CN105327976A - Shaft-part straightening device capable of adjusting conveying speed - Google Patents
Shaft-part straightening device capable of adjusting conveying speed Download PDFInfo
- Publication number
- CN105327976A CN105327976A CN201510791950.5A CN201510791950A CN105327976A CN 105327976 A CN105327976 A CN 105327976A CN 201510791950 A CN201510791950 A CN 201510791950A CN 105327976 A CN105327976 A CN 105327976A
- Authority
- CN
- China
- Prior art keywords
- main shaft
- fuselage
- movable spindle
- shaft seat
- spindle drum
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D3/00—Straightening or restoring form of metal rods, metal tubes, metal profiles, or specific articles made therefrom, whether or not in combination with sheet metal parts
- B21D3/02—Straightening or restoring form of metal rods, metal tubes, metal profiles, or specific articles made therefrom, whether or not in combination with sheet metal parts by rollers
- B21D3/04—Straightening or restoring form of metal rods, metal tubes, metal profiles, or specific articles made therefrom, whether or not in combination with sheet metal parts by rollers arranged on axes skew to the path of the work
-
- 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
Abstract
The invention discloses a shaft-part straightening device capable of adjusting the conveying speed. A machine body comprises a lower machine body part; an upper machine body part is arranged in front of the lower machine body part; two rotating output shafts are arranged in a gearbox; a fixed spindle seat is arranged at the left end of the upper machine body part; a sliding rail is arranged on the upper machine body part on the right side of the fixed spindle seat; a wheel shaft supporting board is arranged on the upper machine body part between the sliding rail and the fixed spindle seat; a movable spindle seat is connected onto the sliding rail in a sliding manner; the piston rod of a hydraulic cylinder is connected with the movable spindle seat; adjusting plates are mounted on the inner lateral surfaces of the fixed spindle seat and the movable spindle seat; spindles are mounted on the adjusting plates; the adjusting plates gradually tilt down from front to back; rollers are mounted on the spindles of the fixed spindle seat and the movable spindle seat in a sleeving manner; an annular concave surface is arranged outside one roller, and an annular convex surface is arranged outside the other roller; the spindles of the fixed spindle seat and the movable spindle seat are connected with the two rotating output shafts of the gearbox through cardan joints. The shaft-part straightening device is simple in structure and convenient to use.
Description
Technical field
The present invention relates to a kind of aligning axis part device that can regulate transporting velocity.
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 the another kind of aligning axis part device that can regulate transporting velocity easy to use.
To achieve these goals, technical scheme of the present invention is as follows: a kind of aligning axis part device that can regulate transporting velocity, 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 bolted adjustable plate (14), the adjustable plate (14) of described fixed main shaft seat (5) and movable spindle drum (7) is all one in front and one in back symmetrical 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 fixed main shaft seat (5) is parallel with the main shaft (10) of movable spindle drum (7), described adjustable plate (14) is downward-sloping gradually from front to back, 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),
Described fixed main shaft seat (5) is connected with two rotary output axis of gearbox (3) respectively by universal joint (4) with the main shaft (10) of movable spindle drum (7), and 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.
By regulating the vertical inclined degree of adjustable plate, even if the angle of inclination obtaining main shaft becomes large and diminishes, the adjustment of wheel shaft transporting velocity just can be realized.As: angle of inclination is large, and transporting velocity is fast, and angle of inclination is little, and transporting velocity is slow.
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.
In such scheme: the leading flank of described fixed main shaft seat (5) and movable spindle drum (7) is provided with scale (15) near adjustable plate (14).Scale is set, is convenient to the height of the adjustable plate controlling both sides, keep the parallel of both sides main shaft.
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, and speed is adjustable.
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: the aligning axis part device of transporting velocity that can regulate 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, adjustable plate 14, scale 15.
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.On lower fuselage 1, electrical control cubicles can also be installed.
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 bolted adjustable plate 14, the adjustable plate 14 of fixed main shaft seat 5 and movable spindle drum 7 is all one in front and one in back symmetrical 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, fixed main shaft seat 5 is parallel with the main shaft 10 of movable spindle drum 7, adjustable plate 14 is downward-sloping gradually from front to back, thus make main shaft 10 downward-sloping gradually from front to back, by regulating the gradient of adjustable plate 14, realize the gradient regulating main shaft 10, gradient is larger, the transporting velocity of wheel shaft is faster, gradient is less, the transporting velocity of wheel shaft is slower.Main shaft 10 on fixed main shaft seat 5 and movable spindle drum 7 is set with roller 12, and the middle part of one of them roller 12 outer surface arranges loop concave 12a, and 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 of 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 (4)
1. one kind can regulate the aligning axis part device of transporting velocity, 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 bolted adjustable plate (14), the adjustable plate (14) of described fixed main shaft seat (5) and movable spindle drum (7) is all one in front and one in back symmetrical 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 fixed main shaft seat (5) is parallel with the main shaft (10) on movable spindle drum (7), described adjustable plate (14) is downward-sloping gradually from front to back, 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),
Described fixed main shaft seat (5) is connected with two rotary output axis of gearbox (3) respectively by universal joint (4) with the main shaft (10) of movable spindle drum (7), and fixed main shaft seat (5) is relative with the roller (12) on movable spindle drum (7) to be rotated.
2. can regulate the aligning axis part device of transporting velocity 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. can regulate the aligning axis part device of transporting velocity 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.
4. can regulate the aligning axis part device of transporting velocity according to claim 1, it is characterized in that: the leading flank of described fixed main shaft seat (5) and movable spindle drum (7) is provided with scale (15) near adjustable plate (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510791950.5A CN105327976A (en) | 2015-11-17 | 2015-11-17 | Shaft-part straightening device capable of adjusting conveying speed |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510791950.5A CN105327976A (en) | 2015-11-17 | 2015-11-17 | Shaft-part straightening device capable of adjusting conveying speed |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105327976A true CN105327976A (en) | 2016-02-17 |
Family
ID=55278853
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510791950.5A Pending CN105327976A (en) | 2015-11-17 | 2015-11-17 | Shaft-part straightening device capable of adjusting conveying speed |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105327976A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109856962A (en) * | 2019-01-15 | 2019-06-07 | 浙江工业大学 | A kind of intelligence circular shaft type straightener main shaft adaptive-feedrate adjustment method |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007021524A (en) * | 2005-07-14 | 2007-02-01 | Daido Machinery Ltd | Device for restraining bar-like material and system for restraining bar-like material using restraining 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 |
| CN100430164C (en) * | 2004-07-01 | 2008-11-05 | 大同玛希纳利股份有限公司 | Straightener |
| 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 |
-
2015
- 2015-11-17 CN CN201510791950.5A patent/CN105327976A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100430164C (en) * | 2004-07-01 | 2008-11-05 | 大同玛希纳利股份有限公司 | Straightener |
| JP2007021524A (en) * | 2005-07-14 | 2007-02-01 | Daido Machinery Ltd | Device for restraining bar-like material and system for restraining bar-like material using restraining 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 |
| 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 |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109856962A (en) * | 2019-01-15 | 2019-06-07 | 浙江工业大学 | A kind of intelligence circular shaft type straightener main shaft adaptive-feedrate adjustment method |
| CN109856962B (en) * | 2019-01-15 | 2022-04-08 | 浙江工业大学 | Main shaft self-adaptive speed control method of intelligent round shaft straightening machine |
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| PB01 | Publication | ||
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| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160217 |