CN219649307U - Clamping loss prevention clamping device for producing aviation materials - Google Patents
Clamping loss prevention clamping device for producing aviation materials Download PDFInfo
- Publication number
- CN219649307U CN219649307U CN202321225225.8U CN202321225225U CN219649307U CN 219649307 U CN219649307 U CN 219649307U CN 202321225225 U CN202321225225 U CN 202321225225U CN 219649307 U CN219649307 U CN 219649307U
- Authority
- CN
- China
- Prior art keywords
- guide rail
- clamp base
- base
- clamping
- clamping device
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 239000000463 material Substances 0.000 title claims abstract description 26
- 230000002265 prevention Effects 0.000 title claims description 13
- 238000004519 manufacturing process Methods 0.000 claims description 6
- 238000009826 distribution Methods 0.000 claims description 3
- 238000003825 pressing Methods 0.000 claims description 3
- 238000010438 heat treatment Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000005452 bending Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000004566 building material Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
Landscapes
- Clamps And Clips (AREA)
Abstract
The utility model discloses an anti-clamping-loss clamping device for producing aviation materials, which relates to the field of aviation material processing and comprises a clamp base, wherein two groups of side baffles are arranged on two sides of the clamp base and perpendicular to the top surface of the clamp base, a telescopic cylinder is arranged on the inner side of the side baffles, a supporting plate is arranged on one side, close to the side baffles, of the telescopic cylinder, a base is fixedly connected with the bottom, close to the clamp base, of the supporting plate, a clamp base is connected to one side, far away from the side baffles, of the telescopic cylinder, a clamping plate is arranged on one side, far away from the telescopic cylinder, of the clamp base, a connecting rod is vertically connected to the bottom of the clamp base, and one end, close to the clamp base, of the connecting rod is fixedly provided with a guide block; according to the utility model, the guide rails and the limiting plates are arranged, so that the spacing between the limiting plates is controlled to be equal to the width of the plate, and excessive movement of the clamp base can be avoided when the clamp base is fixed in a moving way, and the plate inside the clamp base is clamped.
Description
Technical Field
The utility model relates to the field of aviation material processing, in particular to an anti-clamping device for aviation material production.
Background
The aviation material is a building material used by aviation equipment, the common aviation material has a plate-shaped tubular structure and the like, and in the production and processing process, a clamping device is needed to fix the aviation material, so that subsequent processing is convenient, and therefore, the clamping loss prevention clamping device for aviation material production is needed.
The clamping device that provides the production of space-time block in the prior art publication No. CN212020067U in the patent document through set up the hot plate on splint to and the device bottom sets up heating fan, dries the grip block in the device, avoids skidding in the centre gripping process, but still has following defect:
when the clamping device for producing the existing aviation materials is used, due to the fact that the thicknesses of the plates are different and the structure for limiting the moving distance of the clamping blocks is not provided, when the clamping blocks move inwards, the plates inside the bending are easy to move through the clamping blocks, the clamping blocks are provided with heating plates, and the heating plates are easy to damage due to the pressure in the clamping process.
Disclosure of Invention
Based on the above, the utility model aims to provide an anti-clamping and anti-damage clamping device for producing aviation materials, which solves the problems that when the existing anti-clamping and anti-damage clamping device for producing aviation materials is used, due to different thicknesses of plates and no structure for limiting the moving distance of clamping blocks, when the clamping blocks move inwards, the plates in the bent inner parts are easy to move and are damaged by excessive clamping, and the clamping blocks are provided with heating plates, so that the heating plates are easy to damage due to pressure in the clamping process.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the clamping loss prevention clamping device for the production of the aviation materials comprises a clamp base, two groups of side baffles are arranged on two sides of the clamp base and perpendicular to the top surface of the clamp base, a telescopic cylinder is arranged on the inner side of each side baffle, a supporting plate is arranged on one side, close to the side baffle, of each telescopic cylinder, a base is fixedly connected with the clamp base, one side, far away from the side baffle, of each telescopic cylinder is connected with the clamp base, a clamping plate is arranged on one side, far away from the telescopic cylinder, of each clamp base, a connecting rod is vertically connected to the bottom of each clamp base, and one end, close to the clamp base, of each connecting rod is fixedly provided with a guide block;
the fixture is characterized in that a guide rail with a strip-shaped structure is arranged on the fixture base, two ends of the guide rail are fixedly connected with the base, and a hot air port is arranged on the inner side, close to the guide rail, of the supporting plate.
