Method of making tires for vehicle wheels
Abstract
At least one carcass ply ( 3 ) is formed by depositing a strip-like element ( 13 ) comprising longitudinal thread-like elements ( 13 a ) incorporated into a layer of elastomer material ( 13 b ), onto a toroidal support ( 11 ). Deposition of the strip-like element ( 13 ) takes place in alternated deposition sections ( 23, 24 ) each comprising two radially-extending side portions ( 23 a, 24 a, 23 c, 24 c ) and a crown portion ( 23 b, 24 b ) extending at a radially external position. The side portions of each deposition section ( 23, 24 ) are at least partly overlapped with side portions belonging to an adjacent deposition section. Associated with the carcass ply ( 3 ) are annular structures ( 4 ) comprising a circumferentially inextensible annular insert ( 32 ) axially external to an anchoring element ( 31 ). A belt structure ( 5 ), a tread band ( 8 ) and sidewalls ( 9 ) are combined with the thus formed carcass structure ( 2 ) to define a tire ( 1 ) to be submitted to a vulcanization step.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . A method of making a tire, comprising the steps of:
making a carcass structure ( 2 ); applying a belt structure ( 5 ) to the carcass structure ( 2 ) at a circumferentially external position thereof; applying a tread band ( 8 ) to the belt structure ( 5 ) at a circumferentially external position thereof; applying at least one pair of sidewalls ( 9 ) to the carcass structure ( 2 ) at laterally opposite positions; vulcanizing the obtained tire ( 1 ), wherein manufacturing of the carcass structure ( 2 ) involves formation of at least one carcass ply ( 3 ) by the following steps:
preparing at least one continuous strip-like element ( 13 ) comprising a plurality of longitudinal and parallel thread-like elements ( 13 a ) at least partly coated with at least one layer of raw elastomer material ( 13 b );
depositing the strip-like element ( 13 ) onto a toroidal support in alternated deposition sections ( 23 , 24 ) each extending in a substantially U-shaped conformation about the profile in transverse section of the toroidal support ( 11 ), to define two side portions ( 23 a , 23 c , 24 a , 24 c ) substantially extending in planes orthogonal to a geometric axis of rotation of the toroidal support ( 11 ) at mutually spaced apart positions in an axial direction, and a crown portion ( 23 b , 24 b ) extending in a radially external position between the side portions ( 23 a , 23 c , 24 a , 24 c );
the crown portions ( 23 b , 24 b ) of each deposition section ( 23 , 24 ) being disposed consecutively in side by side relationship along the circumferential extension of the toroidal support ( 11 ), whereas the side portions ( 23 a , 23 c , 24 a , 24 c ) of each deposition section ( 23 , 24 ) are each partly overlapped with a side portion of at least one consecutive deposition section.
2 . The method as claimed in claim 1 , wherein the side portions ( 23 a , 23 c , 24 a , 24 c ) in mutual-overlapping relationship are caused to mutually converge at the geometric axis of rotation of the toroidal support ( 11 ).
3 . The method as claimed in claim 1 , wherein mutual overlapping of the side portions ( 23 a , 23 c , 24 a , 24 c ) of the deposition sections ( 23 , 24 ) progressively decreases starting from a maximum value at the radially inner ends of the side portions until a zero value at transition regions between said side portions and crown portions ( 23 b , 24 b ).
4 . The method as claimed in claim 1 , wherein the side portions ( 23 a , 23 c , 24 a , 24 c ) in mutual-overlapping relationship are maintained joined to each other at a bending end region ( 25 ) where the strip-like element ( 13 ) is folded upon itself.
5 . The method as claimed in claim 1 , wherein the individual deposition sections ( 23 , 24 ) are sequentially laid down onto the toroidal support ( 11 ) according to a circumferential distribution pitch corresponding to the width of the strip-like element ( 13 ).
6 . The method as claimed in claim 1 , wherein the individual deposition sections ( 23 , 24 ) are sequentially laid down onto the toroidal support ( 11 ) according to a circumferential distribution pitch corresponding to a multiple of the width of the strip-like element ( 13 ).
7 . The method as claimed in claim 1 , wherein the strip-like element ( 13 ) has a width corresponding to a submultiple of the circumferential extension of the toroidal support ( 11 ), as measured at its equatorial plane.
8 . The method as claimed in claim 1 , wherein manufacturing of said at least one carcass ply ( 3 ) further involves a sequential pressing step of the strip-like element ( 13 ) at the side portions ( 23 a , 23 c , 24 a , 24 c ) of the deposition sections ( 23 , 24 ), to define regions of greater width close to the inner circumferential edges of the carcass structure ( 2 ).
9 . The method as claimed in claim 8 , wherein the pressing step is carried out on the strip-like element ( 13 ) during the deposition step, by exerting a pressing action of the strip-like element at a section thereof upstream of the toroidal support ( 11 ).
10 . The method as claimed in claim 8 , wherein concurrently with said pressing step, moving apart from each other of the thread-like elements ( 13 a ) comprised in the strip-like element ( 13 ) is carried out.
