The present invention relates to a tyre component part production method and machine.
In the rubber industry, a tyre component part is made by gradually depositing a strip of green elastomeric material onto a rotary toroidal support, which may be a rigid core or a toroidal carcass of a tyre being built or retread.
The strip may be prefabricated or, as is more often the case, produced and applied by a profiling unit, which forms part of a machine comprising a spindle for rotating the toroidal support about its axis, and comprises a forming unit, in which the strip, formed directly by an extruder or shaped later by a calender, is fed to an applicator, normally a roller, which forms the tyre component part by applying the strip to a given surface of the rotary toroidal support until the surface is completely covered.
The forming operation is normally performed as described, for example, in U.S. Pat. No. 5,395,475, U.S. Pat. No. 7,641,752 and WO-2007/000443, by moving the applicator so that the point of application of the strip to the surface for covering moves, on the surface for covering, along a trajectory—hereinafter referred to as ‘application trajectory’—defined by the intersection of the surface for covering and a plane—hereinafter referred to as ‘reference plane’—which is always necessarily a radial plane, i.e. any one of the infinite number of planes in the sheaf of planes through the rotation axis of the surface for covering, which axis coincides with the axis of the rotary support.
During or after the forming operation, a stitching operation is performed to eliminate any air pockets trapped in the component part formed or being formed, and also, if the support is part of a tyre being built, to ensure perfect adhesion of the strip to the underlying material.
Like the forming operation, the stitching operation is also usually performed by moving a pressure roller of a stitching unit along the surface for stitching, so that the point of contact between the pressure roller and the surface to be stitched moves, on the surface to be stitched, along a trajectory—hereinafter referred to as ‘rolling trajectory’—defined by the intersection of the surface to be stitched and a plane—hereinafter referred to as ‘reference plane’—which, in the known art, e.g. EP-1775111, US2006/048884, DE-1579161, EP-1754592, U.S. Pat. No. 5,693,176 and JP-59188427, is always a radial plane as defined above.
In other words, known stitching units are all designed so that, during the stitching operation, the point of contact of the moving pressure roller is maintained substantially in a ‘reference plane’ selected from the infinite number of radial reference planes available.
This method is justified on the grounds that, if the support mounted on the spindle is rotated about its axis, the speed vector applied to each point along any ‘stitching trajectory’ of the type defined above extends perpendicularly to the ‘stitching trajectory’, so the pressure roller, whose point of contact with the surface to be stitched moves along the selected ‘stitching trajectory’ and in the relative radial ‘reference plane’, rolls without sliding or skidding at any point along the selected ‘stitching trajectory’.
Forming and stitching as described above pose no problems when the forming and stitching trajectories are straight (forming and stitching cylindrical surfaces), and/or forming and stitching are performed at different times (stitching after forming), and/or the forming and stitching units are completely independent, as in EP-1754592.
Conversely, problems still unsolved are posed when:
Such is the case, for example, when producing shoulders and sidewalls of large-sized tyres, e.g. for farm vehicles or heavy-duty earthmoving machines. In which case, the height of the sidewall may be 70-80% of the support radius, and the size and weight of the strip normally demand practically immediate stitching.
In other words, in such cases, the stitching unit must follow closely behind the forming unit throughout the forming operation, and both units must move in unison along the respective trajectories.
In connection with the above, the major problem is not so much devising mechanical devices capable of moving the forming and stitching units simultaneously along their respective trajectories, as the fact that :
interference between the forming and stitching units, close to the inner periphery of the sidewall, becomes inevitable, thus making it practically impossible to stitch newly applied strips at that point correctly.
It is an object of the present invention to provide a method and machine for producing a tyre component part by gradual deposition of a strip, and designed to eliminate any interference between the forming and stitching units when covering and stitching a surface comprising at least one portion extending crosswise to the rotation axis of the support.
According to the present invention, there is provided a tyre component part production method as claimed in claim 1 and preferably in any one of the following Claims depending directly or indirectly on claim 1.
