CN220145765U - Positioning device for processing aviation parts - Google Patents
Positioning device for processing aviation parts Download PDFInfo
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- CN220145765U CN220145765U CN202321687159.6U CN202321687159U CN220145765U CN 220145765 U CN220145765 U CN 220145765U CN 202321687159 U CN202321687159 U CN 202321687159U CN 220145765 U CN220145765 U CN 220145765U
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- 238000012545 processing Methods 0.000 title claims abstract description 14
- 230000000694 effects Effects 0.000 claims abstract description 11
- 230000007246 mechanism Effects 0.000 claims description 12
- 238000006073 displacement reaction Methods 0.000 claims description 3
- 238000003754 machining Methods 0.000 claims 2
- 238000004519 manufacturing process Methods 0.000 abstract description 4
- 230000005012 migration Effects 0.000 abstract description 3
- 238000013508 migration Methods 0.000 abstract description 3
- 230000007306 turnover Effects 0.000 description 5
- 230000007547 defect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000001174 ascending effect Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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Abstract
The utility model discloses a positioning device for processing aviation parts, which comprises a horizontal moving assembly; the first motor is arranged on the side surface of the horizontal moving assembly and provides power for the operation of the horizontal moving assembly; the electric cylinder is arranged at the top of the horizontal moving assembly, so that the positioning device is lifted in the vertical direction; the overturning assembly is arranged at the top of the electric cylinder, so that the positioning device has an overturning function; the clamping assembly is fixedly connected with the overturning assembly; and the second motor is arranged at the top of the clamping assembly and drives the clamping assembly to operate. In the above-mentioned scheme, set up horizontal migration subassembly, motor, electronic jar, upset subassembly, motor No. two, reach the aviation spare part that can centre gripping different length and width, be applicable to the effect of different specification spare parts, set up upset subassembly, when reaching the omnidirectional processing of aviation spare part, need not remove fixedly and can overturn aviation spare part machine, improve production efficiency's effect.
Description
Technical Field
The utility model relates to the technical field of positioning devices, in particular to a positioning device for processing aviation parts.
Background
The aviation parts are the general names of parts required by manufacturing an airplane, and a positioning device is required to fix and clamp the parts in the processing process of the aviation parts, but the aviation parts still have some defects in actual use, such as: the parts involved in the aircraft manufacturing process are numerous, because the types of the aircraft parts are various, the existing positioning device is mostly single, only the same type of parts are clamped, each type of aviation parts is required to be provided with a specific fixing device, and when the types of the parts change, the positioning clamp is required to be replaced, so that one positioning device cannot clamp different aviation parts, and the work efficiency is affected by frequent replacement of the clamp.
Disclosure of Invention
In order to overcome the defects of the prior art, the embodiment of the utility model provides a positioning device for processing aviation parts, which solves the problems that most of the existing positioning devices in the prior art are single, only clamping is carried out on parts of the same type, each aviation part is required to be provided with a specific fixing device, and when the types of the parts are changed, a positioning clamp is required to be replaced, so that one positioning device cannot clamp different aviation parts.
In order to solve the technical problems, the utility model provides the following technical scheme: positioning device for processing aviation parts, comprising
A horizontal movement assembly;
the first motor is arranged on the side surface of the horizontal moving assembly and provides power for the operation of the horizontal moving assembly;
the electric cylinder is arranged at the top of the horizontal moving assembly, so that the positioning device is lifted in the vertical direction;
the overturning assembly is arranged at the top of the electric cylinder, so that the positioning device has an overturning function;
the clamping assembly is fixedly connected with the overturning assembly, plays a role in clamping aviation parts, can be adjusted in the vertical direction according to the size of the aviation parts, and can adapt to the effects of the aviation parts with different specifications by matching with the horizontal moving assembly;
and the second motor is arranged at the top of the clamping assembly and drives the clamping assembly to operate.
The horizontal movement assembly comprises a horizontal movement outer box, a first screw rod and a sliding block, wherein the first screw rod is rotationally connected with the inside of the horizontal movement outer box, the sliding block is in threaded connection with the outer surface of the first screw rod and is in sliding connection with the length direction inside the horizontal movement outer box, and the sliding block is fixedly connected with the bottom surface of the electric cylinder.