11 . The method as claimed in claim 1 , wherein during the deposition step, at least one deposition section comprising an initial or leading end of the strip-like element is retained on the toroidal support ( 11 ) by a suction action produced through the toroidal support itself.
12 . The method as claimed in claim 1 , wherein formation of each deposition section ( 23 , 24 ) involves the steps of:
guiding the strip-like element ( 13 ) on a distributor element ( 22 ) movable about the profile in transverse section of the toroidal support ( 11 ); translating the distributor element ( 22 ) substantially radially away from the geometric axis of rotation of the toroidal support ( 11 ) to form a first side portion ( 23 a , 24 a ) of the deposition section ( 23 , 24 ) of the strip-like element ( 13 ); rotating the toroidal support ( 11 ) relative to the distributor element ( 22 ) according to an angular pitch corresponding to half the distribution pitch of the deposition sections ( 23 , 24 ), concurrently with formation of said first side portion ( 23 a , 24 a ); translating the distributor element ( 11 ) substantially in a direction parallel to the geometric axis of rotation of the toroidal support ( 11 ) to form the crown portion ( 23 b , 24 b ) of the deposition section ( 23 , 24 ) of the strip-like element ( 13 ); translating the distributor element ( 22 ) substantially radially close to the geometric axis of rotation of the toroidal support ( 11 ) to form a second side portion ( 23 c , 24 c ) of the deposition section ( 23 , 24 ) of the strip-like element ( 13 ); rotating the toroidal support ( 11 ) relative to the distributor element ( 22 ) according to said angular pitch, concurrently with formation of said second side portion ( 23 c , 24 c ).
13 . The method as claimed in claim 12 , wherein during formation of the first side portion ( 23 a , 24 a ) of each deposition section ( 23 , 24 ) the step of retaining the strip-like element ( 13 ) at a bending region ( 25 ) defined between the first side portion and the second side portion ( 23 a , 24 a ) of the previously formed deposition section is carried out.
14 . The method as claimed in claim 13 , wherein retention of the strip-like element ( 13 ) is carried out by disposing a retaining element ( 26 ) alongside the second side portion ( 23 a , 24 a ) after translation of the distributor element ( 22 ) radially close to the geometric axis of rotation of the toroidal support ( 11 ), so that the strip-like element ( 13 ) is turned back about the retaining element ( 26 ) thereby forming the bending region ( 25 ) as a result of translation of the distributor element ( 22 ) radially away from the geometric axis of rotation of the toroidal support ( 11 ).
15 . The method as claimed in claim 14 , wherein the retaining element ( 26 ) is axially disengaged from the bending region ( 25 ), after starting of formation of the crown portion ( 23 b , 24 b ) of the deposition section ( 23 , 24 ) being made.
16 . The method as claimed in claim 1 , further comprising a step of pressing said side portions ( 23 a , 23 c , 24 a , 24 c ) of the deposition sections against side walls of the toroidal support ( 11 ).
17 . The method as claimed in claim 16 , wherein said pressing step is carried out repeatedly on a first and a second side portions ( 23 a , 24 c , 23 c , 24 a ) belonging to two contiguous deposition sections ( 23 , 24 ).
18 . The method as claimed in claim 1 , wherein accomplishment of the carcass structure ( 2 ) further comprises the step of applying at least one inextensible annular structure ( 4 ) to an area close to each of the inner circumferential edges of the carcass ply ( 3 ) obtained from the deposition step.
19 . The method as claimed in claim 18 , wherein accomplishment of the carcass structure ( 2 ) further comprises the step of turning back end flaps of the side portions ( 23 a , 23 c , 24 a , 24 c ) about the respective inextensible annular structures ( 4 ).
20 . The method as claimed in claim 1 , wherein accomplishment of the carcass structure ( 2 ) further comprises the step of forming a second carcass ply in the same manner as formation of the first carcass ply ( 3 ).
21 . A method of making a tire, comprising the steps of:
making a carcass structure ( 2 ); applying a belt structure ( 5 ) to the carcass structure ( 2 ) at a circumferentially external position thereof; applying a tread band ( 8 ) to the belt structure ( 5 ) at a circumferentially external position thereof; applying at least one pair of sidewalls ( 9 ) to the carcass structure ( 2 ) at laterally opposite positions; vulcanizing the obtained tire ( 1 ), wherein accomplishment of each inextensible annular structure ( 4 ) comprises the steps of:
depositing at least one thread-like element in concentric coils ( 32 a ) into a molding cavity ( 34 ) to form a circumferentially inextensible annular insert to be positioned substantially parallelly to adjacent surfaces of the carcass ply ( 3 );
positioning an annular anchoring element ( 31 ) into the molding cavity ( 34 ), at a position axially close to the circumferentially inextensible annular insert ( 32 );
injecting raw elastomeric material into the molding cavity ( 34 ) to make a filling body ( 33 ) intimately joined to the annular anchoring element ( 31 ) and the circumferentially inextensible annular insert ( 32 ).