Preferably, the guide block is provided with two groups of first sliding blocks near the bottom of the clamp base, the first sliding blocks inwardly protrude to form a rectangular structure, and the guide block is in sliding connection with the guide rail through the two groups of first sliding blocks.
The clamp base, the connecting rod and the guide block are parallel and level to the side surface far away from the side baffle
Preferably, the guide rail is arranged on the clamp base between the two groups of side baffles, the clamp base is fixedly connected with the guide rail, the side faces of the guide rail are symmetrically provided with the first sliding grooves of the two groups of bar structures, the center of the guide rail is rotationally provided with a rotating shaft, the side faces of the rotating shaft are fixedly connected with two groups of threaded rods, the threaded rods are arranged in the guide rail, the guide rail is axially symmetrically provided with two groups of limiting plates by taking the rotating shaft as the axis, the limiting plates are arranged at the top of the guide rail away from the clamp base, and the positions, close to the first sliding grooves, of the limiting plates are provided with second sliding blocks.
Preferably, the top surface of the guide rail is carved with graduated scales, and the graduated scales of the guide rail are symmetrically distributed by taking the rotating shaft as an axis.
Preferably, the cross section shape and the position distribution of the first sliding grooves correspond to those of the first sliding blocks, and the two groups of first sliding grooves are distributed in parallel.
Preferably, the thread directions of the surfaces of the two sets of threaded rods are opposite in symmetry with the rotating shaft as an axis.
Preferably, the structure of the limiting plate in the guide rail is penetrated by the threaded rod, the limiting plate is in threaded connection with the threaded rod, and the connecting part of the limiting plate and the guide rail is provided with a second sliding groove.
Compared with the prior art, the utility model has the beneficial effects that:
1. the guide rail and the limiting plates are arranged, so that the spacing between the limiting plates is controlled to be equal to the width of the plate, and excessive movement of the clamp base can be avoided when the clamp base is fixed in a moving way, and the plate inside the clamp base is clamped;
2. according to the utility model, the hot air ports are arranged on the side surfaces in the device, so that the clamping plates on the opposite sides of the two groups of hot air ports are dried;
drawings
FIG. 1 is a schematic diagram of a front view of the present utility model;
FIG. 2 is a schematic view of the top surface structure of the guide rail according to the present utility model;
FIG. 3 is a schematic view of the cross-sectional structure of the A-A in FIG. 2 according to the present utility model;
FIG. 4 is a schematic view of the cross-sectional structure B-B in FIG. 2 according to the present utility model;
FIG. 5 is a schematic view of the cross-sectional structure of FIG. 2 according to the present utility model.
In the figure: 1. a clamp base; 2. side baffles; 3. a telescopic cylinder; 301. a clamp base; 302. a clamping plate; 303. a connecting rod; 304. a base; 305. a support plate; 306. a guide block; 307. a first slider; 4. a guide rail; 401. a first chute; 402. a rotating shaft; 403. a threaded rod; 404. a second chute; 405. a limiting plate; 406. a second slider; 5. and a hot air port.
Detailed Description
The technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model. The embodiments described below by referring to the drawings are illustrative only and are not to be construed as limiting the utility model.
Hereinafter, an embodiment of the present utility model will be described in accordance with its entire structure.