The clamping assembly comprises a clamping shell, a second screw rod, a movable clamping block, a fixed clamping block and a buffer mechanism, wherein the clamping shell is fixedly connected with the overturning assembly, the second screw rod is rotationally connected with the width direction inside the clamping shell, the movable clamping block is in threaded connection with the outer surface of the second screw rod and is in sliding connection with the length direction inside the clamping shell, the fixed clamping block is fixedly connected with the clamping shell, and the buffer mechanism is arranged at the edge of the front length direction of the clamping shell.
The clamping assembly further comprises an anti-slip pad, wherein the anti-slip pad is arranged on the outer surfaces of the movable clamping block and the fixed clamping block, and plays roles in preventing slip and displacement during clamping.
The buffer mechanism comprises a sleeve, a buffer block, a spring, a fixed column and a contact block, wherein the sleeve is fixedly connected with a clamping shell, the buffer block is fixedly connected with the bottom end of the inside of the sleeve, the two ends of the fixed column are respectively fixedly connected with the buffer block and the contact block, and the two ends of the spring are respectively fixedly connected with the buffer block and the contact block and are sleeved on the outside of the fixed column.
The turnover assembly comprises a fixed block, a third motor and a rotary table, wherein the fixed block is fixedly connected with the top end of the electric cylinder, the third motor is fixedly connected with the side face of the fixed block, the rotary table is fixedly connected with the driving shaft of the third motor, the rotary table is rotationally connected with the inside of the fixed block, and the rotary table is fixedly connected with the clamping shell.
The technical scheme of the utility model has the following beneficial effects:
in the above-mentioned scheme, set up horizontal migration subassembly, a motor, the electronic jar, the upset subassembly, no. two motors, place aviation spare part on fixed clamp splice during the use, start No. two motors, make activity clamp splice activity press from both sides the vertical orientation of aviation spare part tightly, start No. one motor, make the slider move in the horizontal direction, thereby drive the clamping assembly activity, make the centre gripping shell press from both sides aviation spare part horizontal direction tightly, reach the aviation spare part that can centre gripping different length and width, be applicable to the effect of different specification spare part, set up the upset subassembly, start No. three motors, make No. three motor drive carousel rotatory, thereby drive the clamping assembly rotatory, make aviation spare part realize the upset of different angles, reach when all-round processing of aviation spare part, need not remove the fixed effect that can overturn aviation spare part machine, improvement production efficiency.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present utility model;
FIG. 2 is a schematic view of a horizontal moving assembly according to the present utility model;
FIG. 3 is a schematic view of a clamping assembly according to the present utility model;
FIG. 4 is a schematic diagram of a buffer mechanism according to the present utility model;
fig. 5 is a schematic structural diagram of a flipping assembly according to the present utility model.
[ reference numerals ]
1. A horizontal movement assembly; 2. a motor I; 3. an electric cylinder; 4. a flip assembly; 5. a clamping assembly; 6. a motor II; 11. the outer box is horizontally moved; 12. a first screw; 13. a slide block; 51. clamping the housing; 52. a second screw; 53. a movable clamping block; 54. fixing the clamping blocks; 55. a buffer mechanism; 56. an anti-slip pad; 551. a sleeve; 552. a buffer block; 553. a spring; 554. fixing the column; 555. a contact block; 41. a fixed block; 42. a third motor; 43. a turntable.
Detailed Description
In order to make the technical problems, technical solutions and advantages to be solved more apparent, the following detailed description will be given with reference to the accompanying drawings and specific embodiments.
The embodiment of the utility model shown in fig. 1 to 5 provides a positioning device for processing aviation components, comprising,
a horizontal movement assembly 1;
the first motor 2 is arranged on the side surface of the horizontal moving assembly 1 and provides power for the operation of the horizontal moving assembly 1;
the electric cylinder 3 is arranged at the top of the horizontal moving assembly 1, so that the positioning device is lifted in the vertical direction;
the overturning assembly 4 is arranged at the top of the electric cylinder 3, so that the positioning device has an overturning function;
the clamping assembly 5, clamping assembly 5 plays the centre gripping effect to aviation spare part with upset subassembly 4 fixed connection, can carry out the ascending regulation of vertical direction according to the size of aviation spare part, cooperates the horizontal migration subassembly to realize the effect that can adapt to different specification aviation spare parts.
