Mould Insert Comprising A High-Contrast Texture

20170157870 · 2017-06-08

    Inventors

    Cpc classification

    International classification

    Abstract

    Lining element intended to be inserted into a mould for moulding and vulcanizing a tire tread, the lining element comprising a body and inserts inserted into this body, at least some of the inserts comprising a pattern comprising a plurality of recessed or projecting elements, the pattern being formed as an integral part of the inserts.

    Claims

    1. A lining element adapted to be inserted into a mould for moulding and vulcanizing a tire tread, the lining element comprising a body and inserts inserted into this body, wherein at least some of the inserts comprise a pattern comprising a plurality of recessed or protruding elements, said pattern being formed as an integral part of the inserts.

    2. The lining element according to claim 1, wherein the pattern comprises an organized arrangement of a plurality of elements, all or some of these elements being the distribution of one and the same basic element.

    3. The lining element according to claim 1, wherein the insert is configured as a mould lining such as a bar, a sipe blade, or a plurality of bars and/or sipe blades.

    4. The lining element according to claim 1, wherein the depth of the recessed elements is less than or equal to 30% of the thickness of the insert or the height of the protrusions is less than or equal to 30% of the thickness of the insert.

    5. The lining element according to claim 1, wherein the depth of the patterns is less than or equal to 15% of the thickness of the insert or the height of the protrusions is less than or equal to 15% of the thickness of the insert.

    6. The lining element according to claim 1, wherein all or part of the pattern is formed by conical cavities distributed through the pattern with a density at least equal to one conical cavity per square millimetre (mm.sup.2), each conical cavity having a mean cross section comprised between 0.0005 mm.sup.2 and 1 mm.sup.2.

    7. The lining element according to claim 1, wherein all or part of the pattern is formed by substantially mutually parallel striations, the spacing of the striations in the pattern being at most equal to 0.5 mm, each striation having a mean width comprised between 0.02 mm and 0.5 mm.

    8. The lining element according to claim 1, wherein all or part of the pattern forms recessed forms of parallelepipeds of side length (C) comprised between 0.05 mm and 0.5 mm, of height (Hp) comprised between 0.05 mm and 0.5 mm, the distance between two adjacent parallelepipeds in the texture being comprised between 0.05 mm and 0.5 mm.

    9. The lining element according to claim 1, wherein the protruding elements form strands, said strands being distributed through the pattern with a density at least equal to one strand per square millimetre (mm.sup.2), each strand having a mean cross section S comprised between 0.0005 mm.sup.2 and 1 mm.sup.2.

    10. The lining element according to claim 1, wherein the protruding elements form mutually parallel strips, the spacing of the strips in the pattern being at most equal to 0.5 mm, each strip having a mean width comprised between 0.02 mm and 0.5 mm.

    11. The lining element according to claim 1, wherein the recessed or protruding elements have mutually variable shapes and distances between them.

    12. The lining element according to claim 1, also configured for moulding a tire sidewall region.

    13. The lining element according to claim 1, produced by laser sintering.

    14. A segmented mould for vulcanizing tires, comprising a plurality of lining elements according to claim 1.

    Description

    DESCRIPTION OF THE FIGURES

    [0034] All the embodiment details are given in the description which follows which is supplemented by FIGS. 1 to 8, given solely by way of non-limiting examples and in which:

    [0035] FIG. 1 is a perspective view of a first example of mould elements inserted on a support block of a mould according to the invention;

    [0036] FIG. 2a is a perspective view of one example of mould elements according to the invention before they are attached to a segment;

    [0037] FIG. 2b is a perspective view of another example of a mould element according to the invention before it is fixed to a segment, with three views in lateral section in order to illustrate examples of means for attaching the mould element onto a support;

    [0038] FIG. 3 shows a mould element comprising a pattern formed of striations recessed into the mould;

    [0039] FIG. 4 shows a mould element in which the striations of the pattern have a pyramid-like cross section;

    [0040] FIG. 5 depicts a pattern comprising a plurality of holes;

    [0041] FIG. 6 is an enlarged view of the pattern of FIG. 5;

    [0042] FIG. 7 shows a mould element comprising a pattern formed of strands protruding from the mould;

    [0043] FIG. 8 shows a mould element comprising a pattern formed of strips.

