CN210147270U - Cutting device is used in aviation private cable processing - Google Patents
Cutting device is used in aviation private cable processing Download PDFInfo
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- CN210147270U CN210147270U CN201920880416.5U CN201920880416U CN210147270U CN 210147270 U CN210147270 U CN 210147270U CN 201920880416 U CN201920880416 U CN 201920880416U CN 210147270 U CN210147270 U CN 210147270U
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- fixed
- machine body
- aviation
- cutting device
- wire
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- 238000005520 cutting process Methods 0.000 title claims abstract description 32
- 238000003698 laser cutting Methods 0.000 claims abstract description 34
- 238000003754 machining Methods 0.000 claims description 2
- 230000002035 prolonged effect Effects 0.000 abstract description 8
- 238000005299 abrasion Methods 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 abstract description 4
- 230000001681 protective effect Effects 0.000 abstract description 4
- 230000003139 buffering effect Effects 0.000 abstract description 2
- 230000004075 alteration Effects 0.000 description 1
- 239000000084 colloidal system Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a cutting device for aviation special cable processing, which comprises a machine body, an operation box, a lead, a fixing part and a cross beam, wherein two supporting blocks which are distributed relatively are fixed at the bottom end of the cross beam, the supporting blocks can move back and forth on the machine body, a laser which can move left and right is installed on the cross beam, and a laser cutting head is fixed on the front surface of the laser through the fixing part; the utility model solves the problem of inconvenient fastening when cutting aviation special cables in the prior art through the designed clamping assembly, thereby being beneficial to better cutting the aviation special cables and improving the cutting efficiency of the aviation special cables; the protective pad is adhered to the contact surface of the laser cutting head and the fixing piece, so that the protective pad is beneficial to protecting the laser cutting head, the abrasion of the laser cutting head is reduced, and the service life of the laser cutting head is prolonged; through set up the support buffering subassembly on wire and support ring, slowed down the load that the wire received, prolonged the life of wire.
Description
Technical Field
The utility model belongs to the technical field of aviation private cable processing, concretely relates to cutting device is used in aviation private cable processing.
Background
When the aviation special cable is processed, the aviation special cable needs to be cut, and a laser cutting machine is often used for cutting the aviation special cable. The laser of the laser cutting machine can move left and right on the cross beam, and the supporting block below the cross beam can move back and forth on the machine body.
The existing cutting device for processing aviation-dedicated cables has the following defects when in use:
1. when the laser cutting head is fixed by the fixing part, the laser cutting head is not protected;
2. when the aviation special cable is cut, the cable is not fastened;
3. when the operation box is connected with the machine body through a wire, the load of the wire is not easy to buffer.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a cutting device for aviation special cable processing, which solves the problem that the laser cutting head provided in the background technology is not enough in protection when the laser cutting head is fixed by a fixing part; when the aviation special cable is cut, the cable is not fastened; when the operation box is connected with the machine body through a wire, the load problem of the wire is not easy to buffer.
In order to achieve the above object, the utility model provides a following technical scheme: a cutting device for machining a cable special for aviation comprises a machine body, an operation box, a conducting wire, a fixing part and a cross beam, wherein two supporting blocks which are distributed oppositely are fixed at the bottom end of the cross beam, the supporting blocks can move back and forth on the machine body, a laser capable of moving left and right is installed on the cross beam, a laser cutting head is fixed on the front surface of the laser through the fixing part, a cutting table is arranged at the top of the machine body, the operation box is located on one side of the machine body, a supporting rod and a supporting ring are further arranged between the machine body and the operation box, the supporting ring is fixed at the top of the supporting rod, one end of the conducting wire is connected with the operation box, the other end of the conducting wire penetrates through the supporting ring to be connected with the machine body, two upright columns which are distributed oppositely are fixed at the top of the cutting table, clamping components, a nut screwed with the screw thread of the screw rod is fixed in the through hole, a clamping block is fixed at one end of the screw rod, and a bearing is arranged at the joint of the clamping block and the screw rod.
