CN104525798A - Aviation tire radial tire bead ring production line - Google Patents
Aviation tire radial tire bead ring production line Download PDFInfo
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- CN104525798A CN104525798A CN201410801930.7A CN201410801930A CN104525798A CN 104525798 A CN104525798 A CN 104525798A CN 201410801930 A CN201410801930 A CN 201410801930A CN 104525798 A CN104525798 A CN 104525798A
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- wire
- production line
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- winding
- aviation
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Abstract
The invention provides an aviation tire radial tire bead ring production line. The production line is characterized by comprising an opening guiding machine, a wire removing device, an extruder, a traction storing device, a retaining and prebending device, a wire arranging device, a winding device and an operating table, wherein the opening guiding machine, the wire removing device, the extruder, the traction storing device, the retaining and prebending device, the wire arranging device, the winding device and the operating table are sequentially arranged according to the working procedures. A steel wire breaking monitoring device and a steel wire moving speed monitoring device are arranged between the opening guiding machine and the wire removing device. The retaining and prebending device enables the diameter of bent steel wires to be the same as that of steel wires finally produced. A winding plate for producing the steel wires of different specifications can be installed on the winding device. The operating table is provided with an Ethernet interface. The aviation tire radial tire bead ring production line is high in production efficiency, winding is close, and the section shape is stable.
Description
Technical field
The present invention relates to wire loop production line, be specifically related to a kind of aviation tire Ring for Meridian Tyre production line.
Background technology
Wire loop is vitals tire playing carrying and safety effect, and the shape according to section is classified, and wherein hexagonal wire loop is mainly used in the giant tire such as high-capacity tyre and engineering tyre.In the production of giant tire, wire loop needs to have been produced by a set of wire loop production line with finer wire, current production line produce giant tire time locate not accurate enough, be wound around efficiency low, repeatability poor.
Summary of the invention
For solving the problems of the technologies described above, the invention provides a kind ofly to be wound around closely, cross sectional shape is stablized, production efficiency is high aviation tire Ring for Meridian Tyre production line.
The technical solution adopted in the present invention is: a kind of aviation tire Ring for Meridian Tyre production line, comprise be arranged in order according to operation lead start, clear silk device, extruder, traction storage device, retaining and prebuckling device, thread arranging device, wind, operating desk, described leading between start and clear silk device is provided with steel wire fracture of wire monitoring device, steel wire translational speed monitoring device, described retaining and prebuckling device the diameter of steel wire bent is identical with the diameter of the wire loop of final production, described wind can install the winding disc producing different size wire loop, described operating desk arranges Ethernet interface.
Preferably, the section configuration of described wire loop is square or hexagon.
Preferably, the internal diameter of described wire loop is 8-42 cun.
The invention has the beneficial effects as follows: the present invention can automatic winding wire loop, accurate positioning, reproducible, is realized the control of full production line, arrange Ethernet interface, conveniently upload device fabrication parameter at operating desk by the man-machine interface management of operating desk; The winding disc of replaceable different size, be applicable to the production of huge aviation tire and common agricultural tire, it is convenient to change, and is no more than 10 minutes; Steel wire fracture of wire monitoring device, steel wire translational speed monitoring device are set, monitor the situation of steel wire at any time.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
In figure: 1. lead start, 2. steel wire fracture of wire monitoring device, 3. steel wire translational speed monitoring device, 4. clear silk device, 5. extruder, 6. draw storage device, 7. retaining and prebuckling device, 8. thread arranging device, 9. wind, 10. operating desk.
Detailed description of the invention
Below in conjunction with accompanying drawing, specific embodiments of the invention are elaborated.
As shown in Figure 1, a kind of aviation tire Ring for Meridian Tyre production line, comprise be arranged in order according to operation lead start 1, clear silk device 4, extruder 5, traction storage device 6, retaining and prebuckling device 7, thread arranging device 8, wind 9, operating desk 10.Operating desk 10 has fault diagnosis, parameter display, setting specifications parameter, stores the functions such as specifications parameter, warning and protection; lead between start 1 and clear silk device 4 and be provided with steel wire fracture of wire monitoring device 2, steel wire translational speed monitoring device 3; retaining and prebuckling device 7 diameter of steel wire bent is identical with the diameter of the wire loop of final production; wind 9 can install winding disc; the wire loop that production section is hexagon, internal diameter is 42 cun; operating desk 10 arranges Ethernet interface, so that uploading device manufacturing parameter.
