CN1962246A - Meridian line tyre forming method - Google Patents
Meridian line tyre forming method Download PDFInfo
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- CN1962246A CN1962246A CN 200510110125 CN200510110125A CN1962246A CN 1962246 A CN1962246 A CN 1962246A CN 200510110125 CN200510110125 CN 200510110125 CN 200510110125 A CN200510110125 A CN 200510110125A CN 1962246 A CN1962246 A CN 1962246A
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- drum
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- tyre
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Abstract
The invention relates to a method for shaping radial-type tyre, wherein it eliminates the tyre expansion and adhere process between tyre and beam layer, but directly adheres the beam layer on the tyre after shaping the tyre on shaping drum. The invention can simplify the radial-type tyre shaping machine, to reduce the cost. And it can use semi-drum or semi-corn shaping drum. The invention can shape the radial-type tyre without zero-degree beam structure.
Description
Technical field:
The present invention relates to a kind of tire moulding method, particularly a kind of fiber radial and whole steel wire radial tyre belt assembly method of not having the zero degree belt structure.
Background technology:
In the existing technology, the forming method of fiber radial and whole steel wire radial tyre generally is divided into post forming method and once moulding method.The post forming method is that moulding is divided into first stage building and second stage building, first stage building can adopt half drum-type, semi-core wheeled or core wheeled assembly drum moulding carcass shell, shrink or the folding forming drum, take off the carcass shell of first stage building, be placed on the second stage building machine head, two sections heads (no matter having or not the capsule drum) are inflated and are made carcass expand into specified diameter with carcass shell bead lock and while shrinking bead spacing of tyre, this moment the belt of fitting, tyre surface, or with the good band bundle of combination forming on band bundle laminating drum, tread rings is fitted, and then is shaped to radial-ply tyre green tire embryo through some processing steps again; Once moulding method is one section, two sections functions merging with the post forming method, the form of make-up machine can be divided into two drum-types, three drum-type, four-drum and pipeline system etc., its key character is that carcass building drum is a drum-type, also available mechanical transfer is accurately located after the carcass moulding, carcass building drum is then locked the distance of shrinking behind the tyre bead between the tyre bead on one side, inflation on one side makes carcass expand into specified diameter, has special-purpose band bundle laminating drum that belt, tyre surface are fitted simultaneously and forms band bundle tread rings.Come clamping band bundle tread rings with the mechanical transfer ring, it is delivered to accurate centering on the carcass building drum.This moment, carcass building drum further shrank bead spacing of tyre to setting, carcass and interior week of band bundle tread rings are fitted, and belt layer tread ring external diameter was the fetus diameter.From the fetus diameter to the expansion rate tyre vulcanization die cavity internal diameter generally about 2%.Above-mentioned post forming method and once moulding method have common characteristics, be body piles must be become the garden curved annular from its barrel expansion of fitting between two wire loops that form at assembly drum in the tire building process, after expanding into the process stipulation diameter, its external diameter could fit with belt or band bundle tread rings, just because of this technical process and radial-ply tyre high request, make the radial tire building machine complexity that becomes to formed precision.The fetus that existing technological forming is made is the circular arc ring-type, and is very approaching with the finished product the form of the foetus shape after the sulfuration, but its external diameter is smaller.
Summary of the invention:
The purpose of this invention is to provide a kind of simple and effective radial forming method.
To achieve these goals, technical scheme of the present invention is: a meridian line tyre forming method comprises following steps: A, the carcass of the expandable auxilliary drum of fitting is stretched to working diameter, finish the moulding of carcass bandage; B, the vacuum suction transmission ring is enclosed within on the carcass bandage and the centering location, laminating drum stretches to second working diameter, by transmission ring the carcass bandage is adsorbed, and laminating drum shrinks, and transmission ring shifts out the carcass bandage; C, the composite set in the main drum outside of moulding is removed, the main drum of moulding shrinks, and a steel wire snare overmolding master drum that has posted triangle glue is placed on the bead ring in the inboard composite set, and another is placed on the bead ring in the composite set of the outside; D, transmission ring move, and with carcass cord jacket casing centering location on the main drum of moulding, the main drum of moulding stretches to working diameter, transmission ring discharges the carcass bandage, and the carcass bandage shrinks, and bag is attached on the main drum drum of the moulding face, transmission ring withdraws to be removed, and the main drum of moulding outside composite set resets; E, the main bulging both sides of moulding composite set synchronous working are finished successively and are just being wrapped the action of button circle anti-package; F, location applying tyre bead enhancement Layer, the composite members of glue is filled on location applying tyre bead toe mouth encapsulate or toe mouth encapsulate and sidewall; G, by the feed frame feed, location each layer belt of fitting successively, tyre surface, sidewall are finished the tire base and are made; H, the main drum outside of moulding composite set is removed, the main bulging diameter of moulding shrinks, and takes out the tire base.
