CN220660132U - Protective structure of aviation aluminum plate cutting machine - Google Patents
Protective structure of aviation aluminum plate cutting machine Download PDFInfo
- Publication number
- CN220660132U CN220660132U CN202322339619.2U CN202322339619U CN220660132U CN 220660132 U CN220660132 U CN 220660132U CN 202322339619 U CN202322339619 U CN 202322339619U CN 220660132 U CN220660132 U CN 220660132U
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- China
- Prior art keywords
- fixedly connected
- box
- aluminum plate
- protective structure
- cutting machine
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- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims abstract description 35
- 229910052782 aluminium Inorganic materials 0.000 title claims abstract description 35
- 230000001681 protective effect Effects 0.000 title claims abstract description 17
- 239000000428 dust Substances 0.000 claims abstract description 12
- 230000007246 mechanism Effects 0.000 claims abstract description 8
- 229910001095 light aluminium alloy Inorganic materials 0.000 claims 5
- 230000000694 effects Effects 0.000 abstract description 6
- 238000010521 absorption reaction Methods 0.000 abstract description 3
- 238000000605 extraction Methods 0.000 abstract description 2
- 239000003292 glue Substances 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 9
- 230000008569 process Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 239000002699 waste material Substances 0.000 description 3
- 206010000372 Accident at work Diseases 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004040 coloring Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/10—Greenhouse gas [GHG] capture, material saving, heat recovery or other energy efficient measures, e.g. motor control, characterised by manufacturing processes, e.g. for rolling metal or metal working
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- Sawing (AREA)
Abstract
The utility model relates to a protective structure of an aviation aluminum plate cutting machine, which comprises a box body, wherein the top of the box body is fixedly connected with a shell, a dust collection mechanism is arranged on the box body, a limiting assembly is arranged on the box body, the dust collection mechanism comprises two cylinders which are fixedly arranged at the top of the shell, output shafts of the two cylinders are fixedly connected with movable plates, the left side and the right side of each movable plate are fixedly connected with a first sliding block, the bottom of each movable plate is fixedly provided with an electric sliding rail, and the inside of each electric sliding rail is slidably connected with an electric sliding block. This aviation aluminum plate cutting machine's protective structure through setting up dust extraction, makes the cutting machine have the function of dust absorption, reaches the effect of absorbing and collecting the sweeps that aluminum plate cutting produced to avoid the piece to glue and influence the cutting effect on the aluminum product, and then conveniently collect the processing to the sweeps, made things convenient for the use of user, increased the practicality of cutting machine.
Description
Technical Field
The utility model relates to the technical field of aluminum processing, in particular to a protective structure of an aviation aluminum plate cutting machine.
Background
Aluminum materials are manufactured from aluminum and other alloying elements. The aluminum alloy is usually manufactured by processing into cast products, forged products, foils, plates, belts, pipes, bars, sectional materials and the like, and then performing cold bending, sawing, drilling, assembling, coloring and other procedures.
For example, chinese patent CN218193801U discloses a novel cutting machine for aviation aluminum plate processing, including second mounting panel, rotating assembly and moving assembly, the equal fixed mounting in both ends of second mounting panel upside has the support column, the both ends fixed mounting of second mounting panel downside has the support sill, two the top fixed mounting of support column has the roof, rotating assembly is located the upside of second mounting panel, moving assembly is located the below of roof, rotating assembly includes the second motor rack, the upside fixed mounting of second motor rack has the second motor, the output shaft direction of second motor is the upside, the output shaft of second motor runs through in the middle part of second mounting panel, the output shaft top fixed mounting of second motor has the rotating plate, however this cutting machine is at cutting aluminum plate in-process, and the piece produces easily and splashes, probably falls into workman's eye, causes industrial accident, and aluminum plate has also caused the pollution to operational environment, so proposes an aviation cutting machine's protective structure to solve above-mentioned problem.
