CN105215094A - Aligning axis part device - Google Patents
Aligning axis part device Download PDFInfo
- Publication number
- CN105215094A CN105215094A CN201510786259.8A CN201510786259A CN105215094A CN 105215094 A CN105215094 A CN 105215094A CN 201510786259 A CN201510786259 A CN 201510786259A CN 105215094 A CN105215094 A CN 105215094A
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- China
- Prior art keywords
- main shaft
- fuselage
- shaft seat
- spindle drum
- movable spindle
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/10—Greenhouse gas [GHG] capture, material saving, heat recovery or other energy efficient measures, e.g. motor control, characterised by manufacturing processes, e.g. for rolling metal or metal working
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Abstract
The invention discloses a kind of aligning axis part device, fuselage comprises lower fuselage, and the front portion of lower fuselage arranges fuselage, is provided with two rotary output axis in gearbox; Upper fuselage left end arranges fixed main shaft seat, upper fuselage on the right side of fixed main shaft seat arranges slip rail, upper fuselage between slip rail and fixed main shaft seat arranges wheel shaft supporting plate, and movable spindle drum is slidably connected on slip rail, and the piston rod of hydraulic cylinder is connected with movable spindle drum; The medial surface of fixed main shaft seat and movable spindle drum one in front and one in back arranges main shaft mount pad respectively, before and after fixed main shaft seat and movable spindle drum side main shaft mount pad on respectively main shaft is installed, main shaft is downward-sloping gradually from front to back, main shaft on fixed main shaft seat and movable spindle drum is set with roller, arrange loop concave outside one of them roller, another roller arranges annular convex surface; Fixed main shaft seat is connected with two rotary output axis of gearbox by universal joint with the main shaft of movable spindle drum.Structure is simple, easy to use.
Description
Technical field
The present invention relates to a kind of aligning axis part device.
Background technology
Wheel shaft is axial workpiece, may there is distortion in process, causes wheel shaft not straight.Structure steel tube straightener disclosed in ZL2014207587657 of current coalignment, it is not very convenient that the axial workpiece less for diameter as wheel shaft, length is shorter uses.
Summary of the invention
In order to solve the problems of the technologies described above, the invention provides another kind of aligning axis part device easy to use.
To achieve these goals, technical scheme of the present invention is as follows: a kind of aligning axis part device, comprise fuselage, gearbox (3), it is characterized in that: described fuselage comprises lower fuselage (1), the nock of described lower fuselage (1) arranges fuselage (2), described gearbox (3) is fixed on the rear portion of lower fuselage (1), described gearbox (3) is connected with variable-frequency motor, is provided with two rotary output axis in described gearbox (3);
The left end of the upper surface of described upper fuselage (2) arranges fixed main shaft seat (5), the upper fuselage (2) on described fixed main shaft seat (5) right side is arranged the slip rail (6) that left and right extends, upper fuselage (2) between slip rail (6) and fixed main shaft seat (5) arranges wheel shaft supporting plate (11), movable spindle drum (7) is slidably connected on slip rail (6), in the right-hand end of the upper surface of upper fuselage (2), hydraulic cylinder (8) is installed, the piston rod of described hydraulic cylinder (8) is connected with movable spindle drum (7),
The medial surface of described fixed main shaft seat (5) and movable spindle drum (7) is all one in front and one in back arranged two main shaft mount pads (9), between the main shaft mount pad (9) of described fixed main shaft seat (5) and side, movable spindle drum (7) front and back, main shaft (10) is installed respectively, described main shaft (10) is downward-sloping gradually from front to back, described fixed main shaft seat (5) is parallel with the main shaft (10) of movable spindle drum (7), main shaft (10) on described fixed main shaft seat (5) and movable spindle drum (7) is set with roller (12), the middle part of one of them roller (12) outer surface arranges loop concave (12a), the centre corresponding loop concave (12a) of another roller (12) arranges annular convex surface (12b),
Be connected with two rotary output axis of gearbox (3) respectively by universal joint (4) after described fixed main shaft seat (5) extends back with the main shaft (10) of movable spindle drum (7), fixed main shaft seat (5) is relative with the roller (12) on movable spindle drum (7) to be rotated.
Adopt such scheme, according to the size of wheel shaft, the distance between two rollers is regulated by hydraulic cylinder, then variable-frequency motor is started, two rollers rotate relatively, are placed by wheel shaft on supporting plate between the rollers 27 and 28, because main shaft is obliquely installed from front to back, wheel shaft moves between the rollers 27 and 28 backward by automatically drawing, and finally product is out the product of alignment.