According to the present invention, there is also provided a tyre component part production machine as claimed in claim 4 and preferably in any one of the following Claims depending directly or indirectly on claim 4.
A non-limiting embodiment of the present invention will be described by way of example with reference to the accompanying drawings, in which :
Number 1 in
In the example shown, strip 7 is deposited onto surface 4 by a forming unit 8 and along a path P, which extends along a cylindrical coil at cylindrical lateral portion 5, and along a spiral at each of annular end portions 6. Forming unit 8 comprises an applicator roller 9 positioned contacting surface 4 at an application point 10 which, during the forming operation, moves along an application trajectory 11 crosswise to path P. Application trajectory 11 is normally U-shaped, and is defined by the intersection of surface 4 and a radial plane P1, i.e. one of the infinite number of planes in the sheaf through axis 3. Plane P1 may be tilted at any angle, which normally depends on the size of the other devices (not shown) around spindle 2.
Plane P1 being radial, the speed vector V1 applied at each instant to each point along application trajectory 11 differs from one point to another, and is perpendicular to application trajectory 11 and plane P1, so strip 7 does not slip laterally on surface 4 at application point 10.
In the known art shown in
This is prevented, on the other hand, using the solution shown schematically in
In this case, the speed vectors V2 applied to points along stitching trajectory 16 are not all perpendicular to stitching trajectory 16, but tilt at increasing angles as they get closer to axis 3. So, to ensure slipfree stitching, pressure roller 13 is allowed to oscillate about an axis 19, which is crosswise to axis 14 and stitching trajectory 16, and is translated parallel to plane P1 to move contact point 15 along stitching trajectory 16 as application point 10 moves along application trajectory 11.
In other words, as axis 19 translates, any point C along axis 19 moves in a plane P3 parallel to plane P1 and intersecting surface 4.
Plane P3 being merely parallel to plane P1 allows the designer absolute freedom of choice by enabling location of stitching unit 18 in any number of positions with respect to spindle 2 and forming unit 8, with no interference between application trajectory 11 and stitching trajectory 16.
Planes P1 and P3 being parallel, spindle 2, forming unit 8 and stitching unit 18 can be incorporated in profiling unit 17, which is a perfected profiling unit as shown in
With reference to
The top end of bed 20 is fitted with a guide 27, which extends in a horizontal direction 28 diametrical with respect to pivot 21 and axis 22, and is fitted with a powered bottom slide 29 of an operating head 30 housing forming unit 8 and profiling unit 17.
Operating head 30 comprises two parallel, opposite vertical plates 31, 32, which are parallel to direction 28, extend upwards from slide 29, and are connected to each other, close to their front edges 33, by a horizontal pin 34 having an axis 35 perpendicular to plates 31, 32 and crosswise to direction 28. Applicator roller 9 is mounted idly on pin 34, is located between plates 31 and 32, projects partly frontwards from front edges 33, and is designed to receive a strip 7 of elastomeric material, as shown in
As shown in
To the front of the front end of guide 27, profiling unit 17 comprises a plate 40, which is normally in a vertical position perpendicular to direction 28, and forms part of a thrust device 41 of stitching unit 18.
Thrust device 41 comprises a lever 42 located on the outside of plate 32, hinged at its top end to pin 34 to oscillate about axis 35, and fitted on its bottom end with plate 40; and an air-powered jack 43 substantially parallel to direction 28, and which is hinged at its front end to an intermediate point of lever 42, and at its rear end to a bracket 44 fitted to the rear of operating head 30.
Stitching unit 18 comprises a horizontal slide assembly 45 for a bracket 46 supporting pressure roller 13. More specifically, slide assembly 45 comprises two horizontal guides 47 parallel to axis 35, integral with plate 40, and fitted one above the other to a front surface of plate 40; a slide 48 mounted to slide along guides 47 in a horizontal direction 49 crosswise to direction 28 and parallel to axis 35; and an actuating device 50 comprising a screw 51 parallel to guides 47 and fitted in rotary manner to plate 40, beneath guides 47, by two brackets 52. Screw 51 is fitted to a bottom appendix of slide 48 by a screw-nut screw coupling 53, and is connected by a bevel gear coupling 54 to the output shaft of a motor 55 fitted to plate 40 and substantially parallel to direction 28.