Disclosure of Invention
Aiming at the defects of the prior art, the utility model provides a protective structure of an aviation aluminum plate cutting machine, which has the advantages of preventing scraps from splashing and the like, and solves the problems that scraps are easy to splash and possibly fall into eyes of workers to cause industrial accidents and pollute the working environment in the process of cutting an aluminum plate by the cutting machine.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the protection structure of the aviation aluminum plate cutting machine comprises a box body, wherein the top of the box body is fixedly connected with a shell, a dust collection mechanism is arranged on the box body, and a limiting assembly is arranged on the box body;
the dust absorption mechanism comprises a plurality of cylinders which are two and fixedly arranged at the top of a shell, wherein the two cylinders are fixedly connected with a movable plate on the output shaft of the cylinders, a first sliding block is fixedly connected to the left side and the right side of the movable plate, an electric sliding rail is fixedly arranged at the bottom of the movable plate, an electric sliding block is fixedly connected to the inside of the electric sliding rail, a first motor is fixedly arranged at the bottom of the electric sliding block, a rotating shaft is fixedly connected to the output shaft of the first motor, a cutting knife is fixedly connected to the outer side of the rotating shaft, a connecting shell is fixedly connected to the bottom of the electric sliding block, a cover body is fixedly connected to the second sliding block on the left side and the right side of the connecting shell, a collecting box is fixedly connected to the top of the box, a telescopic hose is fixedly connected to the bottom of the collecting box, a filter plate is fixedly connected to the left side and the right side of the filter plate, and an exhaust fan is fixedly arranged inside of the collecting box.
Further, spacing subassembly includes No. two motors with box right side fixed mounting, no. two motor's output shaft fixedly connected with threaded rod, the outside threaded connection of threaded rod has the screw thread piece, the top fixedly connected with connecting block of screw thread piece, the top fixedly connected with U template of connecting block, the equal fixedly connected with in left and right sides of U template inner wall is two fixed plate of quantity, and the top is two equal threaded connection in inside of fixed plate has the bolt, two equal fixedly connected with limiting plate in bottom of bolt, the interior bottom wall sliding connection of U template has the cabin body.
Further, a sliding groove is formed in the left side and the right side of the inner wall of the box body, the inside of the sliding groove is in sliding connection with the outer side of the sliding block, a sliding groove No. two is formed in the connecting shell, and the inside of the sliding groove No. two is in sliding connection with the outer side of the sliding block No. two.
Further, limit grooves are formed in the left side and the right side of the inner wall of the collecting box, and the inside of each limit groove is in sliding connection with the outer side of each limit block.
Further, the top of collecting box has seted up the venthole, flexible hose's one end runs through and extends to the inside of the cover body.
Further, the inside of connecting the shell has seted up the slip through-hole, the inside of slip through-hole and the outside sliding connection of the cover body.
Further, rectangular through holes are formed in the top of the box body, and the size of each rectangular through hole is matched with the size of the connecting block.
Compared with the prior art, the technical scheme of the application has the following beneficial effects:
1. this aviation aluminum plate cutting machine's protective structure through setting up dust extraction, makes the cutting machine have the function of dust absorption, reaches the effect of absorbing and collecting the sweeps that aluminum plate cutting produced to avoid the piece to glue and influence the cutting effect on the aluminum product, and then conveniently collect the processing to the sweeps, made things convenient for the use of user, increased the practicality of cutting machine.
2. This aviation aluminum plate cutting machine's protective structure through setting up spacing subassembly, makes the cutting machine have spacing function, reaches the effect that carries out spacing to aluminum plate to conveniently cut aluminum plate, also conveniently adjust aluminum plate's position simultaneously, made things convenient for user's use, improved cutting machine's practicality.
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. 1A according to the present utility model;
fig. 3 is a front view of the structure of the present utility model.
In the figure: the device comprises a box body 1, a shell 2, a cylinder 3, a movable plate 4, a slider 5, an electric slide rail 6, an electric slider 7, a motor 8, a rotating shaft 9, a cutting knife 10, a connecting shell 11, a cover body 12, a slider 13, a collecting box 14, a telescopic hose 15, a filter plate 16, a limiting block 17, an exhaust fan 18, a motor 19, a threaded rod 20, a threaded block 21, a connecting block 22, a U-shaped plate 23, a fixed plate 24, a bolt 25, a limiting plate 26 and a cabin 27.
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. 1-3, the protection structure of an aviation aluminum plate cutting machine in this embodiment includes a box 1, a first chute is provided on both sides of an inner wall of the box 1, a rectangular through hole is provided at a top of the box 1, a housing 2 is fixedly connected to the top of the box 1, a dust suction mechanism is provided on the box 1, and a limit assembly is provided on the box 1.