The present invention improves present radial-ply tyre moulding process, has promptly cancelled the technology that carcass in the radial-ply tyre forming process expands and to fit with belt, but after the carcass forming, need not expand on assembly drum, directly belt is fitted on the carcass.The present invention can make the radial tire building machine structure simplify relatively, and the equipment making cost reduces significantly, and moulding board area occupied is less.Because the present invention can allow to use half drum-type or semi-core wheeled assembly drum, design is adjusted and is brought higher flexibility for tire construction.
The specific embodiment:
Below the present invention will be further described.
One meridian line tyre forming method comprises following steps: A, the carcass of the expandable auxilliary drum of fitting is stretched to working diameter, applying inner liner and casingply on carcass is fitted auxilliary drum are finished the moulding of carcass bandage; B, the vacuum suction transmission ring is enclosed within on the carcass bandage and the centering location, laminating drum stretches to second working diameter, by transmission ring the carcass bandage is adsorbed, and laminating drum shrinks, and transmission ring shifts out the carcass bandage; C, the composite set in the main drum outside of moulding is removed, the main drum of moulding shrinks, and a steel wire snare overmolding master drum that has posted triangle glue is placed on the bead ring in the inboard composite set, and another is placed on the bead ring in the composite set of the outside; D, transmission ring move, and with carcass cord jacket casing centering location on the main drum of moulding, the main drum of moulding stretches to working diameter, transmission ring discharges the carcass bandage, and the carcass bandage shrinks, and bag is attached on the main drum drum of the moulding face, transmission ring withdraws to be removed, and the main drum of moulding outside composite set resets; E, the main bulging both sides of moulding composite set synchronous working are finished successively and are just being wrapped the action of button circle anti-package; F, location applying tyre bead enhancement Layer, the composite members of glue is filled on location applying tyre bead toe mouth encapsulate or toe mouth encapsulate and sidewall; G, by the feed frame feed, location each layer belt of fitting successively, tyre surface, sidewall are finished the tire base and are made; H, the main drum outside of moulding composite set is removed, the main bulging diameter of moulding shrinks, and takes out the tire base, is placed on the tyre blank storage frame.
Wherein in steps A, the auxilliary drum of carcass applying of expandable is stretched to the applying working diameter, by inner liner and carcass cord feed frame feed, inner liner feed frame end is displaced near the auxilliary drum drum face of fitting, draw the inner liner end and be fitted on the bulging face, with methods such as pressing magnet piece or abrasive paper this termination is fixed on the laminating drum, the auxilliary drum of fitting rotates a week along the applying direction, assist drum and rotate simultaneously, feed frame is to assist the synchronous feed of drum linear resonance surface velocity a little less than fitting; Manual severing, the withdrawal of feed frame termination, plain adapter connects the jail; The auxilliary drum of fitting rotates an angle, so that inner liner joint and carcass cord joint are staggered; Similarly, the applying casingply splices cord with splicer, uses the nip drum compacting, finishes the moulding of carcass bandage.In step C, the main bulging both sides of moulding respectively have the positive and negative bag of carcass cloth tube and buckle the composite set of circle function with a cover, in step F, if tire construction has shoulder wedge, then also should locate the applying shoulder wedge on the drum face.In step G, also need locate tyre surface sidewall composite members sometimes, in addition, main drum of moulding and carcass are fitted to assist to rouse and are respectively with several groups of corresponding rolling devices, in forming process, can suitably set and carry out roll extrusion according to getting rid of bubble and the smooth closely knit actual needs of fitting with corresponding rolling device.