22 . The method as claimed in claim 21 , wherein said deposition step is preceded by a rubberizing step in which said thread-like element is coated with at least one layer of raw elastomer material.
23 . The method as claimed in claim 21 , further comprising the step of magnetically retaining the circumferentially inextensible annular insert ( 32 ), at a predetermined position, within the molding cavity ( 34 ).
24 . The method as claimed in claim 21 , wherein injection of the raw elastomer material is carried out through at least one circumferential admission hollow space ( 35 ) opening into the molding cavity ( 34 ).
25 . A method of making a tire, comprising the steps of:
making a carcass structure ( 2 ); applying a belt structure ( 5 ) to the carcass structure ( 2 ) at a circumferentially external position thereof; applying a tread band ( 8 ) to the belt structure ( 5 ) at a circumferentially external position thereof; applying at least one pair of sidewalls ( 9 ) to the carcass structure ( 2 ) at laterally opposite positions; vulcanizing the obtained tire ( 1 ), wherein application of the belt structure ( 5 ) comprises the steps of:
forming at least one continuous belt ribbon ( 36 ) comprising at least one layer of raw elastomer material ( 36 b ) at least partly incorporating a plurality of longitudinal parallel cords ( 36 a );
cutting said continuous belt ribbon ( 36 ) according to a predetermined inclination relative to its longitudinal extension to form belt lengths ( 42 ) having a predetermined size in width, measured perpendicularly to the cutting direction;
laying down the belt lengths ( 41 ) consecutively in circumferential alignment onto the carcass structure ( 2 ) to form at least one first continuous belt strip ( 6 ) having said cords ( 36 a ) disposed transversely according to an inclination corresponding to the cutting inclination of said lengths ( 42 ).
26 . The method as claimed in claim 25 , wherein before said cutting step, the continuous belt ribbon ( 36 ) is submitted to a calendering step to give said lengths a circumferential size corresponding to a submultiple of the circumferential extension of the belt strip ( 6 ).
27 . The method as claimed in claim 25 , wherein application of the belt structure ( 5 ) further comprises the step of forming at least one second belt strip ( 7 ) by winding of at least one continuous thread-like element ( 44 ) in coils disposed axially in side by side relationship and extending circumferentially about the first belt strip ( 6 ).
28 . The method as claimed in claim 27 , wherein the winding coils formed by the elongated element ( 44 ) are disposed mutually in side by side relationship according to a variable axial-distribution pitch.
29 . The method as claimed in claim 28 , wherein said axial-distribution pitch is greater close to the equatorial median plane (X-X) of the tire ( 1 ) relative to the opposite side edges of the belt structure ( 5 ).
30 . The method as claimed in claim 1 , wherein application of the tread band ( 8 ) comprises the step of circumferentially winding at least one continuous sheet of raw elastomer material ( 49 ) about the belt structure ( 5 ) in a plurality of radially superposed coils (S).
31 . The method as claimed in claim 30 , wherein the continuous sheet of elastomer material ( 49 ) is produced directly during its application to the belt structure ( 5 ).
32 . The method as claimed in claim 30 , further comprising the step of progressively reducing the width of the elastomer material sheet ( 49 ), concurrently with formation of each winding coil (S) about the belt structure ( 5 ).
33 . The method as claimed in claim 1 , wherein each of said sidewalls ( 9 ) is made by injection of elastomer material into a mold ( 53 ).
34 . The method as claimed in claim 33 , wherein accomplishment of each of said sidewalls ( 9 ) comprises the following steps:
injecting a first elastomer material into a first cavity defined in said mold ( 53 ) to form a radially outer portion ( 9 a ) of the sidewall ( 9 ); defining a-second cavity in the mold ( 53 ), which is partly delimited by the radially outer portion ( 9 a ) of the sidewall ( 9 ); injecting a second elastomer material into the second cavity of the mold ( 53 ) to define a radially inner portion ( 9 b ) of the sidewall ( 9 ).
35 . The method as claimed in claim 1 , wherein formation of the carcass ply ( 3 ) is preceded by a step of coating the toroidal support ( 11 ) with at least one air-proof layer or liner ( 10 ) of elastomer material.
36 . The method as claimed in claim 35 , wherein said coating step is carried out by winding at least one ribbon-like band ( 12 ) of an air-proof elastomer material in coils disposed in side-by-side relationship along the profile in transverse section of the toroidal support ( 11 ).
37 . The method as claimed in claim 1 , wherein before the vulcanization step the following steps are carried out:
disengaging the tire ( 1 ) from the toroidal support ( 11 ); inserting an air tube into the carcass structure ( 2 ).
38 . The method as claimed in claim 1 , wherein during said vulcanization step, a step of stretching said carcass plies ( 3 ) and belt strips ( 6 , 7 ) is carried out for achieving an expansion of the tire of a linear amount included between 2% and 5%.Join the waitlist — get patent alerts
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