In such scheme: the two ends, left and right of described upper fuselage (2) arrange sidewall (2a) respectively, sidewall (2a) and the upper fuselage (2) at two ends form " U " shape structure, described fixed main shaft seat (5) is contained in the inner side of the sidewall (2a) in left side, and described hydraulic cylinder (8) is arranged on the inner side of right sidewall (2a).Such installation hydraulic cylinder and fixed main shaft seat are more for convenience.
In such scheme: the rear side of described upper fuselage (2) arranges receiving hopper (13), the material receiving port of described receiving hopper (13) is positioned at supporting plate (11) tail end.The collection of the wheel shaft of the alignment of conveniently going out.
Beneficial effect: of the present invention reasonable in design, structure is simple, and simple to operate, production efficiency is high, and security is high, easy to use.
Accompanying drawing explanation
Fig. 1 is front view of the present invention.
Fig. 2 is top view.
Fig. 3 is main shaft scheme of installation.
Detailed description of the invention
Below in conjunction with drawings and Examples, the invention will be further described:
Embodiment 1: aligning axis part device of the present invention comprises the parts compositions such as fuselage, gearbox 3, universal joint 4, fixed main shaft seat 5, slip rail 6, movable spindle drum 7, hydraulic cylinder 8, main shaft mount pad 9, main shaft 10, supporting plate 11, roller 12, receiving hopper 13.
Fuselage comprises lower fuselage 1, the nock of lower fuselage 1 arranges fuselage 2, gearbox 3 is fixed on the rear portion of lower fuselage 1, gearbox 3 is connected with variable-frequency motor (variable-frequency motor not shown in FIG.), be provided with two rotary output axis in gearbox 3, in gearbox 3, arrange reducing gear, variable-frequency motor output shaft is connected by reducing gear with between rotary output axis, this is prior art, does not repeat at this.
The two ends, left and right of upper fuselage 2 arrange sidewall 2a respectively, and the sidewall 2a at two ends and upper fuselage 2 form " U " shape structure, sidewall 2a and upper fuselage 2 one-body molded.
Fixed main shaft seat 5 is contained in the inner side of the sidewall 2a in left side, upper fuselage 2 on the right side of fixed main shaft seat 5 is arranged the slip rail 6 that left and right extends, upper fuselage 2 between slip rail 6 and fixed main shaft seat 5 arranges wheel shaft supporting plate 11, movable spindle drum 7 is slidably connected on slip rail 6, be arranged on the inner side of right sidewall 2a at hydraulic cylinder 8, the piston rod of hydraulic cylinder 8 is connected with movable spindle drum 7.
The medial surface of fixed main shaft seat 5 and movable spindle drum 7 is all one in front and one in back arranged two main shaft mount pads 9, before and after fixed main shaft seat 5 and movable spindle drum 7 side main shaft mount pad 9 between main shaft 10 is installed respectively, main shaft 10 is downward-sloping installation gradually from front to back, the main shaft 10 of fixed main shaft seat 5 is parallel with the main shaft 10 of movable spindle drum 7, main shaft 10 on fixed main shaft seat 5 and movable spindle drum 7 is set with roller 12, the middle part of one of them roller 12 outer surface arranges loop concave 12a, the corresponding loop concave 12a in centre of another roller 12 arranges annular convex surface 12b,
Main shaft 10 on fixed main shaft seat 5 and movable spindle drum 7 all extends back, fixed main shaft seat 5 is connected with two rotary output axis of gearbox 3 respectively by universal joint 4 with the elongated end backward of the main shaft 10 on movable spindle drum 7, and fixed main shaft seat 5 is relative with the roller 12 on movable spindle drum 7 to be rotated.
The rear side of upper fuselage 2 arranges receiving hopper 13, and the material receiving port of receiving hopper 13 is positioned at supporting plate 11 tail end.
The present invention is not limited to above-mentioned specific embodiment, should be appreciated that those of ordinary skill in the art just design according to the present invention can make many modifications and variations without the need to creative work.In a word, all technical staff in the art, all should by the determined protection domain of claims under this invention's idea on the basis of existing technology by the available technical scheme of logical analysis, reasoning, or a limited experiment.