During production, with the special steel wire of rolling for raw material, through leading out, decontamination, laser heating, kiss-coating, traction storage, prebuckling, row's silk, be wound around one-shot forming, produce finished steel wire ring.
Above one embodiment of the present of invention have been described in detail, but described content being only preferred embodiment of the present invention, can not being considered to for limiting practical range of the present invention.All equalizations done according to the present patent application scope change and improve, and all should still belong within patent covering scope of the present invention.
Claims (3)
1. an aviation tire Ring for Meridian Tyre production line, it is characterized in that: comprise be arranged in order according to operation lead start, clear silk device, extruder, traction storage device, retaining and prebuckling device, thread arranging device, wind, operating desk, described leading between start and clear silk device is provided with steel wire fracture of wire monitoring device, steel wire translational speed monitoring device, described retaining and prebuckling device the diameter of steel wire bent is identical with the diameter of the wire loop of final production, described wind can install the winding disc producing different size wire loop, described operating desk arranges Ethernet interface.
2. a kind of aviation tire Ring for Meridian Tyre production line according to claim 1, is characterized in that: the section configuration of described wire loop is square or hexagon.
3. a kind of aviation tire Ring for Meridian Tyre production line according to claim 1 and 2, is characterized in that: the internal diameter of described wire loop is 8-42 cun.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410801930.7A CN104525798A (en) | 2014-12-19 | 2014-12-19 | Aviation tire radial tire bead ring production line |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410801930.7A CN104525798A (en) | 2014-12-19 | 2014-12-19 | Aviation tire radial tire bead ring production line |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104525798A true CN104525798A (en) | 2015-04-22 |
Family
ID=52841529
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410801930.7A Pending CN104525798A (en) | 2014-12-19 | 2014-12-19 | Aviation tire radial tire bead ring production line |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104525798A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201040424Y (en) * | 2007-06-01 | 2008-03-26 | 昊华南方(桂林)橡胶有限责任公司 | Hexagonal steel traveler winding producing line |
| CN102189202A (en) * | 2011-03-29 | 2011-09-21 | 天津赛象科技股份有限公司 | Six-station radial tyre steel wire ring production line |
| CN202052891U (en) * | 2011-03-29 | 2011-11-30 | 天津赛象科技股份有限公司 | Six-position steel wire ring production line of radial ply tire |
| CN202667517U (en) * | 2012-04-27 | 2013-01-16 | 澳星机电科技无锡有限公司 | Six-station tyre steel wire coil production line |
| CN204413006U (en) * | 2014-12-19 | 2015-06-24 | 天津隆达伟业橡胶机械有限公司 | A kind of aviation tire Ring for Meridian Tyre production line |
-
2014
- 2014-12-19 CN CN201410801930.7A patent/CN104525798A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201040424Y (en) * | 2007-06-01 | 2008-03-26 | 昊华南方(桂林)橡胶有限责任公司 | Hexagonal steel traveler winding producing line |
| CN102189202A (en) * | 2011-03-29 | 2011-09-21 | 天津赛象科技股份有限公司 | Six-station radial tyre steel wire ring production line |
| CN202052891U (en) * | 2011-03-29 | 2011-11-30 | 天津赛象科技股份有限公司 | Six-position steel wire ring production line of radial ply tire |
| CN202667517U (en) * | 2012-04-27 | 2013-01-16 | 澳星机电科技无锡有限公司 | Six-station tyre steel wire coil production line |
| CN204413006U (en) * | 2014-12-19 | 2015-06-24 | 天津隆达伟业橡胶机械有限公司 | A kind of aviation tire Ring for Meridian Tyre production line |
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| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20150422 |
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| RJ01 | Rejection of invention patent application after publication |