CURING MOLD FOR A TIRE, COMPRISING MEANS FOR CUTTING A RUBBER MOLD SEAM
20230356489 · 2023-11-09
Inventors
Cpc classification
B29D2030/0613
PERFORMING OPERATIONS; TRANSPORTING
B29D30/0681
PERFORMING OPERATIONS; TRANSPORTING
B29D30/0606
PERFORMING OPERATIONS; TRANSPORTING
B29C2793/0054
PERFORMING OPERATIONS; TRANSPORTING
B29C37/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
B29D30/06
PERFORMING OPERATIONS; TRANSPORTING
B29D30/68
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A curing mold (10) for a tire comprises: a plurality of circumferentially distributed sectors (18) that are intended to mold the tread of the tire, at least one sipe blade (40) intended to mold a void in the tread, the sipe blade extending over two adjacent sectors (18) such that the sipe blade comprises a part (40a, 40b) in each of the two sectors, the two parts of the sipe blade being separated, in the closed position of the mold, by a space (26) that creates flash during the curing of a tire, the parts of the sipe blade comprising cutting means (38) that are able to cut off the flash during the opening of the mold.
Claims
1.-12. (canceled)
13. A tire curing mold (10) comprising: a plurality of circumferentially distributed sectors (18) that are intended to mold the tread of the tire; and at least one sipe blade (40) intended to mold a void in the tread, the sipe blade extending over two adjacent sectors (18) such that the sipe blade comprises a part (40a, 40b) in each of the two sectors, the two parts of the sipe blade being separated, in a closed position of the mold, by a space (26) that creates flash during curing of a tire, the two parts of the sipe blade comprising cutting means (38) that are able to cut off the flash during opening of the mold.
14. The tire curing mold according to claim 13, wherein each of the parts of the sipe blade (24) comprises an edge (36) partially delimiting the space (26), the cutting means (38) being arranged on the edge of at least one of the parts of the sipe blade such that the cutting means (38) cut off the flash during withdrawal from the tire, each of the parts of the sipe blade (24) being able to be withdrawn during the opening of the mold.
15. The tire curing mold according to claim 14, wherein the cutting means (38) are arranged on the edge (36) of each of the parts of the sipe blade, the cutting means of each of the parts of the sipe blade (24) having complementary shapes.
16. The tire curing mold according to claim 14, wherein the cutting means (38) are integral with the edge (36) of at least one of the parts of the sipe blade (24).
17. The tire curing mold according to claim 13, wherein the cutting means (38) have a recessed and/or protruding shape.
18. The tire curing mold according to claim 13, wherein the space (26) has a length (L) of between 0.2 and 20 mm.
19. The tire curing mold according to claim 13, wherein the space (26) has a thickness (E) of between 0.1 and 3 mm.
20. The tire curing mold according to claim 13, wherein the sipe blade (40) has a thickness of between 0.2 and 20 mm.
21. The tire curing mold according to claim 13, wherein the cutting means (38) have the shape of a triangular or crenellated toothing.
22. The tire curing mold according to claim 13, wherein the cutting means (38) are obtained by way of a process of consolidation by selective melting.
23. A method for manufacturing a tire comprising a step of curing a tire in the tire curing mold according to claim 13.
24. A tire intended to be mounted on a rim of a wheel, wherein the tire is obtained by the manufacturing method according to claim 23.
Description
[0023] The invention will be understood better from the rest of the description, which is based on the following figures:
[0024]
[0025]
[0026]
[0027] In the various figures, elements that are identical or similar bear the same reference signs. Their description is therefore not systematically repeated.
[0028]
[0029] Throughout the following text and unless indicated to the contrary, an axial direction denotes a direction parallel to the central axis 12, a radial direction 16 denotes a direction perpendicular to and intersecting the central axis 12, and a circumferential direction denotes a direction perpendicular to a radial direction 16 and to the central axis 12.
