CN215238654U

CN215238654U - Pipe laser cutting machine head integrating positioning and collision prevention

Info

Publication number: CN215238654U
Application number: CN202121441007.9U
Authority: CN
Inventors: 高开伟
Original assignee: Taicang Hengqi Mechanical Equipment Co ltd
Current assignee: Taicang Hengqi Mechanical Equipment Co ltd
Priority date: 2021-06-28
Filing date: 2021-06-28
Publication date: 2021-12-21
Anticipated expiration: 2031-06-28

Abstract

The utility model discloses a collect location, crashproof integrative tubular product laser cutting machine aircraft nose belongs to tubular product processing equipment technical field, including casing (1), casing (1) top is equipped with reflection seat (2), be equipped with speculum (21) in reflection seat (2), casing (1) bottom is equipped with copper nozzle (3), casing (1) bottom is equipped with protection casing (4) with copper nozzle (3) department of linking to each other, be equipped with infrared ray sensor (41) and distancer (42) in protection casing (4). This kind of collect location, integrative tubular product laser cutting machine aircraft nose of anticollision can fix a position tubular product, can also have the anticollision effect, can protect the aircraft nose not impaired.

Description

Pipe laser cutting machine head integrating positioning and collision prevention

Technical Field

The utility model belongs to the technical field of the tubular product processing equipment, specifically, relate to an integrative tubular product laser cutting machine aircraft nose of collection location, anticollision.

Background

The laser cutting is to irradiate the material to be cut with high-power-density laser beam, so that the material is heated to vaporization temperature quickly and evaporated to form holes, and the holes continuously form slits with narrow width along with the movement of the material by the light beam, thereby completing the cutting of the material. Because the laser facula is little, energy density is high, cutting speed is fast, therefore laser cutting can obtain better cutting quality, and cutting speed is fast moreover, and cutting efficiency is high, need not contact with the machined part, need not change the cutter, and the cutting material is many kinds, and the range of application is wide.

The metal pipe is applied to various fields, and the metal pipe is cut by a laser cutting machine in the processing process. Because the machine head of the laser cutting machine is expensive, and for the processing of some metal pipe fittings, if the machine head is collided, the machine head is easy to be damaged in the carrying process, and the normal work of the machine head is influenced; in addition, many laser cutting machines all adopt artifical location now, and the location precision is relatively poor, leads to laser cutting machine cutting inefficiency.

SUMMERY OF THE UTILITY MODEL

In order to solve the problem, the utility model provides a collect location, integrative tubular product laser cutting machine aircraft nose of anticollision, this kind of collect location, integrative tubular product laser cutting machine aircraft nose of anticollision can fix a position tubular product, can also have the anticollision effect, can protect the aircraft nose not impaired.

In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: the utility model provides a collect location, integrative tubular product laser cutting machine aircraft nose of anticollision, includes the casing, the casing top is equipped with the reflection seat, be equipped with the speculum in the reflection seat, chassis bottom is equipped with the copper nozzle, chassis bottom and copper nozzle department of linking to each other are equipped with the protection casing, be equipped with infrared ray sensor and distancer in the protection casing. Laser enters the machine shell through an inlet of the reflecting seat, is reflected by the reflecting mirror and is emitted on the surface of a workpiece through the copper nozzle to cut the workpiece; the infrared sensor can be used for positioning a workpiece, and the distance measuring instrument can be used for detecting the distance and conveniently adjusting the position of the machine head.

Furthermore, the copper nozzle is detachably connected with the bottom of the machine shell. The installation and the replacement of the copper nozzle are convenient.

Further, the cross section of the protective cover is arc-shaped. The protective cover has the protective effect and can prevent metal scraps generated in the cutting process from splashing everywhere.

Furthermore, a lifting mechanism is arranged on the top side of the reflection seat.

Further, elevating system includes connecting seat, motor, lead screw, connecting block and connecting plate, establish to the connecting seat side and establish to the shape of falling L, the connecting seat top is located to the motor, the connecting seat side is equipped with the recess, the lead screw is located in the recess and the top links to each other with motor drive, the lead screw outside cover is equipped with the nut piece, the connecting plate passes through the fastener and links to each other with reflection seat top side, nut piece side passes through the connecting block and links to each other with the connecting plate. The connecting seat is connected with the machine base, the height of the copper nozzle and the height of the machine shell can be adjusted by the lifting mechanism, a workpiece is conveniently focused, and the cutting efficiency of the laser cutting machine is improved.

Further, the motor is connected with the screw rod through a coupler.

Further, the fastener is a bolt and a nut.

Has the advantages that: compared with the prior art, the utility model has the advantages of it is following: the utility model provides a pipe laser cutting machine head integrating positioning and collision prevention, which is characterized in that laser of the pipe laser cutting machine head integrating positioning and collision prevention enters a machine shell through an inlet of a reflecting seat, is reflected by a reflecting mirror, and is shot on the surface of a workpiece through a copper nozzle to cut the workpiece; the infrared sensor can be used for positioning a workpiece, and the distance measuring instrument can be used for detecting the distance, so that the position of the machine head can be conveniently adjusted; the height of the copper nozzle and the height of the machine shell can be adjusted through the lifting mechanism, a workpiece is conveniently focused, and the cutting efficiency of the laser cutting machine is improved.