The dust collection mechanism comprises two cylinders 3 fixedly arranged at the top of a shell 2, the output shafts of the two cylinders 3 are fixedly connected with a movable plate 4, the left side and the right side of the movable plate 4 are fixedly connected with a first sliding block 5, the inside of the first sliding block is in sliding connection with the outer side of the first sliding block 5, the bottom of the movable plate 4 is fixedly provided with an electric sliding rail 6, the inside of the electric sliding rail 6 is in sliding connection with an electric sliding block 7, the bottom of the electric sliding block 7 is fixedly provided with a first motor 8, the output shaft of the first motor 8 is fixedly connected with a rotating shaft 9, the outer side of the rotating shaft 9 is fixedly connected with a cutting knife 10, the bottom of the electric sliding block 7 is fixedly connected with a connecting shell 11, the inside of the connecting shell 11 is provided with a second sliding block, the inside of the connecting shell 11 is provided with a sliding through hole, the inside of the connecting shell 11 is in sliding connection with a cover body 12, the inside of sliding through hole and the outside sliding connection of the cover body 12, the equal fixedly connected with No. two sliders 13 in the left and right sides of the cover body 12, the inside and the outside sliding connection of No. two sliders 13 of No. two spouts, the top fixedly connected with collecting box 14 of box 1, the spacing groove has all been seted up to the left and right sides of collecting box 14 inner wall, the venthole has been seted up at the top of collecting box 14, the bottom fixedly connected with flexible hose 15 of collecting box 14, the one end of flexible hose 15 runs through and extends to the inside of the cover body 12, the inside sliding connection of collecting box 14 has filter 16, the equal fixedly connected with stopper 17 in the left and right sides of filter 16, the inside and the outside sliding connection of stopper 17 of spacing groove, the inside fixed mounting of collecting box 14 has air exhauster 18.
The front surface of the collecting box 14 is movably provided with a movable door, and the outer side of the movable door is fixedly connected with a sealing ring which is attached to the front surface of the collecting box 14.
In this embodiment, spacing subassembly includes with box 1 right side fixed mounting's No. two motor 19, no. two motor 19's output shaft fixedly connected with threaded rod 20, threaded rod 20's outside threaded connection has screw thread piece 21, screw thread piece 21's top fixedly connected with connecting block 22, the size of rectangle through hole and connecting block 22's size looks adaptation, connecting block 22's top fixedly connected with U template 23, U template 23's the equal fixedly connected with fixed plate 24 of the left and right sides of inner wall is two in quantity, the equal threaded connection in the inside of two fixed plates 24 in top has bolt 25, the equal fixedly connected with limiting plate 26 in bottom of two bolts 25, U template 23's interior bottom wall sliding connection has cabin body 27.
The working principle of the embodiment is as follows:
this aviation aluminum plate cutting machine's protective structure, when using, place aluminum plate at the top of two fixed plates 24 in two bottoms, then rotate bolt 25, bolt 25 drives limiting plate 26 downstream, carry out spacing fixed to aluminum plate, start motor No. two 19, motor No. two 19's output shaft drives threaded rod 20, threaded rod 20 drives screw thread piece 21 and rotates, through setting up the rectangle through-hole, carry out spacing support to it, make it only can control the motion, thereby drive aluminum plate side-to-side motion, the convenience is adjusted aluminum plate's position, the convenience cuts aluminum plate's different positions, start two cylinders 3, cylinder 3's output shaft drives movable plate 4 downstream, through setting up slider 5 and spout No. one, carry out spacing support to movable plate 4, stability when increasing movable plate 4 motion, start motor No. 8, motor No. 8's output shaft drives pivot 9 and rotates, thereby drive cutter 10 and rotate, and drive cutter 10 downstream cuts aluminum plate, and then make cover 12 upwards slide in the inside of coupling shell 11, through setting up slider 13 and spout No. two, the position to support the aluminum plate 12, the convenience is cut at the inside of the side-to-side motion is cut at the side-to-side edge of the side of the aluminum plate, the exhaust fan is cut at the side-to the side of the exhaust fan is cut to the end of the exhaust fan is cut, the effect is produced at the end of the expansion machine is cut to the exhaust fan is increased to the exhaust fan is 16, the side-to the exhaust fan is cut, the exhaust fan is further has been carried out to the exhaust fan is more in the end of the exhaust fan is 16, and is more convenient to the exhaust fan is cut, the waste chip is cut, and is further to the waste chip is more than 16, and has been cut, and has been more convenient to the waste chip is more than is cut and has been cut.
The control mode of the utility model is controlled by the controller, the control circuit of the controller can be realized by simple programming of a person skilled in the art, the supply of the power supply also belongs to the common knowledge in the art, and the utility model is mainly used for protecting mechanical devices, so the utility model does not explain the control mode and circuit connection in detail.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising one … …" does not exclude the presence of other like elements in a process, method, article, or apparatus that comprises the element.