Preferably, the other end of the screw rod is fixed with a knob.
Preferably, a protection pad is fixed on the contact surface of the laser cutting head and the fixing piece.
Preferably, be provided with the support buffer assembly on wire and the support ring, this support buffer assembly includes movable block, fixed slot and spring, the inner wall at the support ring is seted up to the fixed slot, the one end embedding fixed slot of movable block, the other end stretch out the fixed slot to can offset with the wire, the one end of spring is connected with the embedding end terminal surface of movable block, and the other end is connected with the tank bottom of fixed slot.
Preferably, two chutes that distribute relatively are seted up to the medial surface of fixed slot, the embedding end lateral surface of movable block be provided with spout assorted gleitbretter, the port department of spout is fixed with the spacing piece.
Preferably, the end face of the extending end of the movable block is of an arc structure.
Preferably, four corners of the bottom of the machine body are fixed with supporting feet.
Preferably, the front surface of the operation box is hinged with an access door.
Compared with the prior art, the beneficial effects of the utility model are that:
(1) by the designed clamping assembly, the problem that the aviation special cable is inconvenient to fasten in the traditional cutting process is solved, so that the aviation special cable can be better cut, and the aviation special cable cutting efficiency is improved;
(2) the protective pad is adhered to the contact surface of the laser cutting head and the fixing piece, so that the protective pad is beneficial to protecting the laser cutting head, the abrasion of the laser cutting head is reduced, and the service life of the laser cutting head is prolonged;
(3) through set up the support buffering subassembly on wire and support ring, slowed down the load that the wire received, prolonged the life of wire.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the present invention in a partial cross-sectional structure;
FIG. 3 is a side view of the support ring and the support rod of the present invention;
fig. 4 is a schematic view of the structure of fig. 3 in partial section according to the present invention;
fig. 5 is an enlarged schematic structural view of the region a in fig. 4 according to the present invention;
FIG. 6 is a schematic side view of the fixing member of the present invention;
in the figure: 1. a body; 2. supporting legs; 3. a support bar; 4. an access door; 5. an operation box; 6. a support ring; 7. a wire; 8. a laser; 9. a fixing member; 10. a column; 11. a bearing; 12. a screw rod; 13. cutting table; 14. a support block; 15. a cross beam; 16. a laser cutting head; 17. a knob; 18. a nut; 19. a clamping block; 20. a movable block; 21. a limiting sheet; 22. a chute; 23. fixing grooves; 24. a spring; 25. sliding blades; 26. a pad.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1, fig. 2, fig. 3, fig. 4, fig. 5 and fig. 6, the present invention provides a technical solution: a cutting device for processing aviation special cables comprises a machine body 1, an operation box 5, a wire 7, a fixing part 9 and a cross beam 15, wherein two supporting blocks 14 which are distributed oppositely are fixed at the bottom end of the cross beam 15, the supporting blocks 14 can move back and forth on the machine body 1, a laser 8 which can move left and right is installed on the cross beam 15, a laser cutting head 16 is fixed on the front surface of the laser 8 through the fixing part 9, the laser cutting head 16 is used for carrying out laser cutting on the aviation special cables, a cutting table 13 is arranged at the top of the machine body 1, the operation box 5 is positioned at one side of the machine body 1, a supporting rod 3 and a supporting ring 6 are further arranged between the machine body 1 and the operation box 5, the supporting ring 6 is fixed at the top of the supporting rod 3, one end of the wire 7 is connected with the operation box 5, the other end of the wire penetrates, be provided with clamping component on this stand 10, this clamping component includes lead screw 12, nut 18 and clamp splice 19, the perforation has been seted up on the surface of stand 10, this perforation internal fixation has the nut 18 of closing with lead screw 12 screw thread soon, the one end of lead screw 12 is fixed with clamp splice 19, and the junction of clamp splice 19 and lead screw 12 is provided with bearing 11, the other end of lead screw 12 is fixed with knob 17, in using, rotate knob 17, knob 17 drives lead screw 12 and rotates, it impels to drive clamp splice 19 when lead screw 12 rotates, utilize two opposite clamp splices 19 to fix the aviation private cable who treats the cutting, the inconvenient problem of fastening when having solved aviation private cable cutting among the tradition, thereby help better cutting aviation private cable, improve the efficiency of aviation private cable cutting.