In the above-mentioned forming process, may also have some parts to need to fit for different structure, because the realization of each step process is compared with existing technology, it is any special to there is no, and is easy to realize, so omitted.This a kind of forming method can be realized on the shaping machine set that includes make-up machine main frame, half drum-type master drum, the auxilliary drum of carcass applying, carcass transmission ring and feeding device.
According to radial forming method of the present invention, it is characterized in that the main drum of moulding is half drum-type or semi-core wheeled assembly drum, when carcass on the main drum of moulding after the moulding, need not carcass to be fitted after expanding with the band bundle again, but directly will band restraint on applying and the carcass that assembly drum is close to mutually while shrinking bead spacing of tyre.
The present invention improves present radial-ply tyre moulding process, has promptly cancelled the technology that carcass in the radial-ply tyre forming process expands and to fit with belt, but after the carcass forming, need not expand on assembly drum, directly belt is fitted on the carcass.This moulding process needs according to the diameter of finished product requirement and assembly drum semi-products parameter, physical dimension, the particularly width of belt semi-products, angle, thickness and the tyre surface section physical dimension of each parts to be carried out particular design.The semi-products width of belt and angle all need to calculate preliminary definite by following two principle according to the rate that is radially expanded from fetus to the finished product belt: the area of each layer belt equates with corresponding each layer belt area in the finished product (1) tire base; (2) the severing angle [alpha] of each layer band bundle
1With corresponding belt angle [alpha] in finished product
2Between relation obey following formula:
Sinα
1/R
1＝Sinα
2/R
2
In the formula, R
1--belt applying radius in the-moulding
R
2--belt ring radius in the-finished product.
Then need be by trial-production test, formally determine after doing suitable adjustment correction.
Once moulding method of the present invention is different from two present drums or rouses once moulding method and streamline moulding process more.The meridian fetus shape of once moulding method of the present invention institute moulding is similar to common oblique tire tire base shape, near tubular, and is different from the radial tyre blank near finished product the form of the foetus shape of present various radial-ply tyre method of forming institute moulding.Adopt once moulding method of the present invention, its fetus must be finalized the design through curing bag in vulcanization process, thereby makes the tubular fetus expand into ring-type, when its profile expand into less than cover tire model internal diameter 2-3%, stops typing, matched moulds sulfuration immediately; But also vulcanize after the outer typing of machine, also the sulfuration process with common oblique tire is identical for this again.
The present invention can make the radial tire building machine designs simplification, and the equipment making cost reduces significantly, and moulding board area occupied is less.Because the present invention can allow to use half drum-type or semi-core wheeled assembly drum, design is adjusted and is brought higher flexibility for tire construction.Adopt radial forming method of the present invention, can carry out common technological design to half and half article component by at product design requirement and assembly drum physical dimension.Can realize the fetus moulding of the radial of any no zero degree belt structure by the technological operation of standard, then can become the tire finished product that meets design requirement through sulfuration.
Claims (2)
1, a meridian line tyre forming method comprises following steps: A, the carcass of the expandable auxilliary drum of fitting is stretched to working diameter, finish the moulding of carcass bandage; B, the vacuum suction transmission ring is enclosed within on the carcass bandage and the centering location, laminating drum stretches to second working diameter, by transmission ring the carcass bandage is adsorbed, and laminating drum shrinks, and transmission ring shifts out the carcass bandage; C, the composite set in the main drum outside of moulding is removed, the main drum of moulding shrinks, and a steel wire snare overmolding master drum that has posted triangle glue is placed on the bead ring in the inboard composite set, and another is placed on the bead ring in the composite set of the outside; D, transmission ring move, and with carcass cord jacket casing centering location on the main drum of moulding, the main drum of moulding stretches to working diameter, transmission ring discharges the carcass bandage, and the carcass bandage shrinks, and bag is attached on the main drum drum of the moulding face, transmission ring withdraws to be removed, and the main drum of moulding outside composite set resets; E, the main bulging both sides of moulding composite set synchronous working are finished successively and are just being wrapped the action of button circle anti-package; F, location applying tyre bead enhancement Layer, the composite members of glue is filled on location applying tyre bead toe mouth encapsulate or toe mouth encapsulate and sidewall; G, by the feed frame feed, location each layer belt of fitting successively, tyre surface, sidewall are finished the tire base and are made; H, the main drum outside of moulding composite set is removed, the main bulging diameter of moulding shrinks, and takes out the tire base.
