CN202461202U - Tension straightening machine - Google Patents
Tension straightening machine Download PDFInfo
- Publication number
- CN202461202U CN202461202U CN2012200082489U CN201220008248U CN202461202U CN 202461202 U CN202461202 U CN 202461202U CN 2012200082489 U CN2012200082489 U CN 2012200082489U CN 201220008248 U CN201220008248 U CN 201220008248U CN 202461202 U CN202461202 U CN 202461202U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- workpiece
- machine body
- pull head
- feeding rack
- 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.)
- Withdrawn - After Issue
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Abstract
The utility model discloses a tension straightening machine which comprises a feeding frame and a machine body. The feeding frame is formed by a plurality of brackets which are independent from each other or are integrated and are transversely arranged in a staggered mode; the feeding frame is positioned in front of the feed end of the machine body; the feeding frame and the machine body are arranged side by side; the cross section of the machine body is C-shaped; an open part of the machine body is positioned in the feeding direction; the open port of the C-shaped machine body is provided with a safety door which can rise and fall; a cylinder which can rise and fall and a conveying device which can move leftwards and rightwards are arranged inside the machine body; one end inside the machine body is provided with a twisting pull head and the other end inside the machine body is provided with an inserted pin pull head; a through hole is formed in the end of the machine body, which is positioned at a discharge port; a row of conveying raceways and elevators, which are longitudinally arranged, are arranged outside the through hole; and a discharge frame with the same structure as the feeding frame is arranged side by side with the conveying raceways and the elevators. The tension straightening machine has the beneficial effects that the tension straightening machine is convenient and safe to process and has high efficiency; and the production line operation is implemented.
Description
Technical field
The utility model relates to a kind of tension flattening machine, particularly a kind of tension flattening machine that section bar is stretching.
Background technology
A lot of section bar productions are not very straight through extruding or roll forming, need clamp two ends through tension flattening machine, and apply certain force of strain and stretch, and the section bar that stretched so just meets the standard of dispatching from the factory.Existing tension flattening machine has many deficiencies, such as, security protection is not enough; Section bar processing can not pipelining, or the like.
The utility model content
To the deficiency of prior art, the utility model provides a kind of novel tension flattening machine.
To achieve these goals; The technical scheme that the utility model is taked is: tension flattening machine, comprise feeding rack and fuselage, and feeding rack is configured to by transversely arranged the propping up of staggering each other of several independent or one; Feeding rack is positioned at the place ahead of fuselage feed end; With fuselage side by side, the cross section of fuselage is a C shape, and opening is positioned at feedstock direction; The C shape opening of fuselage is provided with the safety door of ability oscilaltion; Fuselage interior is provided with the cylinder of ability oscilaltion and the transport of side-to-side movement; One end of fuselage interior is provided with turns round stubborn pull head, and the other end is provided with the latch pull head, and the end that fuselage is positioned at discharging opening is provided with through hole; Through hole is provided with conveying raceway and the lift that a row vertically arranges outward, is arranged side by side the discharge rack identical with the feeding rack structure with carrying raceway and lift; Unprocessed workpiece laterally is placed on the feeding rack, workpiece is transported in the fuselage on row's dance roller the action of gas (oil) cylinder through the transport before the feeding rack; Make workpiece be lifted to specified altitude assignment; Workpiece is twisted a move toward one another (starting the plunger tip device simultaneously) with turning round then, and motion back clamping work pieces one end that puts in place drives to turn round again and twists head and advance to latch pull head direction; After motion put in place, the other end of (starting the plunger tip device) clamping work pieces was realized the stretching action of two ends to workpiece; Stretching finishes, and gas (oil) cylinder descends, and workpiece passes from the through hole of discharge end; Simultaneously, safety door descends, and prepares next workpiece and gets into from charging aperture; Finished workpiece transports out through extendable conveyor gradually, is transported to discharge rack through lift and conveying raceway.
The beneficial effect of the utility model: easy to process, safety, efficient is high, realizes pipelining.
Description of drawings
The front view of Fig. 1, the utility model;
The vertical view of Fig. 2, Fig. 1;
Fig. 3, Fig. 4, Fig. 5, Fig. 6 are respectively the G-G, B-B, F-F, D-D of Fig. 1 to view.