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. The utility model provides a protective structure of aviation aluminum plate cutting machine, includes box (1), its characterized in that: the top of the box body (1) is fixedly connected with a shell (2), a dust collection mechanism is arranged on the box body (1), and a limiting assembly is arranged on the box body (1);
the dust collection mechanism comprises two cylinders (3) fixedly mounted on the top of a shell (2), two output shafts of the cylinders (3) are fixedly connected with a movable plate (4), a first sliding block (5) is fixedly connected to the left side and the right side of the movable plate (4), an electric sliding rail (6) is fixedly mounted on the bottom of the movable plate (4), an electric sliding block (7) is fixedly connected to the inside of the electric sliding rail (6), a first motor (8) is fixedly mounted on the bottom of the electric sliding block (7), a rotating shaft (9) is fixedly connected to the output shaft of the first motor (8), a cutting knife (10) is fixedly connected to the outer side of the rotating shaft (9), a connecting shell (11) is fixedly connected to the bottom of the electric sliding block (7), a cover body (12) is fixedly connected to the inner side of the connecting shell (11), a second sliding block (13) is fixedly connected to the left side and the right side of the cover body (12), a collecting box (14) is fixedly connected to the top of the box (1), a first motor (8) is fixedly connected to the bottom of the electric sliding block (14), a limiting block (16) is fixedly connected to the bottom of the collecting box (14), a limiting block (16) is fixedly connected to the left side of the inner side of the electric sliding block (16), an exhaust fan (18) is fixedly arranged in the collecting box (14).
2. The protective structure of an aircraft aluminum plate cutter according to claim 1, wherein: the utility model discloses a motor, including box (1) right side fixed mounting, motor (19) No. two, the output shaft fixedly connected with threaded rod (20) of motor (19) No. two, the outside threaded connection of threaded rod (20) has screw thread piece (21), the top fixedly connected with connecting block (22) of screw thread piece (21), the top fixedly connected with U template (23) of connecting block (22), the equal fixedly connected with of the left and right sides of U template (23) inner wall is fixed plate (24) that the quantity is two, and the top is two equal threaded connection in inside of fixed plate (24) has bolt (25), two equal fixedly connected with limiting plate (26) in bottom of bolt (25), the interior bottom sliding connection of U template (23) has cabin body (27).
3. The protective structure of an aircraft aluminum plate cutter according to claim 1, wherein: the utility model discloses a box, including box (1) and slider (13), the left and right sides of box (1) inner wall has all seted up a spout, the inside of a spout and the outside sliding connection of a slider (5), no. two spouts have been seted up to the inside of connection shell (11), the inside of No. two spouts and the outside sliding connection of No. two sliders (13).
4. The protective structure of an aircraft aluminum plate cutter according to claim 1, wherein: limiting grooves are formed in the left side and the right side of the inner wall of the collecting box (14), and the inside of each limiting groove is in sliding connection with the outer side of each limiting block (17).
5. The protective structure of an aircraft aluminum plate cutter according to claim 1, wherein: the top of collection box (14) has seted up the venthole, the one end of flexible hose (15) runs through and extends to the inside of cover body (12).
6. The protective structure of an aircraft aluminum plate cutter according to claim 1, wherein: the inside of the connecting shell (11) is provided with a sliding through hole, and the inside of the sliding through hole is in sliding connection with the outer side of the cover body (12).
7. The protective structure of an aviation aluminum plate cutting machine according to claim 2, wherein: rectangular through holes are formed in the top of the box body (1), and the size of each rectangular through hole is matched with the size of the connecting block (22).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202322339619.2U CN220660132U (en) | 2023-08-30 | 2023-08-30 | Protective structure of aviation aluminum plate cutting machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202322339619.2U CN220660132U (en) | 2023-08-30 | 2023-08-30 | Protective structure of aviation aluminum plate cutting machine |
Publications (1)
Publication Number | Publication Date |
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CN220660132U true CN220660132U (en) | 2024-03-26 |
Family
ID=90329412
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202322339619.2U Active CN220660132U (en) | 2023-08-30 | 2023-08-30 | Protective structure of aviation aluminum plate cutting machine |
Country Status (1)
Country | Link |
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CN (1) | CN220660132U (en) |
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2023
- 2023-08-30 CN CN202322339619.2U patent/CN220660132U/en active Active
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