Referring to fig. 1-5, an anti-pinching clamping device for producing aviation materials comprises a clamp base 1, side baffles 2, a telescopic cylinder 3, a clamp base 301, a clamping plate 302, a connecting rod 303, a base 304, a supporting plate 305, a guide block 306, a first sliding block 307, a guide rail 4, a first sliding groove 401, a rotating shaft 402, a threaded rod 403, a second sliding groove 404, a limiting plate 405, a second sliding block 406 and a hot air port 5, wherein two groups of side baffles 2 are arranged on two sides of the clamp base 1, the two groups of side baffles 2 are perpendicular to the top surface of the clamp base 1, the telescopic cylinder 3 is arranged on the inner side of the side baffles 2, a supporting plate 305 is arranged on one side of the telescopic cylinder 3 close to the side baffles 2, a base 304 is fixed on the bottom of the supporting plate 305 close to the clamp base 1, the base 304 is fixedly connected with the clamp base 1, one side of the telescopic cylinder 3 far away from the side baffles 2 is connected with the clamp base 301, the clamp base 301 is provided with a clamping plate 302 at one side far away from the telescopic cylinder 3, the bottom of the clamp base 301 is vertically connected with a connecting rod 303, one end of the connecting rod 303 close to the clamp base 1 is fixedly provided with a guide block 306, the bottom of the guide block 306 close to the clamp base 1 is provided with two groups of first sliding blocks 307, the first sliding blocks 307 are internally protruded with rectangular structures, the guide block 306 is slidably connected with the guide rail 4 through the two groups of first sliding blocks 307, the guide block 306 can be hung on the guide rail 4 through the first sliding blocks 307 to avoid separation from the guide rail 4, and the clamp base 301, the connecting rod 303 and the guide block 306 are flush with the side surface far away from the side baffle 2, so that when the guide block 306 is blocked by the limiting plate 405, the side surface of the clamp base 301 is flush with the limiting plate 405, and the spacing between the clamp bases 301 can be controlled by the limiting plate 405;
referring to fig. 1-5, a clamping loss prevention clamping device for producing aviation materials is provided, a guide rail 4 with a bar-shaped structure is arranged on a clamp base 1, two ends of the guide rail 4 are fixedly connected with a base 304, a hot air port 5 is installed on the inner side of a support plate 305 close to the guide rail 4, graduated scales are carved on the top surface of the guide rail 4, the graduated scales of the guide rail 4 are distributed in an axisymmetric manner by taking a rotating shaft 402 as an axisymmetric manner, a limiting plate 405 on the guide rail 4 moves, and then the observed graduated scales can be adjusted according to the width of a plate, so that the clamp base 301 is prevented from excessively moving to clamp the plate.
Referring to fig. 1-5, a clamping loss prevention clamping device for producing aviation materials is disclosed, a guide rail 4 is arranged on a clamp base 1 between two groups of side baffles 2, the clamp base 1 is fixedly connected with the guide rail 4, two groups of first sliding grooves 401 with bar structures are symmetrically arranged on the side surface of the guide rail 4, a rotating shaft 402 is rotatably arranged at the center of the guide rail 4, two groups of threaded rods 403 are fixedly connected on the side surface of the rotating shaft 402, the thread directions of the surfaces of the two groups of threaded rods 403 are opposite with the rotating shaft 402 as axial symmetry, so that when the two groups of threaded rods 403 are driven to rotate by the rotating shaft 402, two groups of limiting plates 405 can move simultaneously, the moving distance of the two groups of limiting plates 405 is consistent, the threaded rods 403 are arranged in the guide rail 4, the guide rail 4 is symmetrically provided with two groups of limiting plates 405 by taking the rotating shaft 402 as axial symmetry, the structure of the limiting plates 405 in the guide rail 4 is penetrated by the threaded rods 403, and the limiting plates 405 are in threaded connection with the threaded rods 403, the second sliding groove 404 is formed at the connection part of the limiting plate 405 and the guide rail 4, the sliding of the limiting plate 405, the second sliding groove 404 and the first sliding groove 401 can make the movement of the limiting plate 405 more stable, the limiting plate 405 is arranged at the top of the guide rail 4 far away from the clamp base 1, the second sliding block 406 is arranged at the position of the limiting plate 405 near the first sliding groove 401, the profile shape and the position distribution of the first sliding groove 401 are corresponding to those of the first sliding block 307, the two groups of first sliding grooves 401 are distributed in parallel, the sliding of the limiting plate 405 and the guide block 306 can be more stable by the first sliding groove 401 distributed in parallel, the limiting plate 405 arranged on the guide rail 4 can be adjusted by the distance between the threaded rods 403 driven by the rotation of the rotating shaft 402, thus the sliding limitation of the two groups of limiting plates 405 to the guide block 306 can control the displacement distance of the clamp base 301, thereby avoiding excessive movement to cause clamping of the sheet material on the device.