And the motor No. two 6 is arranged at the top of the clamping assembly 5 and drives the clamping assembly 5 to operate.
The horizontal movement assembly 1 comprises a horizontal movement outer box 11, a first screw rod 12 and a sliding block 13, wherein the first screw rod 12 is rotationally connected with the inside of the horizontal movement outer box 11, the sliding block 13 is in threaded connection with the outer surface of the first screw rod 12 and is in sliding connection with the length direction inside the horizontal movement outer box 11, and the sliding block 13 is fixedly connected with the bottom surface of the electric cylinder 3.
The clamping assembly 5 comprises a clamping shell 51, a second screw rod 52, a movable clamping block 53, a fixed clamping block 54 and a buffer mechanism 55, wherein the clamping shell 51 is fixedly connected with the overturning assembly 4, the second screw rod 52 is rotationally connected with the inside of the clamping shell 51 in the width direction, the movable clamping block 53 is in threaded connection with the outer surface of the second screw rod 52 and is in sliding connection with the inside of the clamping shell 51 in the length direction, the fixed clamping block 54 is fixedly connected with the clamping shell 51, and the buffer mechanism 55 is arranged at the edge of the front side of the clamping shell 51 in the length direction; the buffer mechanism 55 can play a role in buffering aviation components and parts, and overcomes the defect that the pressure intensity is high due to the fact that the contact surface is too small when the device is clamped in the horizontal direction.
The clamping assembly 5 further comprises an anti-slip pad 56, wherein the anti-slip pad 56 is arranged on the outer surfaces of the movable clamping block 53 and the fixed clamping block 54, and plays roles in anti-slip and displacement prevention during clamping.
The buffer mechanism 55 comprises a sleeve 551, a buffer block 552, a spring 553, a fixed column 554 and a contact block 555, wherein the sleeve 551 is fixedly connected with the clamping shell 51, the buffer block 552 is fixedly connected with the bottom end inside the sleeve 551, two ends of the fixed column 554 are respectively fixedly connected with the buffer block 552 and the contact block 555, and two ends of the spring 553 are respectively fixedly connected with the buffer block 552 and the contact block 555 and are sleeved outside the fixed column 554.
The overturning assembly 4 comprises a fixed block 41, a third motor 42 and a rotary table 43, wherein the fixed block 41 is fixedly connected with the top end of the electric cylinder 3, the third motor 42 is fixedly connected with the side surface of the fixed block 41, the rotary table 43 is fixedly connected with a driving shaft of the third motor 42, the rotary table 43 is rotationally connected with the inside of the fixed block 41, and the rotary table 43 is fixedly connected with the clamping shell 51; the two mutually opposite turnover assemblies 4 are shared, one turnover assembly 4 has no active rotation function, the rotation is driven by the active rotation of the other turnover assembly 4, when the aviation parts with larger size are turned over, the parts possibly collide with the horizontal movement assembly 1 and cannot be turned over, and then the height of the electric cylinder 3 is increased, so that the turnover can be smoothly carried out.
The working process of the utility model is as follows: the aviation part is placed on the fixed clamping block 54, the motor No. 6 is started, the movable clamping block 53 is enabled to move to clamp the aviation part in the vertical direction, the motor No. 2 is started, the sliding block 13 is enabled to move in the horizontal direction, the clamping assembly 5 is driven to move, the clamping shell 51 is enabled to clamp the aviation part in the horizontal direction, the aviation part is enabled to be completely fixed, the overturning assembly 4 is arranged, the motor No. 42 is started, the motor No. 42 is enabled to drive the turntable 43 to rotate, the clamping assembly 5 is driven to rotate, and the aviation part is enabled to overturn.