The specific embodiment
As shown in the figure, tension flattening machine comprises feeding rack 4 and fuselage 2; Feeding rack 4 is by transversely arranged being configured to of staggering each other of several independent or one, and feeding rack 4 is positioned at the place ahead of fuselage 2 feed ends, with fuselage side by side; The cross section of fuselage is a C shape, and opening is positioned at feedstock direction; The C shape opening of fuselage 2 is provided with the safety door of ability oscilaltion; Fuselage 2 inside are provided with the cylinder of ability oscilaltion and the transport of side-to-side movement; Fuselage 2 inner ends are provided with to turn round twists pull head 1, and the other end is provided with latch pull head 3, and the end that fuselage 2 is positioned at discharging opening is provided with through hole; Through hole is provided with the conveying raceway 8 and lift 7 that a row vertically arranges outward, is arranged side by side the discharge rack 5 identical with feeding rack 4 structures with carrying raceway 8 and lift 7; Unprocessed workpiece laterally is placed on the feeding rack 4, through the transport before the feeding rack 4 just workpiece be transported in the fuselage 2 on row's dance rollers the action of gas (oil) cylinder; Make workpiece be lifted to specified altitude assignment; Workpiece is twisted a move toward one another (starting the plunger tip device simultaneously) with turning round then, and motion back clamping work pieces one end that puts in place drives to turn round again and twists head and advance to latch pull head direction; After motion put in place, the other end of (starting the plunger tip device) clamping work pieces was realized the stretching action of two ends to workpiece; Stretching finishes, and gas (oil) cylinder descends.Workpiece passes from the through hole of discharge end, and simultaneously, safety door descends, and prepares next workpiece and gets into from charging aperture, and finished workpiece transports out through extendable conveyor 6 gradually, is transported to discharge rack 5 through lift 7 and conveying raceway 8.
Claims (1)
1. tension flattening machine; It is characterized in that, comprise feeding rack (4) and fuselage (2), feeding rack (4) is configured to by transversely arranged the propping up of staggering each other of several independent or one; Feeding rack (4) is positioned at the place ahead of fuselage (2) feed end; With fuselage side by side, the cross section of fuselage is a C shape, and opening is positioned at feedstock direction; The C shape opening of fuselage (2) is provided with the safety door of ability oscilaltion; Fuselage (2) inside is provided with the cylinder of ability oscilaltion and the transport of side-to-side movement; The inner end of fuselage (2) is provided with turns round stubborn pull head (1), and the other end is provided with latch pull head (3), and the end that fuselage (2) is positioned at discharging opening is provided with through hole; Through hole is provided with conveying raceway (8) and the lift (7) that a row vertically arranges outward, is arranged side by side the discharge rack (5) identical with feeding rack (4) structure with carrying raceway (8) and lift (7); Unprocessed workpiece laterally is placed on the feeding rack (4), and the transport preceding through feeding rack (4) is transported to workpiece on the interior exhaust casing of fuselage (2) the cylinder action; Make workpiece be lifted to certain altitude; Transport is twisted the motion of pull head direction with workpiece to turning round then, and after motion put in place, the end that pull head is clamped workpiece was twisted in turning round of an end; The latch pull head (3) of the other end is clamped the other end of workpiece, realizes the stretching action of two ends to workpiece; Stretching finishes, and cylinder descends, and workpiece passes from the through hole of discharge end; Simultaneously, safety door descends, and prepares next workpiece and gets into from charging aperture; Finished workpiece transports out through extendable conveyor (6) gradually, is transported to discharge rack (5) through lift (7) and conveying raceway (8).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012200082489U CN202461202U (en) | 2012-01-09 | 2012-01-09 | Tension straightening machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012200082489U CN202461202U (en) | 2012-01-09 | 2012-01-09 | Tension straightening machine |
Publications (1)
Publication Number | Publication Date |
---|---|
CN202461202U true CN202461202U (en) | 2012-10-03 |
Family
ID=46909400
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2012200082489U Withdrawn - After Issue CN202461202U (en) | 2012-01-09 | 2012-01-09 | Tension straightening machine |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN202461202U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102527776A (en) * | 2012-01-09 | 2012-07-04 | 温州久一重工有限公司 | Tension straightening machine |
-
2012
- 2012-01-09 CN CN2012200082489U patent/CN202461202U/en not_active Withdrawn - After Issue
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102527776A (en) * | 2012-01-09 | 2012-07-04 | 温州久一重工有限公司 | Tension straightening machine |
CN102527776B (en) * | 2012-01-09 | 2014-01-22 | 温州久一重工有限公司 | Tension straightening machine |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
AV01 | Patent right actively abandoned |
Granted publication date: 20121003 Effective date of abandoning: 20140122 |
|
RGAV | Abandon patent right to avoid regrant |