moving column (15), and the cross beam (17) is fixedly arranged on the top wall of the vertical beam (16).
3. The aviation tire sidewall machining jig according to claim 1, wherein the adjusting component comprises a second hydraulic cylinder (18), the second hydraulic cylinder (18) is fixedly arranged on the left side of the top wall of the cross beam (17), a U-shaped frame (19) is fixedly arranged at the output end of the second hydraulic cylinder (18), and a polishing component is arranged on the U-shaped frame (19).
4. The fixture for machining the side walls of the aviation tire according to claim 1, further comprising a sliding rail (22) and a limiting beam (23), wherein the limiting beam (23) is fixedly arranged on the bottom wall of the U-shaped frame (19), the sliding rail (22) is fixedly arranged at the position, corresponding to the limiting beam (23), of the top wall of the cross beam (17), and the sliding rail (22) is in sliding connection with the limiting beam (23).
5. The fixture for machining the side walls of the aviation tires according to claim 1, wherein the polishing assembly comprises a driving motor IV (20) and polishing wheels (21), the polishing wheels (21) are rotatably arranged on the U-shaped frame (19), the driving motor IV (20) is fixedly arranged on the outer wall of one side of the U-shaped frame (19), and the output end of the driving motor IV (20) is connected with the polishing wheels (21).
6. The fixture for machining the side walls of the aviation tires according to claim 1, wherein the positioning assembly comprises positioning columns (13), and a plurality of groups of positioning columns (13) are fixedly arranged on the top wall of the third fixing plate (12).
7. The fixture for machining the side wall of the aviation tire according to claim 6, further comprising positioning grooves, wherein a plurality of groups of positioning grooves are formed in the lower side wall of the second fixing plate (10), and the positioning columns (13) are matched with the positioning grooves.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202422283779.4U CN223369141U (en) | 2024-09-19 | 2024-09-19 | Aviation tire sidewall processing jig |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202422283779.4U CN223369141U (en) | 2024-09-19 | 2024-09-19 | Aviation tire sidewall processing jig |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN223369141U true CN223369141U (en) | 2025-09-23 |
Family
ID=97098830
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202422283779.4U Active CN223369141U (en) | 2024-09-19 | 2024-09-19 | Aviation tire sidewall processing jig |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN223369141U (en) |
-
2024
- 2024-09-19 CN CN202422283779.4U patent/CN223369141U/en active Active
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| GR01 | Patent grant | ||
| GR01 | Patent grant |