CN205128708U - Omnipotent angle of attack machine - Google Patents
Omnipotent angle of attack machine Download PDFInfo
- Publication number
- CN205128708U CN205128708U CN201520982345.1U CN201520982345U CN205128708U CN 205128708 U CN205128708 U CN 205128708U CN 201520982345 U CN201520982345 U CN 201520982345U CN 205128708 U CN205128708 U CN 205128708U
- Authority
- CN
- China
- Prior art keywords
- cutting die
- fuselage
- die
- press
- scale
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
Abstract
The utility model discloses an omnipotent angle of attack machine, it relates to stainless steel processing technology field, the press is installed to the upper end of fuselage, and the hood is installed in the outside of press, installs the pressure pole on the press, and the conveyer belt is installed on the right side of fuselage, and foot switch passes through the internal connection of wire and accuse electronic box, and the mold machine structure is installed on the work plane of fuselage, mold machine construct contain the die shank, go up the cutting die, cutting die, fixed plate, angular adjustment slider, scale, loose pin, guide pillar down, the die shank is installed on the pressure pole, and the die shank is connected with the upper end of last cutting die, installs the several guide pillar on going up the cutting die, and the angular adjustment slider is installed on last cutting die, and one side of angular adjustment slider is provided with the scale, and the two loose pin is installed under on the cutting die, and lower cutting die is installed on the fixed plate, and the fixed plate is installed on the working plane of fuselage, the utility model provides high machining efficiency has realized that a mould is multi -purpose, long service life, and intensity is high, saves time, and application scope is wide.
Description
Technical field
The utility model relates to stainless steel processing technique field, is specifically related to a kind of omnipotent angle punching machine.
Background technology
Because on market, the angle of stainless steel pipe splicing soldering opening forms by metal circular saw cutting, there is extruding force in metal circular saw cutting, saw blade cutter tooth is easy to wear unfavorable, and the tubing appearance deformation cut out is large, angle is crooked accurate, brings the flaw of inconvenience and technique outward appearance greatly to the work of welder.
Summary of the invention
The purpose of this utility model is defect for prior art and deficiency, provides a kind of omnipotent angle punching machine.
In order to solve the problem existing for background technology, the omnipotent angle punching machine of one of the present utility model, it comprises fuselage, forcing press, head-shield, conveyer belt, motor, power switch, power control box, floor push, press rods, mold mechanism; The upper end of fuselage is provided with forcing press, the outside of forcing press is provided with head-shield, forcing press is provided with press rods, the right side of fuselage is provided with conveyer belt, the lower end of fuselage interior is provided with motor, the outside of fuselage is separately installed with power switch, power control box, and floor push is connected with the inside of power control box by wire, and mold mechanism is arranged on the working face of fuselage; Described mold mechanism comprises die shank, upper cutting die, lower cutting die, fixed head, angle adjustment slide block, scale, loose pin, guide pillar; Die shank is arranged in press rods, die shank is connected with the upper end of upper cutting die, upper cutting die is provided with several guide pillar, angle adjustment slide block is arranged on cutting die, the side of angle adjustment slide block is provided with scale, two loose pins are arranged on lower cutting die, and lower cutting die is arranged on fixed head, and fixed head is arranged on the working face of fuselage.
The utility model beneficial effect is: improve working (machining) efficiency, achieves one module multiple usages, long service life, and intensity is high, saves time, applied widely.
accompanying drawing illustrates:
Fig. 1 is structural representation of the present utility model.
Description of reference numerals:
1-fuselage; 2-forcing press; 3-head-shield; 4-conveyer belt; 5-motor; 6-power switch; 7-power control box; 8-floor push; 9-press rods; 10-die shank; The upper cutting die of 11-; Cutting die under 12-; 13-fixed head; 14-angle adjustment slide block; 15-scale; 16-loose pin; 17-guide pillar.
detailed description of the invention:
Below in conjunction with accompanying drawing, the utility model is further described.
