CN209888509U

CN209888509U - Engraving machine integrated strong beam

Info

Publication number: CN209888509U
Application number: CN201920042404.5U
Authority: CN
Inventors: 邹俊; 苏冬明; 郭贺敏
Original assignee: Dongguan Dingling Precision Machinery Co Ltd
Current assignee: Dongguan Dingling Precision Machinery Co Ltd
Priority date: 2019-01-11
Filing date: 2019-01-11
Publication date: 2020-01-03
Anticipated expiration: 2029-01-11

Abstract

The utility model discloses a powerful crossbeam of engraver integrated into one piece, be two including quantity the equal fixed mounting in one side relative of bearing plate has the mounting. This powerful crossbeam of engraver integrated into one piece, crossbeam and mounting butt joint through setting up, thereby realize the fixed to the vertical direction of crossbeam, the joint spring of setting promotes solid fixed ring, make peg graft pole and crossbeam card die, thereby realize that the front and back of crossbeam is fixed, avoid it to produce the skew, it is fixed to realize the quick installation of crossbeam, the drive motor of setting drives the dwang and rotates, make screw thread seat lateral shifting, thereby drive aircraft nose lateral shifting, remove in the spout on the fixed rail of slider edge of setting, increase the stability of screw thread seat removal process, the lateral shifting of the supporting spring through flexible supplementary screw thread seat of setting, guarantee that the aircraft nose is difficult for producing the skew when the operation, promote its reliability.

Description

Engraving machine integrated strong beam

Technical Field

The utility model relates to a engraver integrated into one piece powerful crossbeam technical field specifically is engraver integrated into one piece powerful crossbeam.

Background

The engraving is a drilling and milling combined processing in principle, a plurality of data input modes of an engraving machine have more free edges as required, a computer engraving machine has two types of laser engraving and mechanical engraving, the two types have high power and low power, the application range of the engraving machine is very wide, so that the most suitable application range of various engraving machines needs to be known, the low power is only suitable for manufacturing bicolor plates, building models, small-sized labels, three-dimensional artware and the like, the power required for engraving jade, metal and the like is more than 1500W, and the high-power engraving machine can be used as a small-power engraving machine and is most suitable for large-scale cutting, embossing and engraving.

At present engraver in the manufacture, the spandrel girder that uses generally adopts fixed welding, and its installation is loaded down with trivial details relatively, and the maintenance in later stage of not being convenient for moreover, the carving head that uses generally along spandrel girder lateral shifting at the in-process that removes, but the carving head removal process easily produces the skew, influences the result of working, so proposes the powerful crossbeam of engraver integrated into one piece and solves above-mentioned problem.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a powerful crossbeam of engraver integrated into one piece to solve the present engraver that proposes in the above-mentioned background art and in the manufacturing process, the spandrel girder that uses generally adopts fixed welding, and its installation is loaded down with trivial details relatively, and the maintenance in later stage of being not convenient for moreover, the carving head that uses is at the in-process that removes, generally along spandrel girder lateral shifting, but the carving head removes the easy skew that produces of process, influences the problem of processing effect.

In order to achieve the above object, the utility model provides a following technical scheme: the powerful crossbeam integrally formed by the engraving machine comprises two bearing plates, wherein two opposite sides of the bearing plates are fixedly provided with fixing parts, two fixing parts are movably arranged between the fixing parts, the bottom of the crossbeam is fixedly provided with a mounting frame, the inside of the mounting frame is fixedly provided with a transmission motor, the bottom of the crossbeam is fixedly provided with two positioning plates which are positioned at the right side of the mounting frame, the bottom of the crossbeam is fixedly provided with a fixed rail which is positioned between the two positioning plates, the right side of the positioning plate is fixedly provided with a fixed block, the output shaft of the transmission motor is fixedly connected with a rotating rod which penetrates through the left positioning plate and is movably connected with the fixed block, the outer part of the rotating rod is sleeved with a supporting spring which is in contact with the right side of the left positioning plate, the outer part of the rotating rod is sleeved, the right side fixed mounting of spacing ring has the screw thread seat that is run through by the dwang, the top fixed mounting of screw thread seat has the slider with the bottom swing joint of fixed rail, the bottom fixed mounting of screw thread seat has the aircraft nose, two the equal fixed mounting in one side that the bearing plate was carried on the back mutually has joint spare, two the grafting pole that runs through two bearing plates respectively and respectively with the left and right sides looks joint of crossbeam is all pegged graft to one side that joint spare was carried on the back mutually, two the inside joint spring that is located two joint spares respectively, two has all been cup jointed to the outside of grafting pole the equal fixed mounting in outside of grafting pole is located the solid fixed ring that two joint spares are inside respectively and respectively with the relative one side contact of two joint springs, two the equal fixed mounting in one end that the grafting pole was carried on.

Preferably, the bottom of the fixed rail is provided with a sliding groove, and the sliding block is connected in the sliding groove in a sliding and clamping manner.