Drawings

Fig. 1 is the utility model discloses a collection location, integrative tubular product laser cutting machine aircraft nose block diagram of anticollision.

In the figure: the device comprises a machine shell 1, a reflection seat 2, a reflector 21, a copper burner 3, a protective cover 4, an infrared sensor 41, a distance meter 42, a lifting mechanism 5, a connection seat 51, a groove 511, a motor 52, a screw rod 53, a coupling 54, a nut 55 block 56, a connection block 57, a 571 bolt and a nut 572.

Detailed Description

Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary and intended to be used for explaining the present invention, and should not be construed as limiting the present invention.

In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "clockwise", "counterclockwise" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and to simplify the description, but do not indicate or imply that the device or element 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" and "first" 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" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, unless otherwise specified, "a plurality" means two or more unless explicitly defined otherwise.

In the present invention, unless otherwise expressly specified or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be 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 according to specific situations by those skilled in the art.

In the present disclosure, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact between the first and second features, or may comprise contact between the first and second features not directly. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.

The invention will be further elucidated with reference to the drawings and the embodiments.

Example 1

As shown in figure 1, a collect location, integrative tubular product laser cutting machine aircraft nose of anticollision, including casing 1, casing 1 top is equipped with reflection seat 2, be equipped with speculum 21 in the reflection seat 2, casing 1 bottom is equipped with copper nozzle 3, casing 1 bottom and the department of connecting of copper nozzle 3 are equipped with protection casing 4, be equipped with infrared ray sensor 41 and distancer 42 in the protection casing 4.

Example 2

As shown in figure 1, a collect location, integrative tubular product laser cutting machine aircraft nose of anticollision, including casing 1, casing 1 top is equipped with reflection seat 2, be equipped with speculum 21 in the reflection seat 2, casing 1 bottom is equipped with copper nozzle 3, copper nozzle 3 links to each other for dismantling with casing 1 bottom, casing 1 bottom is equipped with protection casing 4 with copper nozzle 3 department of linking to each other, be equipped with infrared ray sensor 41 and distancer 42 in the protection casing 4, protection casing 4 cross-section is arc.

The top side of the reflection seat 2 is provided with a lifting mechanism 5, the lifting mechanism 5 comprises a connecting seat 51, a motor 52, a screw rod 53, a connecting block 56 and a connecting plate 57, the side surface of the connecting seat 51 is designed to be inverted L-shaped, the motor 52 is arranged at the top of the connecting seat 51, the side surface of the connecting seat 51 is provided with a groove 511, the screw rod 53 is arranged in the groove 511, the top end of the screw rod 53 is connected with the motor 52 through a coupling 54, a nut block 55 is sleeved on the outer side of the screw rod 53, the connecting plate 57 is connected with the top side of the reflection seat 2 through a fastening piece, the side surface of the nut block 55 is connected with the connecting plate 57 through the connecting block 56, and the fastening piece is a bolt 571 and a nut 572.

The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, a plurality of modifications can be made without departing from the principles of the present invention, and these modifications should also be regarded as the protection scope of the present invention.

Claims

1. The utility model provides a collect location, integrative tubular product laser cutting machine aircraft nose of anticollision which characterized in that: including casing (1), casing (1) top is equipped with reflection seat (2), be equipped with speculum (21) in reflection seat (2), casing (1) bottom is equipped with copper nozzle (3), casing (1) bottom is equipped with protection casing (4) with copper nozzle (3) department of linking to each other, be equipped with infrared ray sensor (41) and distancer (42) in protection casing (4).

2. The pipe laser cutting machine head integrating positioning and collision prevention as claimed in claim 1, wherein: the copper nozzle (3) is detachably connected with the bottom of the machine shell (1).

3. The pipe laser cutting machine head integrating positioning and collision prevention as claimed in claim 1, wherein: the section of the protective cover (4) is arc-shaped.

4. The pipe laser cutting machine head integrating positioning and collision prevention as claimed in any one of claims 1-3, wherein: and a lifting mechanism (5) is arranged on the top side of the reflection seat (2).

5. The pipe laser cutting machine head integrated with positioning and collision prevention as claimed in claim 4, wherein: elevating system (5) are including connecting seat (51), motor (52), lead screw (53), connecting block (56) and connecting plate (57), establish to fall L shape connecting seat (51) side, connecting seat (51) top is located in motor (52), connecting seat (51) side is equipped with recess (511), lead screw (53) are located in recess (511) and the top links to each other with motor (52) drive, lead screw (53) outside cover is equipped with nut piece (55), connecting plate (57) link to each other with reflection seat (2) top side through the fastener, nut piece (55) side passes through connecting block (56) and links to each other with connecting plate (57).

6. The pipe laser cutting machine head integrated with positioning and collision prevention as claimed in claim 5, wherein: the motor (52) is connected with the screw rod (53) through a coupling (54).

7. The pipe laser cutting machine head integrated with positioning and collision prevention as claimed in claim 5, wherein: the fastener is a bolt (571) and a nut (572).