[0030] The mould 10 more particularly comprises a plurality of sectors 18 intended to mould the tread of the tyre, two shells 20 intended to mould the sidewalls of the tyre, and two rings 22 intended to mould the beads of the tyre. In the closed position of the mould, the sectors 18 are distributed circumferentially with respect to the central axis 12 of the mould so as to form a ring, and are able to be withdrawn radially with respect to the tyre during the opening of the mould.
[0031]
[0032]
[0033] The cutting means have a recessed and/or protruding shape. The recesses and the protrusions of the cutting means make it possible to lengthen the sliding path of the flash along the cutting means as they are withdrawn. By way of examples, the cutting means take the form of scissors, blades, spikes or any other suitable shape for cutting, tearing or forming an incipient crack in the flash.
[0034] Preferably, the cutting means are arranged on the edge 36 of each of said moulding elements 24, the cutting means of each of said moulding elements having complementary shapes. Thus, the effectiveness of the cutting off of the flash by the cutting means is improved. The cutting means 38 are integral with the edge 36 of at least one of said moulding elements 24. By way of example, the cutting means may also be fixed to the edges 36 of the moulding elements 24 by any other suitable means.
[0035] Said space 26 has a length L of between 0.2 and 20 mm and, more preferably, between 0.5 and 5 mm. The length of said space denotes, in a circumferential plane, the longest distance along which the two moulding elements are edge-to-edge. Thus, it is particularly appropriate to provide a space 26 and cutting means 38 on the edges of moulding elements 24, the contact surface of which has a short extent and is, consequently, more fragile.
[0036] Said space has a thickness E of between 0.1 and 3 mm, more preferably between 0.2 and 2 mm, and even more preferably between 0.3 and 1 mm. The thickness of said space denotes, in a circumferential plane, the shortest distance separating the two moulding elements. It is necessary for the moulding elements to be sufficiently far apart to prevent any risk of impact therebetween and sufficiently close together to minimize the thickness of the flash and thus to make it easier to cut off.
[0037] According to a preferred embodiment, the mould comprises at least one sipe blade 40 that extends over two adjacent sectors 18 such that said sipe blade comprises a part in each of the two sectors. In other words, said sipe blade comprises two parts 40a, 40b, said moulding elements 24 taking the form of each part of the sipe blade and, optionally, of the sector 18 to which a sipe blade part is joined. It is particularly appropriate to provide a space 26 and cutting means 38 on the particularly fragile edges of a “sectored” sipe blade. The sipe blade has a thickness of between 0.2 and 20 mm and, more preferably, between 0.5 and 5 mm.
[0038] Preferably, the cutting means have the shape of a triangular or crenellated toothing. Such a shape is particularly easy to arrange on the edge 36 of a sipe blade 40.
[0039] The different moulding elements 24 and the cutting means 38 that are used in the composition of a mould 10 are made from alloys of steel, aluminium, polymer resin or some other rigid material suitable for such a use.
[0040] The different moulding elements 24 and the cutting means 38 are obtained using a process chosen from the following group of processes: casting, pressing, laser cutting lasering, electrical discharge machining or consolidation by selective melting.
[0041] “Selective consolidation by melting” is understood to be an additive manufacturing process intended to aggregate or agglomerate a feed of incoming work material progressively and selectively so as to obtain an outgoing work material. The incoming work material takes the form of and/or is used in the composition of a powder, of a wire or of a solution/bath. The incoming work material is generally introduced by depositing a powder on a support such as to form a layer. The support takes the form of a plate or a previously agglomerated layer. The agglomeration is generally achieved by solidification of the incoming work material, which is melted completely or partially (sintering) by localized or generalized input of energy, and then cooled. The input of energy is generally realized by a laser or an electron beam, although it can be realized by infrared radiation or induction. In the case of the laser and the electron beam, the localization of the input of energy is achieved by means for orienting the input of energy, such as optical or electromagnetic means, respectively. The process provides the incoming work material with a shape and mechanical characteristics that are predetermined. Said shape and said characteristics depend on the material of the incoming work material and on parameters of the process. Said shape is generally a one-piece solid, although it can be made up of a plurality of one-piece solids.
[0042] Further variants and embodiments of the invention may be envisaged without departing from the scope of these claims.