Preferably, the inner diameter of the supporting spring is matched with the diameter of the rotating rod, and the inner diameter of the limiting ring is matched with the diameter of the rotating rod.

Preferably, the diameter of the limiting ring is larger than that of the supporting spring, and the moving distance of the limiting ring corresponds to the telescopic length of the supporting spring.

Preferably, the left side and the right side of the cross beam are both provided with grooves, and the two insertion rods are respectively clamped in the two grooves.

Preferably, the size of the clamping spring is matched with the diameter of the insertion rod, and the telescopic length of the clamping spring corresponds to the moving distance of the fixing ring.

Compared with the prior art, the beneficial effects of the utility model are that: this powerful crossbeam of engraver integrated into one piece, crossbeam and mounting butt joint through setting up, thereby realize the fixed to the vertical direction of crossbeam, the joint spring of setting promotes solid fixed ring, make peg graft pole and crossbeam card dead, thereby realize the front and back fixed of crossbeam, avoid it to produce the skew, realize fixed to the quick installation of crossbeam, the dismantlement of crossbeam can be accomplished to the pulling pull ring, make things convenient for the staff to overhaul and maintain, the drive motor of setting drives the dwang and rotates, make screw thread seat lateral shifting, thereby drive aircraft nose lateral shifting, remove in the spout on the slider along the fixed rail of setting, increase the stability of screw thread seat removal process, the lateral shifting of supporting spring through flexible supplementary screw thread seat of setting, guarantee the aircraft nose difficult production skew when the operation, promote its reliability.

Drawings

Fig. 1 is a schematic structural diagram of the present invention.

Fig. 2 is an enlarged view of a portion a in fig. 1 according to the present invention.

In the figure: 1-a bearing plate; 2-a fixing piece; 3-a cross beam; 4-a mounting frame; 5-a transmission motor; 6, positioning a plate; 7-fixing blocks; 8-rotating the rod; 9-a support spring; 10-a fixed rail; 11-a spacing ring; 12-a threaded screw seat; 13-a slide block; 14-a machine head; 15-a clip; 16-a plug rod; 17-a snap spring; 18-a fixed ring; 19-a pull ring.

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 and fig. 2, the present invention provides an embodiment: an integrally-formed powerful beam of an engraving machine comprises two bearing plates 1, wherein fixing pieces 2 are fixedly arranged on opposite sides of the two bearing plates 1, a beam 3 is movably arranged between the two fixing pieces 2, an installation frame 4 is fixedly arranged at the bottom of the beam 3, a transmission motor 5 is fixedly arranged in the installation frame 4, the type of the transmission motor 5 can be XCWL370, two positioning plates 6 which are positioned on the right side of the installation frame 4 are fixedly arranged at the bottom of the beam 3, a fixed rail 10 which is positioned between the two positioning plates 6 is fixedly arranged at the bottom of the beam 3, a fixing block 7 is fixedly arranged on the left side of the positioning plate 6 on the right side, an output shaft of the transmission motor 5 is fixedly connected with a rotating rod 8 which penetrates through the positioning plate 6 on the left side and is movably connected with the fixing block 7, a supporting spring 9 which is contacted, a limiting ring 11 contacted with the right end of a supporting spring 9 is sleeved outside the rotating rod 8, the inner diameter of the supporting spring 9 is matched with the diameter of the rotating rod 8, the inner diameter of the limiting ring 11 is matched with the diameter of the rotating rod 8, the diameter of the limiting ring 11 is larger than that of the supporting spring 9, the moving distance of the limiting ring 11 corresponds to the telescopic length of the supporting spring 9, a threaded screw seat 12 penetrated by the rotating rod 8 is fixedly installed on the right side of the limiting ring 11, a sliding block 13 movably connected with the bottom of the fixed rail 10 is fixedly installed on the top of the threaded screw seat 12, a sliding groove is formed in the bottom of the fixed rail 10, the sliding block 13 is clamped in the sliding groove, a machine head 14 is fixedly installed at the bottom of the threaded screw seat 12, clamping pieces 15 are fixedly installed on one side of two bearing plates 1 opposite to each other, inserting rods 16 respectively penetrated through the two bearing plates 1 and respectively clamped with the left side and the right side of the, the left side and the right side of the cross beam 3 are respectively provided with a groove, the two insertion rods 16 are respectively clamped in the two grooves, clamping springs 17 respectively positioned in the two clamping pieces 15 are sleeved outside the two insertion rods 16, fixing rings 18 respectively positioned in the two clamping pieces 15 and respectively contacted with one side opposite to the two clamping springs 17 are fixedly installed outside the two insertion rods 16, the size of each clamping spring 17 is matched with the diameter of the insertion rod 16, the telescopic length of each clamping spring 17 corresponds to the moving distance of the corresponding fixing ring 18, pull rings 19 are fixedly installed at the opposite ends of the two insertion rods 16, the cross beam 3 is butted with the fixing piece 2 through the arranged cross beam, so that the cross beam 3 is fixed in the vertical direction, the arranged clamping springs 17 push the fixing rings 18, the insertion rods 16 are clamped with the cross beam 3, so that the front and back fixing of the cross beam 3 is realized, and the deviation of the cross beam, the realization is fixed to the quick installation of crossbeam 3, crossbeam 3's dismantlement can be accomplished to pulling pull ring 19, make things convenient for the staff to overhaul and maintain, the transmission motor 5 of setting drives dwang 8 and rotates, make screw thread seat 12 lateral shifting, thereby drive aircraft nose 14 lateral shifting, the slider 13 of setting is removed along the spout on fixed rail 10, increase the stability of screw thread seat 12 removal process, the supporting spring 9 of setting is through the lateral shifting of flexible supplementary screw thread seat 12, guarantee that aircraft nose 14 is difficult for producing the skew when the operation, promote its reliability.