In this embodiment, it is preferable that a protection pad 26 is bonded to a contact surface of the laser cutting head 16 and the fixing member 9, when the laser cutting head is used, the protection pad 26 is bonded to the fixing member 9 in a colloid bonding manner, and when the laser cutting head 16 is fastened by the fixing member 9, the protection pad 26 is used for protecting the laser cutting head 16, so that abrasion of the laser cutting head 16 is reduced, and the service life of the laser cutting head 16 is prolonged.
In this embodiment, preferably, the wire 7 and the support ring 6 are provided with a supporting buffer assembly, the supporting buffer assembly includes a movable block 20, a fixed groove 23 and a spring 24, the fixed groove 23 is disposed on an inner wall of the support ring 6, one end of the movable block 20 is embedded into the fixed groove 23, the other end of the movable block 20 extends out of the fixed groove 23 and can be abutted against the wire 7, one end of the spring 24 is connected with an end face of the embedded end of the movable block 20, the other end of the spring is connected with a groove bottom of the fixed groove 23, two sliding grooves 22 are disposed on an inner side surface of the fixed groove 23, a sliding piece 25 matched with the sliding groove 22 is disposed on an outer side surface of the embedded end of the movable block 20, a limiting piece 21 is fixed at a port of the sliding groove 22, when in use, the wire 7 applies pressure to the movable block 20, the spring 24 is compressed by the movable block, the load borne by the lead 7 is relieved, and the service life of the lead 7 is prolonged.
In this embodiment, preferably, the end surface of the extending end of the movable block 20 is an arc-shaped structure, so that the movable block 20 can better support the wire 7.
In this embodiment, preferably, the four corners of the bottom of the machine body 1 are fixed with the supporting legs 2, so as to support the machine body 1.
In this embodiment, it is preferred, the front surface of control box 5 articulates there is access door 4, is convenient for utilize access door 4 to protect the components and parts in the control box 5, also is convenient for open access door 4, overhauls the components and parts of its inside and maintains.
The utility model discloses a theory of operation and use flow: when the laser cutting head 16 is fastened through the fixing part 9, the protection pad 26 is used for protecting the laser cutting head 16, so that the abrasion of the laser cutting head 16 is reduced, and the service life of the laser cutting head 16 is prolonged;
one end of the wire 7 is connected with the operation box 5, and the other end of the wire passes through the support ring 6 to be connected with the machine body 1, when the device is used, the wire 7 applies pressure to the movable block 20, the spring 24 is compressed after the movable block 20 is pressed, the spring 24 has a reset function after being compressed, the movable block 20 is pushed upwards to abut against the wire 7, the load borne by the wire 7 is relieved, and the service life of the wire 7 is prolonged;
the knob 17 is rotated, the knob 17 drives the screw rod 12 to rotate, the screw rod 12 drives the clamping blocks 19 to advance when rotating, and the aviation special cable to be cut is fixed by utilizing the two opposite clamping blocks 19;
and the laser cutting head 16 on the laser 8 cuts the fastened aviation special cable through the operation box 5.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (8)
1. A cutting device for machining aviation special cables comprises a machine body (1), an operation box (5), a wire (7), a fixing piece (9) and a cross beam (15), wherein two supporting blocks (14) which are distributed oppositely are fixed at the bottom end of the cross beam (15), the supporting blocks (14) can move back and forth on the machine body (1), a laser (8) which can move left and right is installed on the cross beam (15), a laser cutting head (16) is fixed on the front surface of the laser (8) through the fixing piece (9), a cutting table (13) is arranged at the top of the machine body (1), the operation box (5) is located on one side of the machine body (1), a supporting rod (3) and a supporting ring (6) are further arranged between the machine body (1) and the operation box (5), the supporting ring (6) is fixed at the top of the supporting rod (3), one end of the wire (7) is connected with the operation box (5), the other end passes support ring (6) and is connected with organism (1), its characterized in that: the top of cutting bed (13) is fixed with two stand (10) that distribute relatively, is provided with clamping assembly on this stand (10), and this clamping assembly includes lead screw (12), nut (18) and clamp splice (19), the perforation has been seted up on the surface of stand (10), and this perforation internal fixation has nut (18) with lead screw (12) screw thread closure, the one end of lead screw (12) is fixed with clamp splice (19), and the junction of clamp splice (19) and lead screw (12) is provided with bearing (11).