The last points to be described are: first, in the description of the present utility model, it should be noted that, unless otherwise specified and defined, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be mechanical or electrical, or may be a direct connection between two elements, and "upper," "lower," "left," "right," etc. are merely used to indicate relative positional relationships, which may be changed when the absolute position of the object being described is changed;
secondly: in the drawings of the disclosed embodiments, only the structures related to the embodiments of the present disclosure are referred to, and other structures can refer to the common design, so that the same embodiment and different embodiments of the present disclosure can be combined with each other under the condition of no conflict;
finally: 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 principles of the utility model are intended to be included within the scope of the utility model.
Claims (6)
1. Positioning device for processing aviation parts, which is characterized by comprising
A horizontal movement assembly;
the first motor is arranged on the side surface of the horizontal moving assembly and provides power for the operation of the horizontal moving assembly;
the electric cylinder is arranged at the top of the horizontal moving assembly, so that the positioning device is lifted in the vertical direction;
the overturning assembly is arranged at the top of the electric cylinder, so that the positioning device has an overturning function;
the clamping assembly is fixedly connected with the overturning assembly, plays a role in clamping aviation parts, can be adjusted in the vertical direction according to the size of the aviation parts, and can adapt to the effects of the aviation parts with different specifications by matching with the horizontal moving assembly;
and the second motor is arranged at the top of the clamping assembly and drives the clamping assembly to operate.
2. The positioning device for machining aviation components of claim 1, wherein the horizontal moving assembly comprises a horizontal moving outer box, a first screw rod and a sliding block, the first screw rod is rotationally connected with the inside of the horizontal moving outer box, the sliding block is in threaded connection with the outer surface of the first screw rod and is in sliding connection with the length direction inside the horizontal moving outer box, and the sliding block is fixedly connected with the bottom surface of the electric cylinder.
3. The positioning device for machining aviation components according to claim 1, wherein the clamping assembly comprises a clamping shell, a second screw rod, a movable clamping block, a fixed clamping block and a buffer mechanism, the clamping shell is fixedly connected with the overturning assembly, the second screw rod is rotationally connected with the width direction inside the clamping shell, the movable clamping block is in threaded connection with the outer surface of the second screw rod and is in sliding connection with the length direction inside the clamping shell, the fixed clamping block is fixedly connected with the clamping shell, and the buffer mechanism is arranged at the edge of the front length direction of the clamping shell.
4. The positioning device for processing aviation components of claim 3, wherein the clamping assembly further comprises anti-slip pads, the anti-slip pads are arranged on the outer surfaces of the movable clamping block and the fixed clamping block, and the anti-slip pads play a role in anti-slip and anti-displacement during clamping.
5. The positioning device for processing the aviation components of claim 3, wherein the buffer mechanism comprises a sleeve, a buffer block, a spring, a fixing column and a contact block, the sleeve is fixedly connected with the clamping shell, the buffer block is fixedly connected with the bottom end inside the sleeve, two ends of the fixing column are respectively fixedly connected with the buffer block and the contact block, and two ends of the spring are respectively fixedly connected with the buffer block and the contact block and are sleeved outside the fixing column.
6. The positioning device for processing the aviation components of claim 1, wherein the overturning assembly comprises a fixed block, a third motor and a rotary table, the fixed block is fixedly connected with the top end of the electric cylinder, the third motor is fixedly connected with the side face of the fixed block, the rotary table is fixedly connected with a driving shaft of the third motor, the rotary table is rotatably connected with the inside of the fixed block, and the rotary table is fixedly connected with the clamping shell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321687159.6U CN220145765U (en) | 2023-06-30 | 2023-06-30 | Positioning device for processing aviation parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321687159.6U CN220145765U (en) | 2023-06-30 | 2023-06-30 | Positioning device for processing aviation parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220145765U true CN220145765U (en) | 2023-12-08 |
Family
ID=89010974
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321687159.6U Active CN220145765U (en) | 2023-06-30 | 2023-06-30 | Positioning device for processing aviation parts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220145765U (en) |
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2023
- 2023-06-30 CN CN202321687159.6U patent/CN220145765U/en active Active
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