    DETAILED DESCRIPTION OF THE INVENTION

    [0044] A pattern on a mould means an organized arrangement of a plurality of elements (striations, holes, strands, strips), all or some of these elements being a repeat of one and the same basic element, the pattern present on the mould making it possible to obtain a particular texture on a tire.

    [0045] In the description which will follow, elements that are substantially identical or similar will be denoted by identical references.

    [0046] FIG. 1 illustrates a lining element 10 of a segmented mould (not depicted) for vulcanizing tires. This lining element 10 comprises a body 11 advantageously made of aluminium alloy and notably comprising a plurality of support surfaces 16 intended to accept a plurality of inserts 18. The body 11 moreover comprises a network of tire tread pattern elements 24. Included among the tread pattern elements 24 there are notably sipe blades 26 which are intended to form circumferential slits in the tread of the tire or circumferential bars 28 which are intended to form a longitudinal groove in the tread of the tire. The various bars 28 may be connected by axial sipe blades 29 to form the network of tread pattern elements 24.

    [0047] Each of the inserts 18 comprises a first 20 and a second 22 surface which are opposite surfaces, the first surface 20 being intended to be in contact with the support surface 16 of the lining element. The inserts are specifically designed to allow patterns 30 used to produce textures on the tires and which will be moulded with a mould provided with a plurality of bodies 11 to be incorporated into the body 11. For that, at least some of the inserts 18 comprise a pattern 30 which comprises a plurality of recessed or protruding elements, the said pattern being formed as an integral part of the inserts. In other words, each insert 18 including the patterns 30 is produced as a single piece.

    [0048] The thickness of each insert 18 is comprised between 0.25 and 10 millimetres or even more.

    [0049] As illustrated in FIGS. 1, 2A and 2B the inserts 18 may adopt various shapes according to the various alternative forms of embodiment. First of all, the inserts are advantageously produced in the form of inserts, as shown in FIG. 2B. These inserts are inserted on the support surfaces 16 of the body 11. The inserts may also adopt the form of axial sipe blades 29, as illustrated in FIG. 1 and in FIG. 2A. FIG. 1 finally illustrates another alternative form in which the inserts form portions of circumferential bars 28. These last two alternative forms make it possible to obtain sipe blades 29 and/or bars 28 that have patterns 30.

    [0050] In these various alternative forms of embodiment, these patterns would be difficult to achieve if they had to be formed directly on the body 11.

    [0051] In order to produce such an insert 18, the procedure advantageously involves selective laser sintering of a metallic powder. During manufacture of the insert, care is taken to ensure that the shape of the first surface 20 is the complement of the shape of the support surface 16 of the body 11 so that the insert 18 can engage correctly with the body.

    [0052] FIG. 2a illustrates a number of exemplary embodiments of inserts 18 provided with textures 30 in the regions that will be visible following attachment to a body 11.

    [0053] FIG. 2b shows an example of an insert 18 provided with a texture 30 with various examples of how to fix it to a support surface 16. The examples illustrated include a dovetail fastening, fixing using adhesive bonding or by screw-fastening. The dovetail corresponds to an anchorage when casting the aluminium alloy of the lining element.

    [0054] In the examples such as those of FIGS. 1, 2a and 2b, the extent of the textured regions, the profiles and the positionings of the textured regions vary according to the embodiment, the examples illustrated being provided only by way of nonlimiting illustration. Furthermore, the patterns may adopt striated shapes, as depicted for example in FIG. 3, which shows square-wave striations 19, or in FIG. 4, which shows pyramid-shaped striations 21.

    [0055] FIG. 5 illustrates the pattern according to a non-limiting first alternative form of the first embodiment. In this alternative form, the pattern is formed by a plurality of cavities 112. The cavities 112 here are in the shape of cones which extend into the depth of the mould and open onto the mould in the form of circular openings 111. The cavities 112 thus have a cross section which decreases into the depth of the mould. It will be noted that, in this alternative form, the openings 111 of the cavities 112 do not touch. The openings 111 are separated by intermediate regions 113. Furthermore, the openings 111 are evenly distributed across the mould so that the distance d between each opening of the pattern is roughly similar.

