US4418735A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Tire, particularly for airplanes, having a crown reinforcement with extensible edges and method of manufacturing same
Assignee: Compagnie Generale des Etablissements Michelin SCA
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Filing: 1982-02-05
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Granted: 1983-12-06
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Expires: 2002-02-05
Abstract
Abstract The tripartite crown reinforcement of this tire is subdivided into a median portion composed of two plies of cables whose extensibility is practically zero, flanked by two lateral portions each composed of three plies of cables whose extensibility is very great. When this tire is not inflated, the edges of its tread resume the falling shape which has been imparted to them in the vulcanization mold.
Inventors
- 👤 Jacques Musy
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 10:43
CPC Classifications
B; B29; B29D; B29D30/00; B60; B60C; B60C3/00; B60C3/04; B60C9/00; B60C9/0057; B60C9/18; B60C9/20; B60C9/2003; B60C9/2009; B60C2200/00; B60C2200/02; Y; Y10; Y10T; Y10T152/00; Y10T152/10; Y10T152/10135; Y10T152/10171; Y10T152/1018; Y10T152/10189; Y10T152/10207
Claims Analysis
Total Claims: 20
Claim 1
Independent Claim
280 words
A tire for airplanes having a carcass reinforcement formed of at least one ply of radial cables which is anchored to at least one bead ring in each bead and a tripartite crown reinforcement composed of a median portion and two lateral portions, each of the edtes of the median portion being in contact with a lateral portion, each of these three portions being formed of at least one ply of textile cables forming an angle of between 0° and 30° with the circumferential direction of the tire, the relative camber of convexity of the carcass reinforcement in the crown being at most 0.12, preferably between 0.04 and 0.10, and the relative camber of convexity of the carcass reinforcement in the sidewalls being at most 0.14 when the tire is mounted on its service rim and inflated to its service pressure but not under load, the tire thus having a quasi-rectangular meridian profile, this tire being characterized by the fact that when it is mounted on its service rim but not inflated, its carcass reinforcement has a relative camber of convexity in the crown of at most 0.20, preferably between 0.08 and 0.15, and a relative camber of convexity in the sidewalls of at most 0.25 and a length such that after inflation of the tire to its service pressure its equilibrium curve at the level of the shoulders is located radially outwards of its curve in the uninflated tire, and by the fact that the median portion of the crown reinforcement is formed of cables whose extensibility is low, preferably close to zero, while the lateral portions of the crown reinforcement are formed of cables of very great extensibility.
Claim 2
Dependent Claim
280 words
A tire for airplanes having a carcass reinforcement formed of at least one ply of radial cables which is anchored to at least one bead ring in each bead and a tripartite crown reinforcement composed of a median portion and two lateral portions, each of the edtes of the median portion being in contact with a lateral portion, each of these three portions being formed of at least one ply of textile cables forming an angle of between 0° and 30° with the circumferential direction of the tire, the relative camber of convexity of the carcass reinforcement in the crown being at most 0.12, preferably between 0.04 and 0.10, and the relative camber of convexity of the carcass reinforcement in the sidewalls being at most 0.14 when the tire is mounted on its service rim and inflated to its service pressure but not under load, the tire thus having a quasi-rectangular meridian profile, this tire being characterized by the fact that when it is mounted on its service rim but not inflated, its carcass reinforcement has a relative camber of convexity in the crown of at most 0.20, preferably between 0.08 and 0.15, and a relative camber of convexity in the sidewalls of at most 0.25 and a length such that after inflation of the tire to its service pressure its equilibrium curve at the level of the shoulders is located radially outwards of its curve in the uninflated tire, and by the fact that the median portion of the crown reinforcement is formed of cables whose extensibility is low, preferably close to zero, while the lateral portions of the crown reinforcement are formed of cables of very great extensibility.
Claim 3
Dependent Claim
85 words
A tire according to claim 1, characterized by the fact that when the tire is mounted on its service rim but not inflated, the convexity of the tread is greater by at least 1.5%, preferably 3% to 4%, of the equatorial radius ofthe tire inflated to its service pressure than said convexity measured on the tire when inflated to its service pressure, said convexity measured on the tire inflated to its service pressure being between 0% and 6% of the equatorial radius of the tire.
Claim 4
Dependent Claim
48 words
A tire according to claim 1 or 2, characterized by the fact that the median portion of the crown reinforcement is formed of at least one ply of cables whose relative elongation is less than 3%, preferably between 0.1% and 1.5%, measured at 25% of the rupture force.
Claim 5
Dependent Claim
37 words
A tire according to claim 1 or 2, characterized by the fact that the median portion of the crown reinforcement is formed of cables oriented at about 0° with respect to the circumferential direction of the tire.
Claim 6
Dependent Claim
34 words
A tire according to claim 1 or 2, characterized by the fact that the median portion of the crown reinforcement has an axial width less than 80% of the width of the crown reinforcement.
Claim 7
Dependent Claim
45 words
A tire according to claim 1 or 2, characterized by the fact that the median portion of the crown reinforcement is formed of plies of cables which are crossed symmetrically at angles of less than 30° with respect to the circumferential direction of the tire.
Claim 8
Dependent Claim
36 words
A tire according to claim 1 or 2, characterized by the fact that in the lateral portions of the crown reinforcement the cables have a relative elongation of between 10% and 30% at the rupture force.