In order to make the purpose of this utility model, technical scheme and advantage clearly understand, below in conjunction with the drawings and the specific embodiments, the utility model is further elaborated.Should be appreciated that detailed description of the invention described herein only in order to explain the utility model, and be not used in restriction the utility model.
As shown in Figure 1, this detailed description of the invention adopts following technical scheme: it comprises fuselage 1, forcing press 2, head-shield 3, conveyer belt 4, motor 5, power switch 6, power control box 7, floor push 8, press rods 9, mold mechanism; The upper end of fuselage 1 is provided with forcing press 2, the outside of forcing press 2 is provided with head-shield 3, forcing press 2 is provided with press rods 9, the right side of fuselage 1 is provided with conveyer belt 4, the lower end of fuselage 1 inside is provided with motor 5, the outside of fuselage 1 is separately installed with power switch 6, power control box 7, and floor push 8 is connected by the inside of wire with power control box 7, and mold mechanism is arranged on the working face of fuselage 1; Described mold mechanism comprises die shank 10, upper cutting die 11, lower cutting die 12, fixed head 13, angle adjustment slide block 14, scale 15, loose pin 16, guide pillar 17; Die shank 10 is arranged in press rods 9, die shank 10 is connected with the upper end of upper cutting die 11, upper cutting die 11 is provided with several guide pillar 17, angle adjustment slide block 14 is arranged on cutting die 11, the side of angle adjustment slide block 14 is provided with scale 15, two loose pins 16 are arranged on lower cutting die 12, and lower cutting die 12 is arranged on fixed head 13, and fixed head 13 is arranged on the working face of fuselage 1.
The operation principle of this detailed description of the invention is: add man-hour, material is placed between upper cutting die and lower cutting die, according to processing technology, adopts angle adjustment slide block 14 to realize adjusting angle and size with coordinating of scale 15, upper cutting die 11 is driven to realize corner cut by forcing press, can process various angle, and can realize one module multiple usages, performance is strong, the edge of a knife is durable, improve efficiency, can to the square tube machining angle of more than 36*36 any specification, also can to below 3mm sheet fabrication angle.
The above, only in order to the technical solution of the utility model to be described and unrestricted, other amendment that those of ordinary skill in the art make the technical solution of the utility model or equivalently to replace, only otherwise depart from the spirit and scope of technical solutions of the utility model, all should be encompassed in the middle of right of the present utility model.
Claims (1)
1. an omnipotent angle punching machine, is characterized in that: it comprises fuselage, forcing press, head-shield, conveyer belt, motor, power switch, power control box, floor push, press rods, mold mechanism; The upper end of fuselage is provided with forcing press, the outside of forcing press is provided with head-shield, forcing press is provided with press rods, the right side of fuselage is provided with conveyer belt, the lower end of fuselage interior is provided with motor, the outside of fuselage is separately installed with power switch, power control box, and floor push is connected with the inside of power control box by wire, and mold mechanism is arranged on the working face of fuselage; Described mold mechanism comprises die shank, upper cutting die, lower cutting die, fixed head, angle adjustment slide block, scale, loose pin, guide pillar; Die shank is arranged in press rods, die shank is connected with the upper end of upper cutting die, upper cutting die is provided with several guide pillar, angle adjustment slide block is arranged on cutting die, the side of angle adjustment slide block is provided with scale, two loose pins are arranged on lower cutting die, and lower cutting die is arranged on fixed head, and fixed head is arranged on the working face of fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520982345.1U CN205128708U (en) | 2015-12-02 | 2015-12-02 | Omnipotent angle of attack machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520982345.1U CN205128708U (en) | 2015-12-02 | 2015-12-02 | Omnipotent angle of attack machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205128708U true CN205128708U (en) | 2016-04-06 |
Family
ID=55614534
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520982345.1U Expired - Fee Related CN205128708U (en) | 2015-12-02 | 2015-12-02 | Omnipotent angle of attack machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205128708U (en) |
-
2015
- 2015-12-02 CN CN201520982345.1U patent/CN205128708U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160406 Termination date: 20181202 |