    [0056] FIG. 6 is an enlarged view of the pattern of FIG. 5. All or some of the cavities here have at least one wall 114 which, when viewed in section, makes an angle comprised between 10 and 60 with respect to a direction Z perpendicular to the pattern.

    [0057] FIG. 7 illustrates an embodiment in which the pattern 30 comprises a plurality of strands 106, the strands 106 being distributed through the pattern with a density at least equal to one strand per mm.sup.2, each strand having a mean cross section S comprised between 0.0005 mm.sup.2 and 1 mm.sup.2.

    [0058] It will be noted that the mean cross section of each strand corresponds to the mean of the cross sections S measured at regular intervals from the base of the strand. The strands 106 have a conical overall shape with a cross section decreasing along the height Hb of these strands.

    [0059] FIG. 8 illustrates one embodiment in which the pattern 30 comprises a plurality of mutually parallel strips 107, the spacing of the strips 107 in the pattern 30 being at most equal to 0.5 mm, each strip 107 having a mean width comprised between 0.02 mm and 0.5 mm. It will be noted that the mean width corresponds to the mean of the widths 1 measured at regular intervals along the height Hl of the strip, the height of each strip being comprised between 0.05 and 0.5 mm.

    [0060] In another alternative form of embodiment, the pattern comprises a combination of strands 106 and/or of strips 107.

    [0061] The invention is not restricted to the examples described and depicted and various modifications can be made thereto without departing from its scope. Thus, according to another nonlimiting alternative form of embodiment, the strips 107 of FIG. 8 may be discontinuous. They have a planar part between them. They may further have differences in cross section from one another. In addition, the strips may have curvatures or corners, notably along their length. They may furthermore be of variable length.

    [0062] Thus, according to another nonlimiting alternative form of embodiment, the cavities 112 may have a parallelepipedal cross section of side length C comprised between 0.05 mm and 0.5 mm, of height Hp comprised between 0.05 mm and 0.5 mm, the distance between two adjacent cavities in the texture being comprised between 0.05 mm and 0.5 mm. As an alternative, the cross section of the cavities may be circular, polygonal (for example hexagonal). With square or polygonal structures it is possible to organize the openings 111 more easily in relation to one another so as to limit the surface area of the intermediate regions 113 between these openings. With such shapes of opening it is possible more easily to achieve high levels of occupancy of the openings on the mould.

    [0063] In the event that the inserts are removable, in order to adapt a mould to manufacture a new type of tire all that is required is for the inserts borne by the support blocks corresponding to the old type of tire manufactured to be removed, and for the new inserts 18 to be inserted in the corresponding surfaces 16, advantageously in a single operation.

    [0064] In the event that the lining elements of a mould are manufactured as an aluminium casting, the inserts according to the invention are advantageously anchored during the casting in a plaster mould or a steel die. However, attachment by adhesive bonding or screw-fastening into a lining element made of aluminium or some other alloy may also be envisaged. In the former instance the inserts are not removable, whereas in the latter instance the inserts can be removed, either to allow them to be replaced or to allow them to be cleaned or the like.

    [0065] The invention has been described in conjunction with a mould intended to incorporate a plurality of lining elements like the one illustrated in the example of FIG. 1. It may also be implemented in relation to a mould of some other type.

    NUMERICAL REFERENCES USED IN THE FIGURES

    [0066] 10 Lining element

    [0067] 11 Body

    [0068] 16 Support surface

    [0069] 18 Insert

    [0070] 19 Square-wave striation

    [0071] 20 First surface

    [0072] 21 Pyramid-shaped striation

    [0073] 22 Second surface

    [0074] 24 Network of tire tread pattern elements

    [0075] 26 Sipe blades

    [0076] 28 Circumferential bars

    [0077] 29 Axial sipe blades

    [0078] 30 Patterns

    [0079] 106 Strands

    [0080] 107 Strips

    [0081] 111 Circular opening

    [0082] 112 Cavity

    [0083] 113 Intermediate region

    [0084] 114 Wall