To sum up: the engraving machine integrally forms a strong beam, the beam 3 is butted with the fixing piece 2 through the arranged beam 3, so that the beam 3 is fixed in the vertical direction, the arranged clamping spring 17 pushes the fixing ring 18, so that the insertion rod 16 is clamped with the beam 3, thereby realizing the front and back fixation of the beam 3, avoiding the deviation, realizing the rapid installation and fixation of the beam 3, finishing the disassembly of the beam 3 by pulling the pull ring 19, facilitating the overhaul and maintenance of workers, driving the rotating rod 8 to rotate by the arranged transmission motor 5, leading the thread screw seat 12 to transversely move, thereby drive aircraft nose 14 lateral shifting, the slider 13 that sets up removes along the spout on the fixed rail 10, increases the stability of screw thread seat 12 removal process, and the lateral shifting of the supporting spring 9 through flexible supplementary screw thread seat 12 of setting guarantees that aircraft nose 14 is difficult for producing the skew when the operation, promotes its reliability.

It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Claims

1. Powerful crossbeam of engraver integrated into one piece, be two bearing plate (1) including quantity, its characterized in that: two equal fixed mounting in one side relative of bearing plate (1) has mounting (2), two movable mounting has crossbeam (3) between mounting (2), the bottom fixed mounting of crossbeam (3) has mounting bracket (4), the inside fixed mounting of mounting bracket (4) has drive machine (5), the bottom fixed mounting of crossbeam (3) has locating plate (6) that are located mounting bracket (4) the right and quantity is two, the bottom fixed mounting of crossbeam (3) has fixed rail (10) that are located between two locating plates (6), the left side fixed mounting of locating plate (6) on the right has fixed block (7), the output shaft fixed connection of drive machine (5) runs through locating plate (6) on the left side and dwang (8) with fixed block (7) swing joint, the outside of dwang (8) cup joint with supporting spring (9) with the right side contact of locating plate (6) on the left side, spacing ring (11) with the right-hand member contact of supporting spring (9) has been cup jointed to the outside of dwang (8), the right side fixed mounting of spacing ring (11) has screw base (12) that is run through by dwang (8), the top fixed mounting of screw base (12) has bottom swing joint's slider (13) with fixed rail (10), the bottom fixed mounting of screw base (12) has aircraft nose (14), two the equal fixed mounting in one side that bearing plate (1) was carried on the back mutually has joint spare (15), two joint spare (15) one side that carries on the back mutually all pegs graft and have peg graft pole (16) that run through two bearing plates (1) respectively and respectively with the left and right sides looks joint of crossbeam (3), two the joint spring (17) that are located two joint spare (15) respectively, two the equal fixed mounting in outside of peg pole (16) is located two joint spare (15) respectively inside and divide The fixing rings (18) are respectively contacted with one side opposite to the two clamping springs (17), and pull rings (19) are fixedly installed at the opposite ends of the two insertion rods (16).

2. The engraver integrally formed strength beam of claim 1, wherein: the bottom of the fixed rail (10) is provided with a sliding groove, and the sliding block (13) is clamped in the sliding groove in a sliding manner.

3. The engraver integrally formed strength beam of claim 1, wherein: the inside diameter of supporting spring (9) and the diameter looks adaptation of dwang (8), the inside diameter looks adaptation of internal diameter and dwang (8) of spacing ring (11).

4. The engraver integrally formed strength beam of claim 1, wherein: the diameter of the limiting ring (11) is larger than that of the supporting spring (9), and the moving distance of the limiting ring (11) corresponds to the telescopic length of the supporting spring (9).

5. The engraver integrally formed strength beam of claim 1, wherein: the left side and the right side of the cross beam (3) are both provided with grooves, and the two insertion rods (16) are respectively clamped in the two grooves.

6. The engraver integrally formed strength beam of claim 1, wherein: the size of the clamping spring (17) is matched with the diameter of the insertion rod (16), and the telescopic length of the clamping spring (17) corresponds to the moving distance of the fixing ring (18).