Working principle: when the device is used, the hot air ports 5 arranged on the supporting plate 305 in the side baffle plate 2 can provide hot air flow for the inner side of the device, so that the clamping plates 302 can be dried, and also the plates placed in the device can be dried, and the side baffle plate 2 is provided with two groups, so that the hot air ports 5 can dry the clamping plates 302 on the opposite sides;
then the pivot 402 on the rotatory guide rail 4, the pivot 402 is rotatory can drive the threaded rod 403 of both sides and rotate, can drive limiting plate 405 and remove when the threaded rod 403 is rotatory, limiting plate 405's position can be through the interval of scale control two sets of limiting plates 405 on the guide rail 4, like this when fixed panel, can adjust the width size of fixed panel with two sets of limiting plates 405, play the effect of restriction, then start telescopic cylinder 3, telescopic cylinder 3 can drive anchor clamps base 301 outwards remove, guide block 306 is moved on guide rail 4 can be driven through connecting rod 303 when anchor clamps base 301 remove, guide block 306 can remove the side of limiting plate 405 at last and be blocked by limiting plate 405, and the splint 302 of anchor clamps base 301 side protrusion in the side of guide block 306, can play the effect of pressing from both sides tight panel, make the device avoid pressing from both sides the fixed panel that can be better when damaging the panel, avoid panel's rocking, the use of device has just so accomplished, the content that does not describe in detail in this specification belongs to the prior art that the well known in the art of expert person.
The terms "center," "longitudinal," "transverse," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used for descriptive simplicity and convenience only and not as an indication or implying that the apparatus or element being referred to must have a particular orientation, be constructed and operated for a particular orientation, based on the orientation or positional relationship illustrated in the drawings, and thus should not be construed as limiting the scope of the present utility model.
Although the present utility model has been described with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described, or equivalents may be substituted for elements thereof, and any modifications, equivalents, improvements and changes may be made without departing from the spirit and principles of the present utility model.
Claims (8)
1. A prevent pressing from both sides and damaging clamping device for aviation material production, includes anchor clamps base (1), its characterized in that: two groups of side baffles (2) are arranged on two sides of the clamp base (1), the two groups of side baffles (2) are perpendicular to the top surface of the clamp base (1), a telescopic cylinder (3) is arranged on the inner side of the side baffles (2), a supporting plate (305) is arranged on one side, close to the side baffles (2), of the telescopic cylinder (3), a base (304) is fixed on the bottom, close to the clamp base (1), of the supporting plate (305), the base (304) is fixedly connected with the clamp base (1), a clamp base (301) is connected to one side, far away from the side, of the telescopic cylinder (3), of the clamp base (301), a clamping plate (302) is arranged on one side, far away from the telescopic cylinder (3), of the bottom of the clamp base (301), a connecting rod (303) is perpendicularly connected to one end, close to the clamp base (1), of the connecting rod (303), is fixedly provided with a guide block (306).
The fixture is characterized in that a guide rail (4) with a strip-shaped structure is arranged on the fixture base (1), two ends of the guide rail (4) are fixedly connected with the base (304), and a hot air port (5) is arranged on the inner side, close to the guide rail (4), of the supporting plate (305).
2. The clamping loss prevention clamping device for producing aviation materials according to claim 1, wherein: two groups of first sliding blocks (307) are arranged at the bottom of the guide block (306) close to the clamp base (1), the first sliding blocks (307) are internally protruded to form a rectangular structure, and the guide block (306) is in sliding connection with the guide rail (4) through the two groups of first sliding blocks (307).
3. The clamping loss prevention clamping device for producing aviation materials according to claim 1, wherein: the clamp base (301), the connecting rod (303) and the guide block (306) are flush with the side surface away from the side baffle plate (2).