Claim 9
Dependent Claim
37 words
A tire according to claim 1 or 2, characterized by the fact that in the lateral portions of the crown reinforcement the cables are oriented at about 0° with respect to the circumferential direction of the tire.
Claim 10
Dependent Claim
36 words
A tire according to claim 1 or 2, characterized by the fact that each lateral portion of the crown reinforcement has an axial width of between 10% and 35% of the width of the crown reinforcement.
Claim 11
Dependent Claim
45 words
A tire according to claim 1 or 2, characterized by the fact that the lateral portions of the crown reinforcement are formed of plies of cables which are crossed symmetrically at angles of less than 25° with respect to the circumferential direction of the tire.
Claim 12
Dependent Claim
59 words
A tire according to claim 1 or 2, characterized by the fact that the crown reinforcement has at least one lateral ply arranged radially outwards of at least one median ply in the zone of contact between the lateral and median portions so as to create a zone common to the median portion and each of the lateral portions.
Claim 13
Dependent Claim
42 words
A tire according to claim 11, characterized by the fact that the common zone between each lateral portion and the median portion of the crown reinforcement has an axial width at most equal to 15% of the width of the crown reinforcement.
Claim 14
Dependent Claim
39 words
A tire according to claim 1 or 2, characterized by the fact that the radial carcass reinforcement has a relative elongation under the effect of the service pressure of between 1% and 2% of its length in the mold.
Claim 15
Dependent Claim
26 words
A tire according to claim 1, characterized by the fact that it further comprises customary crown plies which are arranged radially outwards of the crown reinforcement.
Claim 16
Dependent Claim
31 words
A tire according to claim 14, characterized by the fact that the customary crown plies have a width approximately equal to the width of the median portion of the crown reinforcement.
Claim 17
Dependent Claim
39 words
A tire according to claim 14 or 15, characterized by the fact that the customary crown plies are of elastic steel cables arranged at angles at least equal to 45° with respect to the circumferential direction of the tire.
Claim 18
Dependent Claim
88 words
A tire according to claim 1, characterized by the fact that radially outwards of the crown reinforcement there is arranged at least one ply of parallel cables undulated in the plane of the ply, the distance between the cables being between 50% and 100% of the crest-to-crest amplitude of the undulations, the wavelength thereof being between 100% and 200% of the amplitude, and the mean axes of the undulations of these cables being oriented preferably at 0° or 90° with respect to the circumferential direction of the tire.
Claim 19
Independent Claim
273 words
A method for manufacturing a tire for airplanes having a carcass reinforcement formed of at least one ply of radial cables which is anchored to at least one bead ring in each bead and a tripartite crown reinforcement composed of a median portion and two lateral portions, each of the edges of the median portion being in contact with a lateral portion, each of these three portions being formed of at least one ply of textile cables forming an angle of between 0° and 30° with the circumferential direction of the tire, characterized by the use of a vulcanization mold in which the carcass reinforcement of the tire has a relative camber of convexity in the crown of at most 0.20, preferably between 0.08 and 0.15, and a relative camber of convexity in the sidewalls of at most 0.25, and a length such that after inflation of the tire to its service pressure, its equilibrium curve at the level of the shoulders is located radially outwards of its curve in the vulcanization mold; and characterized by the use of a crown reinforcement whose median portion is formed of cables of low extensibility, preferably close to zero, while the lateral portions of the crown reinforcement are formed of cables of very great extensibility; when the tire is mounted on its service rim and inflated to its service pressure but not under load, its carcass reinforcement has a relative camber of convexity in the crown of at most 0.12, preferably between 0.04 and 0.10, and a relative camber of convexity in the sidewalls of at most 0.14, the tire thus having a quasi-rectangular meridian profile.
Claim 20
Independent Claim
273 words
A method for manufacturing a tire for airplanes having a carcass reinforcement formed of at least one ply of radial cables which is anchored to at least one bead ring in each bead and a tripartite crown reinforcement composed of a median portion and two lateral portions, each of the edges of the median portion being in contact with a lateral portion, each of these three portions being formed of at least one ply of textile cables forming an angle of between 0° and 30° with the circumferential direction of the tire, characterized by the use of a vulcanization mold in which the carcass reinforcement of the tire has a relative camber of convexity in the crown of at most 0.20, preferably between 0.08 and 0.15, and a relative camber of convexity in the sidewalls of at most 0.25, and a length such that after inflation of the tire to its service pressure, its equilibrium curve at the level of the shoulders is located radially outwards of its curve in the vulcanization mold; and characterized by the use of a crown reinforcement whose median portion is formed of cables of low extensibility, preferably close to zero, while the lateral portions of the crown reinforcement are formed of cables of very great extensibility; when the tire is mounted on its service rim and inflated to its service pressure but not under load, its carcass reinforcement has a relative camber of convexity in the crown of at most 0.12, preferably between 0.04 and 0.10, and a relative camber of convexity in the sidewalls of at most 0.14, the tire thus having a quasi-rectangular meridian profile.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1986-12-05 | 1987-06-06 | 1987-12-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1990-12-05 | 1991-06-06 | 1991-12-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1994-12-05 | 1995-06-06 | 1995-12-06 | $7700.00 | Window Closed / Lapsed |