CN219881479U - Aviation material cutting device - Google Patents
Aviation material cutting device Download PDFInfo
- Publication number
- CN219881479U CN219881479U CN202321354021.4U CN202321354021U CN219881479U CN 219881479 U CN219881479 U CN 219881479U CN 202321354021 U CN202321354021 U CN 202321354021U CN 219881479 U CN219881479 U CN 219881479U
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- fixedly arranged
- workbench
- top surface
- motor
- screw
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- 239000000463 material Substances 0.000 title claims abstract description 36
- 239000002699 waste material Substances 0.000 claims abstract description 15
- 230000007246 mechanism Effects 0.000 claims abstract description 9
- 230000000694 effects Effects 0.000 abstract description 6
- 239000012141 concentrate Substances 0.000 abstract 1
- 239000011825 aerospace material Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 238000011161 development Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000009931 harmful effect Effects 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model discloses an aviation material cutting device which comprises a workbench, wherein a cutting mechanism is fixedly arranged on the top surface of the workbench, a movable clamping assembly is fixedly arranged on the top surface of the workbench, and a waste collection assembly is fixedly arranged at the bottom of the left side of the workbench. In the above-mentioned scheme, set up and remove clamping assembly, place aviation material on the bottom plate during the use, start electronic jar No. one and No. two electronic jars, carry out the centre gripping to aviation material, make a screw rod drive the vertical direction of movable plate and remove, no. two motors make cutting blade rotatory, begin to cut aviation material, it is rotatory to start No. three motors drive No. two screw rods, make the sliding block at the inside activity of base, reach the effect that can quick adjustment aviation material's position, set up waste collection subassembly, the fan can concentrate the sweeps that the cutting work produced into the sweeps fill, then the sweeps is by leading the sweeps fill and get into the collecting box, the effect that can collect the sweeps that produces during the cutting, it is convenient to carry out recycle to it.
Description
Technical Field
The utility model relates to the technical field of cutting devices, in particular to an aviation material cutting device.
Background
Aerospace materials refer to various materials used by aircrafts and power devices, accessories and instruments thereof, are one of decisive factors for the development of aerospace engineering technology, aerospace material science is also a branch of development in material science, and in the aerospace manufacturing process, cutting equipment is often required to cut the aerospace materials, but in actual use, the aerospace materials still have some defects, such as: fixed length cutting is required to be carried out on the same material in the aviation material processing process, when long parts such as structural rods are faced, adjustment on the horizontal position is required to be carried out frequently, usually, aviation materials are manually released from fixing by workers, are fixed after being adjusted to a proper position, and then the next cutting is completed, so that a great deal of time is required to be consumed to cut and complete the whole structural rod, and the working efficiency is low.
Disclosure of Invention
In order to overcome the above-mentioned drawbacks of the prior art, the embodiment of the present utility model provides an aviation material cutting device, so as to solve the problems that in the prior art, a fixed length of the same material is always required to be cut in the processing process of aviation materials, and when long parts such as structural rods are faced, adjustment on the horizontal position is required to be frequently performed, usually, a worker manually releases the fixation of the aviation material, adjusts the aviation material to a proper position, then fixes the aviation material, and then completes the next cutting, so that a great amount of time is required to be consumed to cut an entire structural rod, and the working efficiency is not high.
In order to solve the technical problems, the utility model provides the following technical scheme: the utility model provides an aviation material cutting device, includes the workstation, the top surface fixed mounting of workstation has cutting mechanism, the top surface fixed mounting of workstation has the removal clamping assembly, the left bottom fixed mounting of workstation has waste collection subassembly.
The cutting mechanism comprises a fixing frame, a sliding opening is formed in the right side of the fixing frame, a first motor is fixedly arranged on the top surface of the fixing frame, a first screw is fixedly connected with a driving shaft of the first motor, a movable plate is arranged on the outer surface of the first screw in a threaded mode, a second motor is fixedly arranged at the bottom of the movable plate, a cutting blade is detachably arranged on a driving shaft of the second motor, and a limiting block is fixedly arranged at the right end of the movable plate.
The bottom of the first screw is rotationally connected with the inside of the fixing frame, the outer surface of the limiting block is slidably connected with the outer surface of the sliding port, and the bottom surface of the fixing frame is fixedly connected with the top surface of the workbench.
The movable clamping assembly comprises a base, wherein a sliding strip is fixedly arranged on the inner surface of the base, a sliding block is slidably arranged on the outer surface of the sliding strip, a second screw rod is arranged on the inner thread of the sliding block, a third motor is fixedly connected with the right end of the second screw rod, a bottom plate is fixedly arranged on the top of the sliding block, a graduated scale is fixedly arranged on the top surface of the bottom plate, a first supporting plate is fixedly arranged on the outer surface of the first supporting plate, a first electric cylinder is fixedly arranged on the bottom end of the first electric cylinder, a second supporting plate is fixedly arranged on the top surface of the bottom plate, a second electric cylinder is fixedly arranged on the left side of the second supporting plate, and a second contact block is fixedly arranged on the left end of the second electric cylinder.
The outer surface of the second screw rod is movably connected with the inside of the base, the bottom surface of the base is fixedly connected with the top surface of the workbench, and the bottom surface of the third motor is fixedly connected with the top surface of the workbench.
The waste collection assembly comprises a chip guiding hopper, the bottom of the chip guiding hopper is fixedly connected with the top of the collection box, a filter screen is detachably arranged in the collection box, a fan is detachably arranged on the right side of the collection box, and the top end of the chip guiding hopper is fixedly connected with the bottom surface of the workbench.
The technical scheme of the utility model has the following beneficial effects:
in the above-mentioned scheme, set up and remove clamping assembly, place aviation material on the bottom plate during the use, start electronic jar and No. two electronic jars, make No. one contact piece and No. two contact piece laminating aviation material, carry out the centre gripping of level and vertical direction to aviation material, start a motor, make a screw rod drive movable plate vertical direction remove, start No. two motors and make cutting blade rotatory, begin to cut aviation material, after once cutting is accomplished, start No. three motors and drive No. two screw rods rotatory, make the sliding block at the inside activity of base, thereby drive aviation material horizontal migration, the cutting of the time of conveniently carrying out, reach the position that can fast adjustment aviation material, the effect of cutting is carried out the time conveniently, improve work efficiency greatly, set up waste collection subassembly, the fan is started, the sweeps that the wind opportunity produced cutting work is concentrated and is inhaled the sweeps fill, then the sweeps is got into the collecting box by the sweeps fill, the effect that can collect the sweeps that produces when cutting is convenient to carry out recycle to it is reached.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present utility model;
FIG. 2 is a schematic diagram of the overall internal structure of the present utility model;
FIG. 3 is a schematic view of a cutting mechanism according to the present utility model;
FIG. 4 is a schematic view of a movable clamping assembly according to the present utility model;
FIG. 5 is a schematic view of a waste collection assembly according to the present utility model.
[ reference numerals ]
1. A work table; 2. a cutting mechanism; 3. moving the clamping assembly; 4. a waste collection assembly; 21. a fixing frame; 22. a sliding port; 23. a motor I; 24. a first screw; 25. a moving plate; 26. a motor II; 27. a cutting blade; 28. a limiting block; 31. a base; 32. a slide bar; 33. a sliding block; 34. a second screw; 35. a third motor; 36. a bottom plate; 37. a graduated scale; 38. a first support plate; 39. a first electric cylinder; 310. a contact block I; 311. a second supporting plate; 312. a second electric cylinder; 313. a second contact block; 41. a chip guiding hopper; 42. a collection box; 43. a filter screen; 44. a blower.
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 provides an aviation material cutting device as shown in figures 1 to 5, which comprises a workbench 1, wherein a cutting mechanism 2 is fixedly arranged on the top surface of the workbench 1, a movable clamping assembly 3 is fixedly arranged on the top surface of the workbench 1, and a waste collection assembly 4 is fixedly arranged at the bottom of the left side of the workbench 1.
As shown in fig. 3, the cutting mechanism 2 includes a fixing frame 21, a sliding opening 22 is formed on the right side of the fixing frame 21, a first motor 23 is fixedly mounted on the top surface of the fixing frame 21, a first screw 24 is fixedly connected to a driving shaft of the first motor 23, a moving plate 25 is mounted on the outer surface of the first screw 24 in a threaded manner, a second motor 26 is fixedly mounted on the bottom of the moving plate 25, a cutting blade 27 is detachably mounted on the driving shaft of the second motor 26, a limiting block 28 is fixedly mounted on the right end of the moving plate 25, the bottom end surface of the first screw 24 is rotationally connected with the inside of the fixing frame 21, the outer surface of the limiting block 28 is slidingly connected with the outer surface of the sliding opening 22, and the bottom surface of the fixing frame 21 is fixedly connected with the top surface of the workbench 1; the cutting blade 27 is a consumable product, and needs to be replaced frequently in order to ensure the cutting quality, so the cutting blade 27 is detachably arranged on the driving shaft of the second motor 26, and the replacement is convenient.
As shown in fig. 4, the movable clamping assembly 3 includes a base 31, an inner surface of the base 31 is fixedly provided with a sliding strip 32, an outer surface of the sliding strip 32 is slidably provided with a sliding block 33, an inner thread of the sliding block 33 is provided with a second screw 34, a right end of the second screw 34 is fixedly connected with a third motor 35, a bottom plate 36 is fixedly provided at a top of the sliding block 33, a graduated scale 37 is fixedly provided at a top surface of the bottom plate 36, a first supporting plate 38 is fixedly provided at a top surface of the bottom plate 36, an electric cylinder 39 is fixedly provided at an outer surface of the first supporting plate 38, a first contact block 310 is fixedly provided at a bottom end of the first electric cylinder 39, a second supporting plate 311 is fixedly provided at a top surface of the bottom plate 36, a second electric cylinder 312 is fixedly provided at a left end of the second supporting plate 311, an outer surface of the second screw 34 is movably connected with an inner part of the base 31, a bottom surface of the base 31 is fixedly connected with a third motor 35, and a top surface of the bottom surface of the base 31 is fixedly connected with a top surface of the third motor 35 of the table 1; the graduated scale 37 can play the role of length reference when cutting work goes on, can make more accurate to the aviation material cutting.
As shown in fig. 5, the waste collection assembly 4 includes a chip guiding hopper 41, wherein the bottom of the chip guiding hopper 41 is fixedly connected with the top of a collection box 42, a filter screen 43 is detachably mounted in the collection box 42, a fan 44 is detachably mounted on the right side of the collection box 42, and the top end of the chip guiding hopper 41 is fixedly connected with the bottom surface of the workbench 1; the filter screen 43 sets up in the junction of collecting box 42 and fan 44, thereby effectively prevents that the sweeps from getting into fan 44, thereby avoids the piece to get into fan 44 and causes the harmful effect.
The working process of the utility model is as follows: the aviation material is placed on the bottom plate 36, the first electric cylinder 39 and the second electric cylinder 312 are started, the first contact block 310 and the second contact block 313 are attached to the aviation material, the aviation material is clamped in the horizontal direction and the vertical direction, the first motor 23 is started, the first screw 24 drives the moving plate 25 to move in the vertical direction, the second motor 26 is started to enable the cutting blade 27 to rotate, the aviation material starts to be cut, after one cutting is completed, the third motor 35 is started to drive the second screw 34 to rotate, the sliding block 33 moves in the base 31, the aviation material is driven to move horizontally, the next cutting is carried out, the fan 44 is started, the waste generated by the cutting work is intensively sucked into the waste guide bucket 41 by the fan 44, and then the waste is led into the collecting box 42 by the waste guide bucket 41, and the waste is collected.
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 (3)
1. The aviation material cutting device comprises a workbench, and is characterized in that a cutting mechanism is fixedly arranged on the top surface of the workbench, a movable clamping assembly is fixedly arranged on the top surface of the workbench, and a waste collection assembly is fixedly arranged at the bottom of the left side of the workbench; the cutting mechanism comprises a fixing frame, a sliding opening is formed in the right side of the fixing frame, a first motor is fixedly arranged on the top surface of the fixing frame, a first screw is fixedly connected to a driving shaft of the first motor, a movable plate is arranged on the outer surface of the first screw in a threaded manner, a second motor is fixedly arranged at the bottom of the movable plate, a cutting blade is detachably arranged on a driving shaft of the second motor, and a limiting block is fixedly arranged at the right end of the movable plate; the bottom of the first screw is rotationally connected with the inside of the fixing frame, the outer surface of the limiting block is in sliding connection with the outer surface of the sliding port, and the bottom surface of the fixing frame is fixedly connected with the top surface of the workbench; the movable clamping assembly comprises a base, a sliding strip is fixedly arranged on the inner surface of the base, a sliding block is slidably arranged on the outer surface of the sliding strip, a second screw is arranged on the inner thread of the sliding block, a third motor is fixedly connected with the right end of the second screw, a bottom plate is fixedly arranged on the top of the sliding block, a graduated scale is fixedly arranged on the top surface of the bottom plate, a first supporting plate is fixedly arranged on the top surface of the bottom plate, a first electric cylinder is fixedly arranged on the outer surface of the first supporting plate, a first contact block is fixedly arranged on the bottom end of the first electric cylinder, a second supporting plate is fixedly arranged on the top surface of the bottom plate, a second electric cylinder is fixedly arranged on the left side of the second supporting plate, and a second contact block is fixedly arranged on the left end of the second electric cylinder.
2. The airborne material cutting device of claim 1, wherein the outer surface of the second screw is movably connected with the interior of the base, the bottom surface of the base is fixedly connected with the top surface of the workbench, and the bottom surface of the third motor is fixedly connected with the top surface of the workbench.
3. The airborne material cutting device of claim 1, wherein the scrap collecting assembly comprises a scrap guiding hopper, the bottom of the scrap guiding hopper is fixedly connected with the top of the collecting box, a filter screen is detachably arranged in the collecting box, a fan is detachably arranged on the right side of the collecting box, and the top end of the scrap guiding hopper is fixedly connected with the bottom surface of the workbench.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321354021.4U CN219881479U (en) | 2023-05-31 | 2023-05-31 | Aviation material cutting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321354021.4U CN219881479U (en) | 2023-05-31 | 2023-05-31 | Aviation material cutting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219881479U true CN219881479U (en) | 2023-10-24 |
Family
ID=88398061
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321354021.4U Active CN219881479U (en) | 2023-05-31 | 2023-05-31 | Aviation material cutting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219881479U (en) |
-
2023
- 2023-05-31 CN CN202321354021.4U patent/CN219881479U/en active Active
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