Claims (3)
1. an aligning axis part device, comprise fuselage, gearbox (3), it is characterized in that: described fuselage comprises lower fuselage (1), the nock of described lower fuselage (1) arranges fuselage (2), described gearbox (3) is fixed on the rear portion of lower fuselage (1), described gearbox (3) is connected with variable-frequency motor, is provided with two rotary output axis in described gearbox (3);
The left end of the upper surface of described upper fuselage (2) arranges fixed main shaft seat (5), the upper fuselage (2) on described fixed main shaft seat (5) right side is arranged the slip rail (6) that left and right extends, upper fuselage (2) between slip rail (6) and fixed main shaft seat (5) arranges wheel shaft supporting plate (11), movable spindle drum (7) is slidably connected on slip rail (6), in the right-hand end of the upper surface of upper fuselage (2), hydraulic cylinder (8) is installed, the piston rod of described hydraulic cylinder (8) is connected with movable spindle drum (7),
The medial surface of described fixed main shaft seat (5) and movable spindle drum (7) is all one in front and one in back arranged two main shaft mount pads (9), between the main shaft mount pad (9) of described fixed main shaft seat (5) and side, movable spindle drum (7) front and back, main shaft (10) is installed respectively, described main shaft (10) is downward-sloping gradually from front to back, described fixed main shaft seat (5) is parallel with the main shaft (10) of movable spindle drum (7), main shaft (10) on described fixed main shaft seat (5) and movable spindle drum (7) is set with roller (12), the middle part of one of them roller (12) outer surface arranges loop concave (12a), the centre corresponding loop concave (12a) of another roller (12) arranges annular convex surface (12b),
Be connected with two rotary output axis of gearbox (3) respectively by universal joint (4) after described fixed main shaft seat (5) extends back with the main shaft (10) of movable spindle drum (7), fixed main shaft seat (5) is relative with the roller (12) on movable spindle drum (7) to be rotated.
2. aligning axis part device according to claim 1, it is characterized in that: the two ends, left and right of described upper fuselage (2) arrange sidewall (2a) respectively, sidewall (2a) and the upper fuselage (2) at two ends form " U " shape structure, described fixed main shaft seat (5) is contained in the inner side of the sidewall (2a) in left side, and described hydraulic cylinder (8) is arranged on the inner side of right sidewall (2a).
3. aligning axis part device according to claim 1, it is characterized in that: the rear side of described upper fuselage (2) arranges receiving hopper (13), the material receiving port of described receiving hopper (13) is positioned at supporting plate (11) tail end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510786259.8A CN105215094A (en) | 2015-11-17 | 2015-11-17 | Aligning axis part device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510786259.8A CN105215094A (en) | 2015-11-17 | 2015-11-17 | Aligning axis part device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105215094A true CN105215094A (en) | 2016-01-06 |
Family
ID=54984552
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510786259.8A Pending CN105215094A (en) | 2015-11-17 | 2015-11-17 | Aligning axis part device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105215094A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1980755A (en) * | 2004-07-01 | 2007-06-13 | 株式会社大同机械制作所 | Straightener |
| CN101020205A (en) * | 2006-12-25 | 2007-08-22 | 西安重型机械研究所 | Method of regulating inclination angle of straightening roller |
| CN201380218Y (en) * | 2009-03-25 | 2010-01-13 | 江苏诚德钢管股份有限公司 | Steel pipe straightening machine with thickened end part |
| JP4699121B2 (en) * | 2005-07-14 | 2011-06-08 | 大同マシナリー株式会社 | Bar material restraint device and bar material restraint system using restraint device |
| CN102847755A (en) * | 2012-09-21 | 2013-01-02 | 北京华谷减振器设备有限公司 | Connecting rod straightening machine and using method thereof |
| CN203565561U (en) * | 2013-11-01 | 2014-04-30 | 杭州新浙南钢管制造有限公司 | Two-roller straightening machine lower roller adjusting mechanism for steel pipe production |
| CN105013875A (en) * | 2015-07-30 | 2015-11-04 | 中国重型机械研究院股份公司 | Overrunning type feeding device for two-roller straightening machine |
-
2015
- 2015-11-17 CN CN201510786259.8A patent/CN105215094A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1980755A (en) * | 2004-07-01 | 2007-06-13 | 株式会社大同机械制作所 | Straightener |
| JP4699121B2 (en) * | 2005-07-14 | 2011-06-08 | 大同マシナリー株式会社 | Bar material restraint device and bar material restraint system using restraint device |
| CN101020205A (en) * | 2006-12-25 | 2007-08-22 | 西安重型机械研究所 | Method of regulating inclination angle of straightening roller |
| CN201380218Y (en) * | 2009-03-25 | 2010-01-13 | 江苏诚德钢管股份有限公司 | Steel pipe straightening machine with thickened end part |
| CN102847755A (en) * | 2012-09-21 | 2013-01-02 | 北京华谷减振器设备有限公司 | Connecting rod straightening machine and using method thereof |
| CN203565561U (en) * | 2013-11-01 | 2014-04-30 | 杭州新浙南钢管制造有限公司 | Two-roller straightening machine lower roller adjusting mechanism for steel pipe production |
| CN105013875A (en) * | 2015-07-30 | 2015-11-04 | 中国重型机械研究院股份公司 | Overrunning type feeding device for two-roller straightening machine |
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Application publication date: 20160106 |