The top end of slide 48 is fitted with a pin 56, which idly supports bracket 46, lies in a vertical plane perpendicular to the plane of plate 40, and has an axis preferably (as in the example shown) but not necessarily sloping upwards, and the point C of which is indicated by way of example at the top end of pin 56.
Bracket 46, viewed from the side, is substantially V-shaped, and, viewed from the front, is annular and defined by two side by side arms 57 connected to each other by a top cross member 58 and a bottom cross member 59.
Top cross member 58 has a through hole parallel to the plane of arms 57 and engaged in rotary manner by pin 56; and bottom cross member 59 is fitted with a counterweight 60 projecting downwards from bracket 46. Arms 57 define a double supporting fork by means of a pin 61 crosswise to pin 56 and coaxial with axis 14 of pressure roller 13, which projects frontwards from bracket 46 and oscillates idly about axis 19 of pin 56.
In other words, pressure roller 13 of stitching unit 18 is movable by slide 48, in direction 49, beneath and from one side to the other of applicator roller 9; is suspended by bracket 46 from pin 56 to oscillate about axis 19; rotates about the axis of pin 61 with respect to bracket 46; and is normally maintained by counterweight 60 in the vertical position shown in
In actual use, to deposit strip 7 of green elastomeric material to gradually form a layer (not shown) covering cylindrical lateral portion 5 of support 1, machine A is set up alongside support 1, with axis 35 parallel to axis 3, with the periphery of applicator roller 9 contacting cylindrical lateral portion 5 at an application point 10 located in a plane P1 which, in the example shown, is a horizontal radial plane, and with pressure roller 13 centred beneath applicator roller 9 and pushed by thrust device 41 into contact with support 1 at a point 15 on surface S, which is located beneath and a given mean distance from plane P1. In this position, point C of axis 19 is located in plane P3 parallel to plane P1 and in an intermediate position between surface S and plane P1.
When forming the layer (not shown), support 1 is rotated clockwise, in
To gradually cover a lateral end portion 6 of support 1 with a strip 7 of green elastomeric material to form a sidewall 62, as shown in
When support 1 is rotated clockwise, in
In connection with the above, it should be noted that, given its initial vertical position, pressure roller 13, when it begins stitching on lateral end portion 6, is subjected to transverse forces, which lift it about axis 19 into a plane whose tilt angle, like that of speed vector V2, varies with the position of point 15 along trajectory 16, thus enabling pressure roller 13 to stitch the deposited strip 7 correctly, with a practically zero skid angle along path P, which in this case is spiral-shaped.
In connection with the above, it should be noted that the tilted position described is a position of stable dynamic equilibrium, in that downward rotation of bracket 46, about axis 19 and with respect to the tilted position, results immediately in the onset, between pressure roller 13 and lateral end portion 6, of forces directed axially with respect to pressure roller 13, and which restore pressure roller 13 to the stable tilted position. And, conversely, upward rotation of bracket 46, about axis 19 and with respect to the tilted position, produces a corresponding increase in the moment generated by counterweight 60 about axis 19, to restore bracket 46 to the stable tilted position.
It should be noted that, regardless of the surface for covering, slide assembly 45 can be adjusted slightly to position pressure roller 13 at either one of the lateral edges of the deposited strip 7.
Moreover, the fact that pressure roller 13 moves towards support 1 along a circular trajectory coaxial with axis 35 enables contact point 15 between pressure roller 13 and support 1 to be kept as close as possible to contact point 10 between applicator roller 9 and support 1, i.e. the point at which strip 7 is deposited.
Finally, it is important to note that, if surface S contained axis 3, it would be impossible for a profiling machine with a built-in stitching unit, such as profiling unit 17, to operate correctly.
Number | Date | Country | Kind |
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TO2010A000348 | Apr 2010 | IT | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/IB2011/000899 | 4/26/2011 | WO | 00 | 1/22/2013 |