2, radial forming method as claimed in claim 1, it is characterized in that when carcass on the main drum of moulding after the moulding, directly will be with on the carcass that bundle is fitted with assembly drum is close to mutually.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2005101101250A CN100467261C (en) | 2005-11-08 | 2005-11-08 | Meridian line tyre forming method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2005101101250A CN100467261C (en) | 2005-11-08 | 2005-11-08 | Meridian line tyre forming method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1962246A true CN1962246A (en) | 2007-05-16 |
| CN100467261C CN100467261C (en) | 2009-03-11 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2005101101250A Active CN100467261C (en) | 2005-11-08 | 2005-11-08 | Meridian line tyre forming method |
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| CN (1) | CN100467261C (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101934595A (en) * | 2009-07-02 | 2011-01-05 | 上海轮胎橡胶（集团）股份有限公司轮胎研究所 | All-steel radial engineering tire semi-drum type tri-drum single-stage building machine |
| CN105196584A (en) * | 2015-08-25 | 2015-12-30 | 江苏通用科技股份有限公司 | Method for preventing connector of tire blank inner liner from cracking |
| CN111674071A (en) * | 2020-06-18 | 2020-09-18 | 青岛双星轮胎工业有限公司 | Meridian aircraft tire forming process |
| CN113910832A (en) * | 2021-11-22 | 2022-01-11 | 三角轮胎股份有限公司 | Meridian aircraft tire |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5354404A (en) * | 1990-05-25 | 1994-10-11 | Cooper Tire & Rubber Company | Control for integrated tire building system |
| DE19742035C1 (en) * | 1997-09-24 | 1999-04-08 | Continental Ag | Method and drum as a device for building a green tire |
| FR2797213B1 (en) * | 1999-08-02 | 2002-08-30 | Michelin Soc Tech | PROCESS FOR THE MANUFACTURE OF A TIRE WITH PRECONFORMATION OF A RADIAL CARCASS SHEET TO MOUNT THE CABLES OF THE CENTRAL PART |
| CN1162270C (en) * | 2000-12-29 | 2004-08-18 | 张建浩 | One-pass shaper for load-beary full-wire meridian tyre |
| RU2302341C2 (en) * | 2002-04-09 | 2007-07-10 | Матадор а.с. | Method and the installation of manufacture of the non-vulcanized tires |
| SK13172003A3 (en) * | 2003-10-22 | 2005-05-05 | Matador A. S. | System of devices for production unvulcanized radial automobile tyres and method for the production thereof |
-
2005
- 2005-11-08 CN CNB2005101101250A patent/CN100467261C/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101934595A (en) * | 2009-07-02 | 2011-01-05 | 上海轮胎橡胶（集团）股份有限公司轮胎研究所 | All-steel radial engineering tire semi-drum type tri-drum single-stage building machine |
| CN101934595B (en) * | 2009-07-02 | 2013-03-20 | 上海轮胎橡胶（集团）股份有限公司轮胎研究所 | All-steel radial engineering tire semi-drum type tri-drum single-stage building machine |
| CN105196584A (en) * | 2015-08-25 | 2015-12-30 | 江苏通用科技股份有限公司 | Method for preventing connector of tire blank inner liner from cracking |
| CN105196584B (en) * | 2015-08-25 | 2017-05-17 | 江苏通用科技股份有限公司 | Method for preventing connector of tire blank inner liner from cracking |
| CN111674071A (en) * | 2020-06-18 | 2020-09-18 | 青岛双星轮胎工业有限公司 | Meridian aircraft tire forming process |
| CN111674071B (en) * | 2020-06-18 | 2022-01-25 | 青岛双星轮胎工业有限公司 | Meridian aircraft tire forming process |
| CN113910832A (en) * | 2021-11-22 | 2022-01-11 | 三角轮胎股份有限公司 | Meridian aircraft tire |
| CN113910832B (en) * | 2021-11-22 | 2024-05-28 | 三角轮胎股份有限公司 | Meridian aviation tyre |
Also Published As
| Publication number | Publication date |
|---|---|
| CN100467261C (en) | 2009-03-11 |
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