4. The clamping loss prevention clamping device for producing aviation materials according to claim 1, wherein: guide rail (4) set up on anchor clamps base (1) between two sets of side shield (2), and anchor clamps base (1) and guide rail (4) fixed connection, first spout (401) of two sets of bar structures have been seted up to the side symmetry of guide rail (4), the center rotation of guide rail (4) is provided with pivot (402), the side fixedly connected with two sets of threaded rods (403) of pivot (402), threaded rod (403) set up in the inside of guide rail (4), guide rail (4) are provided with two sets of limiting plates (405) for axisymmetry with pivot (402), limiting plates (405) set up in guide rail (4) keep away from the top of anchor clamps base (1), limiting plates (405) are provided with second slider (406) on being close to the position of first spout (401).
5. The clamping loss prevention clamping device for producing an aircraft material according to claim 4, wherein: the top surface of the guide rail (4) is carved with a graduated scale, and the graduated scales of the guide rail (4) are symmetrically distributed by taking the rotating shaft (402) as an axis.
6. The clamping loss prevention clamping device for producing an aircraft material according to claim 4, wherein: the cross section shape and the position distribution of the first sliding grooves (401) are corresponding to those of the first sliding blocks (307), and the two groups of first sliding grooves (401) are distributed in parallel.
7. The clamping loss prevention clamping device for producing an aircraft material according to claim 4, wherein: the thread directions of the surfaces of the two groups of threaded rods (403) are opposite in symmetry by taking the rotating shaft (402) as an axis.
8. The clamping loss prevention clamping device for producing an aircraft material according to claim 4, wherein: the structure of limiting plate (405) in guide rail (4) is run through by threaded rod (403), and threaded connection between limiting plate (405) and threaded rod (403), and second spout (404) have been seted up in the junction of limiting plate (405) and guide rail (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321225225.8U CN219649307U (en) | 2023-05-19 | 2023-05-19 | Clamping loss prevention clamping device for producing aviation materials |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321225225.8U CN219649307U (en) | 2023-05-19 | 2023-05-19 | Clamping loss prevention clamping device for producing aviation materials |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219649307U true CN219649307U (en) | 2023-09-08 |
Family
ID=87881367
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321225225.8U Active CN219649307U (en) | 2023-05-19 | 2023-05-19 | Clamping loss prevention clamping device for producing aviation materials |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219649307U (en) |
-
2023
- 2023-05-19 CN CN202321225225.8U patent/CN219649307U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8641408B2 (en) | Device for stretching film sections in a monoaxial or biaxial manner | |
| CN208826100U (en) | A kind of aluminum profile multi-angle clamping and fixing device | |
| CN112872692B (en) | Cable testing bridge preparation welding forming frock clamp | |
| CN219649307U (en) | Clamping loss prevention clamping device for producing aviation materials | |
| CN215470692U (en) | Detection clamp for operation panel | |
| CN215241481U (en) | Nailing machine for processing waterproof bag | |
| CN213179105U (en) | High-quality waterproof building templates processing is with timber drying equipment | |
| CN210923583U (en) | Ultrasonic wave wall body quality detector | |
| CN114054537A (en) | Section bar extrusion device for cable bridge | |
| CN110216630B (en) | Civil air defense cement door leaf frame splicing tool and using method thereof | |
| CN210547305U (en) | Automatic change stretch forming device | |
| CN209440550U (en) | A kind of plaster board cutting tool | |
| CN108265992B (en) | Movable device convenient for adjusting wall surface alignment degree | |
| CN219054571U (en) | Insulation board cutting equipment | |
| CN207549760U (en) | A kind of ceramic tile printing machine that can improve stamp accuracy rate | |
| CN210677833U (en) | Bearing adds clamping apparatus with adjustable vertical specification | |
| CN215638493U (en) | Energy-efficient glass instrument air current drying apparatus | |
| CN220561627U (en) | Building insulation board cutting device | |
| CN209461221U (en) | A kind of device for master row insulating Shape correction | |
| CN217711791U (en) | Adjustable concrete push pedal | |
| CN221219616U (en) | Adjustable jacking of building attached scaffold | |
| CN219996794U (en) | Hardness detection device for building engineering materials | |
| CN220542670U (en) | Building concrete intensity detection device | |
| CN215351454U (en) | Catheter fixing structure for catheter room nursing | |
| CN220014153U (en) | Mounting structure of assembled masonry stone curtain wall |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |