CN214603689U - Multi-wire cutting device for aviation mould - Google Patents
Multi-wire cutting device for aviation mould Download PDFInfo
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- CN214603689U CN214603689U CN202120972099.7U CN202120972099U CN214603689U CN 214603689 U CN214603689 U CN 214603689U CN 202120972099 U CN202120972099 U CN 202120972099U CN 214603689 U CN214603689 U CN 214603689U
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Abstract
The utility model relates to a cutting device technical field discloses an aviation mould multi-thread cutting device, the on-line screen storage device comprises a base, base upper surface left side fixed mounting has the support curb plate of L type, and base upper surface right side fixed mounting has the mounting panel, and the mounting panel mid-rotation is installed the left end and is rotated the lead screw that is connected to on the support curb plate, and slidable mounting has the horizontally movable plate on the lead screw, the equal fixed mounting in side has two sets of bilateral symmetry distribution's supporting shoe around supporting curb plate horizontal segment upper surface. The utility model has the advantages that: the use quantity of leading wheel has been reduced, reduces the volume of device, and it is high to have reduced the operation energy consumption, is favorable to improving cutting efficiency, can be according to the actual cutting length of the actual size control tangent line of cutting the object, reduces the probability that the line of cut produced bending deformation easily when using, reduces the loss of line of cut, is favorable to using for a long time.
Description
Technical Field
The utility model relates to a cutting device technical field specifically is an aviation mould multi-wire cutting device.
Background
The multi-line cutting technology is to grind a workpiece by using abrasive grains or mortar grains of a cutting line by means of a cutting line net running at a high speed. Compared with the early-stage one-by-one cutting process using the inner/outer circular blades, the multi-line cutting process has the advantages of less material loss and high cutting efficiency, and is widely applied to processing of hard and brittle materials such as glass, ceramics, crystals, silicon materials, sapphire and the like.
Among traditional aeronautical mould multi-wire cutting device, the wiring route of line of cut is located the actinobacillus wheel for one end, the other end passes through a plurality of leading wheels or reverse wheel, lay and form the cutting wire net on the home roll, pass through a plurality of leading wheels or reverse wheel and finally reach the take-up pulley, the use quantity of leading wheel or reverse wheel is many, lead to its bulky, the running energy consumption is high, it is long consuming time to lay wire and tear open, be unfavorable for improving cutting efficiency, and can't change the cutting length of line of cut among the current aeronautical mould multi-wire cutting device, lead to the actual cutting length that can't control the line of cut according to the actual size of cutting object, thereby lead to the line of cut to produce bending deformation easily when using, accelerate the loss of line of cut, reduce the live time of line of cut, be unfavorable for permanent use.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aeromould multi-thread cutting device to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
a multi-wire cutting device for an aviation die comprises a base, wherein an L-shaped supporting side plate is fixedly arranged on the left side of the upper surface of the base, a mounting plate is fixedly arranged on the right side of the upper surface of the base, a lead screw with the left end rotatably connected to the supporting side plate is rotatably arranged in the middle of the mounting plate, a horizontal moving plate is slidably arranged on the lead screw, two groups of supporting blocks which are symmetrically distributed left and right are fixedly arranged on the front side and the rear side of the upper surface of a horizontal section of the supporting side plate, a wire releasing roller and a wire collecting roller which are transversely distributed are respectively rotatably arranged on the two groups of supporting blocks on the same side, a U-shaped bracket with a downward opening is fixedly arranged in the middle of the upper surface of the supporting side plate, a vertical second electric telescopic rod is fixedly arranged on the lower surface of the horizontal section of the bracket, a top plate penetrating through the supporting side plate is fixedly arranged at the lower end of the second electric telescopic rod, and a plurality of groups of first connecting plates which are symmetrically distributed in the center are fixedly arranged on the lower surface of the top plate, the first connecting plate end is fixedly provided with a frame-shaped mounting frame, the two ends of the mounting frame are rotatably provided with guide rollers, the mounting frame is provided with two groups of symmetrically distributed moving blocks in a sliding manner, and the lower ends of the moving blocks are rotatably provided with the guide rollers.
As a further aspect of the present invention: the mounting plate left surface fixed mounting has two sets of slide bars that are located the lateral symmetry distribution around the lead screw and are parallel with the lead screw, and slide bar left end fixed connection is to supporting on the curb plate and the equal level of slide bar passes the movable plate, and the lead screw right-hand member passes mounting panel and fixedly connected with fixed mounting at the first motor on base upper surface right side.
As a further aspect of the present invention: the middle of the lower surface of the top plate is fixedly provided with a vertical first electric telescopic rod, the lower end of the first electric telescopic rod is fixedly provided with a connecting block, the connecting block is rotatably provided with two sets of second connecting plates which are distributed in a bilateral symmetry manner, and one end, far away from the connecting block, of each second connecting plate is rotatably connected with the moving block.
As a further aspect of the present invention: the middle part of the upper surface of the horizontal section of the supporting side plate is provided with a positioning part: two groups of guide rollers which are symmetrically distributed on the inner side of the threading hole are rotatably arranged on the lower surface of the horizontal section of the supporting side plate.
As a further aspect of the present invention: the utility model discloses a supporting side board horizontal segment, including the curb plate, the curb plate is equipped with the deflector, the curb plate is equipped with the telescopic link that the fore-and-aft direction distributes around supporting the curb plate horizontal segment, side middle part fixed mounting has the deflector, deflector medial surface upper portion fixed mounting has the telescopic link that distributes along the fore-and-aft direction, the one end fixed mounting that the deflector was kept away from to the telescopic link has the U template, rotate on the U template and install the direction gyro wheel, deflector medial surface upper portion fixed mounting has the spring that distributes around the telescopic link, the one end fixed connection that the deflector was kept away from to the spring has the shower nozzle on the U template, deflector medial surface lower part fixed mounting.
As a further aspect of the present invention: the pay-off roller with receive the equal fixedly connected with in line roller left end and be located the left second motor of support curb plate upper surface, be provided with the line of cut on the pay-off roller, the line of cut distributes and the line of cut keeps away from the one end fixed connection of pay-off roller along guide roller outside surface to receive on the line roller.
Compared with the prior art, the beneficial effects of the utility model are that: by arranging the guide roller and the spring, the second motor drives the pay-off roller and the take-up roller to rotate simultaneously, so that the cutting line rotates around the guide roller, the second electric telescopic rod drives the top plate to move downwards, the top plate enables the cutting line of the lower horizontal section to cut a die, the tensioning degree of the cutting line is ensured under the action of the spring, the using amount of the guide roller is reduced, the size of the device is reduced, the operation energy consumption is reduced, and the cutting efficiency is improved; through setting up the movable block, second connecting plate and electric telescopic handle, thereby drive the connecting block through electric telescopic handle and reciprocate thereby make the movable block move to the inboard or outside simultaneously and change the cutting of the horizontal segment length of line of cut in order to be suitable for not unidimensional mould, can be according to the actual cutting length of the actual size control line of cut object, reduce the line of cut and produce the probability of bending deformation easily when using, reduce the loss of line of cut, be favorable to using for a long time.
Drawings
Fig. 1 is a schematic structural diagram of an aviation die multi-wire cutting device.
Fig. 2 is a right side view of the multi-wire cutting device for the aviation die.
Fig. 3 is a schematic structural diagram of a mounting rack in the multi-wire cutting device for the aviation die.
Wherein: 1. the automatic wire drawing machine comprises a base, 2 supporting side plates, 3 mounting plates, 4 sliding rods, 5 lead screws, 6 moving plates, 7 first motors, 8 supporting blocks, 9 wire paying-off rollers, 10 wire taking-up rollers, 11 second motors, 12 wire threading holes, 13 guide rollers, 14 guide plates, 15 telescopic rods, 16 springs, 17U-shaped plates, 18 first electric telescopic rods, 19 spray heads, 20 supports, 21 second electric telescopic rods, 22 top plates, 23 first connecting plates, 24 mounting frames, 25 moving blocks, 26 connecting blocks, 27 second connecting plates and 28 cutting wires.
Detailed Description
It should be noted that, in the present invention, the embodiments and features of the embodiments may be combined with each other without conflict.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are used merely for convenience of description and for simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention. Furthermore, the terms "first", "second", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first," "second," etc. may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.
The present invention will be described in detail below with reference to the accompanying drawings in conjunction with embodiments.
Example one
Referring to fig. 1-3, a multi-line cutting device for an aviation mold comprises a base 1, wherein an L-shaped supporting side plate 2 is fixedly installed on the left side of the upper surface of the base 1, a mounting plate 3 is fixedly installed on the right side of the upper surface of the base 1, a screw rod 5 with the left end rotatably connected to the supporting side plate 2 is rotatably installed in the middle of the mounting plate 3, a horizontal moving plate 6 is slidably installed on the screw rod 5, two sets of slide bars 4 which are symmetrically distributed on the front and back sides of the screw rod 5 and parallel to the screw rod 5 are fixedly installed on the left side of the mounting plate 3, the left ends of the slide bars 4 are fixedly connected to the supporting side plate 2, the slide bars 4 horizontally penetrate through the moving plate 6, the right end of the screw rod 5 penetrates through the mounting plate 3 and is fixedly connected with a first motor 7 which is fixedly installed on the right side of the upper surface of the supporting side plate 2, two sets of supporting blocks 8 which are symmetrically distributed on the same side and on the front and back sides of the upper surface of the horizontal section of the supporting side plate 2 are fixedly installed with two sets of supporting blocks 8, a pay-off roller 9 and take-up roller 10 which are transversely distributed respectively, support 2 horizontal segment upper surface middle parts of curb plate outside and seted up and be located: the lower surface of the horizontal section of the supporting side plate 2 is rotatably provided with two groups of guide rollers 13 which are symmetrically distributed at the inner side of the threading hole 12, the middle part of the upper surface of the supporting side plate 2 is fixedly provided with a U-shaped bracket 20 with a downward opening, the lower surface of the horizontal section of the bracket 20 is fixedly provided with a vertical second electric telescopic rod 21, the lower end of the second electric telescopic rod 21 is fixedly provided with a top plate 22 which penetrates through the supporting side plate 2, the lower surface of the top plate 22 is fixedly provided with a plurality of groups of first connecting plates 23 which are symmetrically distributed, the ends of the first connecting plates 23 are jointly and fixedly provided with a frame-shaped mounting frame 24, both ends of the mounting frame 24 are rotatably provided with the guide rollers 13, two groups of symmetrically distributed moving blocks 25 are slidably mounted on the mounting frame 24, the lower ends of the moving blocks 25 are rotatably provided with the guide rollers 13, and the middle part of the lower surface of the top plate 22 is fixedly provided with the vertical first electric telescopic rod 18, the lower end of the first electric telescopic rod 18 is fixedly provided with a connecting block 26, the connecting block 26 is rotatably provided with two sets of second connecting plates 27 which are distributed in bilateral symmetry, and one ends, far away from the connecting block 26, of the second connecting plates 27 are rotatably connected with the moving block 25.
Example two
On the basis of the first embodiment, the middle parts of the front side and the rear side of the horizontal section of the supporting side plate 2 are fixedly provided with the guide plates 14, the upper parts of the inner side surfaces of the guide plates 14 are fixedly provided with the telescopic rods 15 distributed along the front-rear direction, one ends, far away from the guide plates 14, of the telescopic rods 15 are fixedly provided with the U-shaped plates 17, the U-shaped plates 17 are rotatably provided with the guide rollers 13, the upper parts of the inner side surfaces of the guide plates 14 are fixedly provided with the springs 16 distributed around the telescopic rods 15, one ends, far away from the guide plates 14, of the springs 16 are fixedly connected to the U-shaped plates 17, the lower parts of the inner side surfaces of the guide plates 14 are fixedly provided with the spray nozzles 19, the pay-off rollers 9 and the take-up rollers 10 are fixedly connected with the second motors 11 positioned on the left side of the upper surface of the supporting side plate 2, the pay-off rollers 9 are provided with the cutting lines 28, and the cutting lines 28 are distributed along the outer side surfaces of the guide rollers 13 and one ends, far away from the pay-off rollers 9, of the cutting lines 28, are fixedly connected to the take-up rollers 10.
The utility model discloses a theory of operation is: place the aeromodelling that will need the cutting on movable plate 6, first motor 7 drives lead screw 5 and rotates and then make movable plate 6 drive aeromodelling to the left side and move, open second motor 11, second motor 11 drives unwrapping wire roller 9 and receipts line roller 10 and rotates simultaneously, thereby make line of cut 28 rotate around guide roller 13, second electric telescopic handle 21 drives roof 22 and moves down, roof 22 thereby make below horizontal segment line of cut 28 cut the mould, thereby it reciprocates to drive connecting block 26 through first electric telescopic handle 18 and makes movable block 25 move to the inboard or outside simultaneously thereby change the horizontal segment length of line of cut 28 in order to be suitable for the cutting of not unidimensional mould, guarantee the tensioning degree of line of cut 28 under the effect of spring 16, it is lubricated to want line of cut 28 injection cutting fluid cooling down to want through shower nozzle 19.
Although the preferred embodiments of the present patent have been described in detail, the present patent is not limited to the above embodiments, and various changes can be made without departing from the spirit of the present patent within the knowledge of those skilled in the art.
Claims (6)
1. The utility model provides an aviation mould multi-thread cutting device, includes base (1), its characterized in that, base (1) upper surface left side fixed mounting has the support curb plate (2) of L type, and base (1) upper surface right side fixed mounting has mounting panel (3), and mounting panel (3) middle part is rotated and is installed lead screw (5) that the left end rotates and is connected to support curb plate (2), and slidable mounting has horizontal movable plate (6) on lead screw (5), support curb plate (2) horizontal segment upper surface front and back side all fixed mounting have two sets of bilateral symmetry distributed supporting shoe (8), and lateral distribution's unwrapping wire roller (9) and receipts line roller (10) are installed in the rotation respectively to homonymy two sets of supporting shoe (8), support curb plate (2) upper surface middle part fixed mounting has U type support (20) that open side down, and support (20) horizontal segment lower surface fixed mounting has vertical second electric telescopic handle (21), second electric telescopic handle (21) lower extreme fixed mounting has roof (22) of passing support curb plate (2), roof (22) lower surface fixed mounting has first connecting plate (23) of multiunit central symmetric distribution, the common fixed mounting in first connecting plate (23) end has mounting bracket (24) of frame type, all the rotational mounting has guide roller (13) at mounting bracket (24) both ends, slidable mounting has movable block (25) of two sets of symmetric distributions on mounting bracket (24), guide roller (13) are installed in movable block (25) lower extreme rotation.
2. The multi-wire cutting device for the aviation dies according to claim 1, wherein two groups of sliding rods (4) which are symmetrically distributed at the front side and the rear side of the screw rod (5) and are parallel to the screw rod (5) are fixedly installed on the left side surface of the installation plate (3), the left ends of the sliding rods (4) are fixedly connected to the supporting side plate (2), the sliding rods (4) horizontally penetrate through the moving plate (6), the right ends of the screw rod (5) penetrate through the installation plate (3), and the first motor (7) fixedly installed on the right side of the upper surface of the base (1) is fixedly connected.
3. The multi-wire cutting device for the aviation dies according to claim 1, wherein a vertical first electric telescopic rod (18) is fixedly installed in the middle of the lower surface of the top plate (22), a connecting block (26) is fixedly installed at the lower end of the first electric telescopic rod (18), two groups of second connecting plates (27) which are distributed in a bilateral symmetry mode are rotatably installed on the connecting block (26), and one end, far away from the connecting block (26), of each second connecting plate (27) is rotatably connected with a moving block (25).
4. The multi-wire cutting device for the aviation dies as claimed in claim 1, wherein the outer side of the middle part of the upper surface of the horizontal section of the supporting side plate (2) is provided with a cutting blade which is positioned at one of the following positions: the lower surfaces of the horizontal sections of the supporting side plates (2) are rotatably provided with two groups of guide rollers (13) which are symmetrically distributed on the inner sides of the threading holes (12) through threading holes (12) below the paying-off roller (9) and the take-up roller (10).
5. The multi-wire cutting device for the aviation dies according to claim 1 or 4, wherein a guide plate (14) is fixedly mounted in the middle of the front side surface and the rear side surface of the horizontal section of the supporting side plate (2), telescopic rods (15) distributed in the front-rear direction are fixedly mounted on the upper portion of the inner side surface of the guide plate (14), a U-shaped plate (17) is fixedly mounted at one end, away from the guide plate (14), of each telescopic rod (15), guide rollers (13) are rotatably mounted on the U-shaped plate (17), springs (16) distributed around the telescopic rods (15) are fixedly mounted on the upper portion of the inner side surface of the guide plate (14), one end, away from the guide plate (14), of each spring (16) is fixedly connected to the U-shaped plate (17), and a spray nozzle (19) is fixedly mounted on the lower portion of the inner side surface of the guide plate (14).
6. The multi-wire cutting device for the aviation dies according to claim 1, wherein the left ends of the pay-off roller (9) and the take-up roller (10) are fixedly connected with a second motor (11) which is positioned on the left side of the upper surface of the supporting side plate (2), cutting wires (28) are arranged on the pay-off roller (9), the cutting wires (28) are distributed along the outer side surface of the guide roller (13), and one end, far away from the pay-off roller (9), of each cutting wire (28) is fixedly connected to the take-up roller (10).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202120972099.7U CN214603689U (en) | 2021-05-08 | 2021-05-08 | Multi-wire cutting device for aviation mould |
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CN202120972099.7U CN214603689U (en) | 2021-05-08 | 2021-05-08 | Multi-wire cutting device for aviation mould |
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CN214603689U true CN214603689U (en) | 2021-11-05 |
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CN202120972099.7U Active CN214603689U (en) | 2021-05-08 | 2021-05-08 | Multi-wire cutting device for aviation mould |
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2021
- 2021-05-08 CN CN202120972099.7U patent/CN214603689U/en active Active
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