2. The cutting device for aviation dedicated cable processing according to claim 1, wherein: and a knob (17) is fixed at the other end of the screw rod (12).
3. The cutting device for aviation dedicated cable processing according to claim 1, wherein: and a protection pad (26) is fixed on the contact surface of the laser cutting head (16) and the fixing piece (9).
4. The cutting device for aviation dedicated cable processing according to claim 1, wherein: be provided with the support buffer unit on wire (7) and support ring (6), this support buffer unit includes movable block (20), fixed slot (23) and spring (24), the inner wall in support ring (6) is seted up in fixed slot (23), the one end embedding fixed slot (23) of movable block (20), fixed slot (23) are stretched out to the other end to can offset with wire (7), the one end of spring (24) is connected with the embedding end terminal surface of movable block (20), and the other end is connected with the tank bottom of fixed slot (23).
5. The cutting device for aviation dedicated cable processing according to claim 4, wherein: two chutes (22) which are distributed relatively are arranged on the inner side surface of the fixing groove (23), an embedding end outer side surface of the movable block (20) is provided with a sliding piece (25) matched with the chutes (22), and limiting pieces (21) are fixed at the port positions of the chutes (22).
6. The cutting device for aviation dedicated cable processing according to claim 5, wherein: the end face of the extending end of the movable block (20) is of an arc-shaped structure.
7. The cutting device for aviation dedicated cable processing according to claim 1, wherein: supporting legs (2) are fixed at four corners of the bottom of the machine body (1).
8. The cutting device for aviation dedicated cable processing according to claim 1, wherein: the front surface of the operation box (5) is hinged with an access door (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920880416.5U CN210147270U (en) | 2019-06-12 | 2019-06-12 | Cutting device is used in aviation private cable processing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920880416.5U CN210147270U (en) | 2019-06-12 | 2019-06-12 | Cutting device is used in aviation private cable processing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210147270U true CN210147270U (en) | 2020-03-17 |
Family
ID=69762596
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920880416.5U Expired - Fee Related CN210147270U (en) | 2019-06-12 | 2019-06-12 | Cutting device is used in aviation private cable processing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210147270U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113280021A (en) * | 2021-05-11 | 2021-08-20 | 成都正山机械制造有限公司 | Integrated proportional valve control method |
| CN117428349A (en) * | 2023-12-14 | 2024-01-23 | 深圳市润泽机器人有限公司 | Robot for cutting arc-shaped metal plates of ship bodies |
-
2019
- 2019-06-12 CN CN201920880416.5U patent/CN210147270U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113280021A (en) * | 2021-05-11 | 2021-08-20 | 成都正山机械制造有限公司 | Integrated proportional valve control method |
| CN117428349A (en) * | 2023-12-14 | 2024-01-23 | 深圳市润泽机器人有限公司 | Robot for cutting arc-shaped metal plates of ship bodies |
| CN117428349B (en) * | 2023-12-14 | 2024-03-19 | 深圳市润泽机器人有限公司 | Robot for cutting arc-shaped metal plates of ship bodies |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200317 |