Patent US4947915A successfully refreshed from Google Patents.
US4947915A
Expired / Lapsed
US
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Radial ply tire
Assignee: Dunlop Ltd
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Filing: 1988-03-07
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Granted: 1990-08-14
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Expires: 2008-03-07
Abstract
Abstract A high speed radial ply tire, such as an aircraft tire, having a tread reinforcement comprising three groups of layers. The first, radially inner, group comprises two bias ply layers; the second group, wider than the first, being substantially parallel to the tire mid-circumferential plane and the third, radially outer group, narrower than the first, also being substantially parallel to the mid-circumferential plane of the tire. A fourth group of bias cut layers may be positioned between the second and third groups.
Inventors
- 👤 Tharamel P. K. Panikkar
- 👤 Stephen Barlow
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 05:22
CPC Classifications
B; B60; B60C; B60C9/00; B60C9/18; B60C9/20; B60C9/2003; B60C9/2009; B60C2200/00; B60C2200/02; Y; Y10; Y10T; Y10T152/00; Y10T152/10; Y10T152/10495; Y10T152/10765; Y10T152/10792
Claims Analysis
Total Claims: 15
Claim 1
Independent Claim
215 words
A radial aircraft tire comprising a tread, a radial ply carcass anchored to at least one bead core in each bead region of the tire and a tread reinforcement comprising three groups of layers of cord reinforcing fabric; the first, radially inner, group comprising at least two layers of parallel cords extending at a bias angle lying in the range 15 degrees to 60 degrees relative to the mid-circumferential plane of the tire, each layer being at opposite bias to the adjacent layer, and the width of the first group of layers being less than the contact width of the tire tread under the scheduled load and inflation pressure of the tire; a second group of layers, positioned radially outwards of the first group, and comprising at least two layers of parallel cords extending substantially parallel to the mid-circumferential plane of the tire, and the width of the second group of layers being greater than the width of the first group of layers; and a third group of layers, positioned radially outwards of the second group, comprising at least two layers of parallel cords extending substantially parallel to the mid-circumferential plane of the tire and having a width lying within the range of 40% to 70% of the width of the second group of layers.
Claim 2
Dependent Claim
215 words
A radial aircraft tire comprising a tread, a radial ply carcass anchored to at least one bead core in each bead region of the tire and a tread reinforcement comprising three groups of layers of cord reinforcing fabric; the first, radially inner, group comprising at least two layers of parallel cords extending at a bias angle lying in the range 15 degrees to 60 degrees relative to the mid-circumferential plane of the tire, each layer being at opposite bias to the adjacent layer, and the width of the first group of layers being less than the contact width of the tire tread under the scheduled load and inflation pressure of the tire; a second group of layers, positioned radially outwards of the first group, and comprising at least two layers of parallel cords extending substantially parallel to the mid-circumferential plane of the tire, and the width of the second group of layers being greater than the width of the first group of layers; and a third group of layers, positioned radially outwards of the second group, comprising at least two layers of parallel cords extending substantially parallel to the mid-circumferential plane of the tire and having a width lying within the range of 40% to 70% of the width of the second group of layers.
Claim 3
Dependent Claim
27 words
A radial aircraft tire according to claim 1 in which the carcass comprises more than one ply having a bias angle in the range 75 degrees-85 degrees.
Claim 4
Dependent Claim
29 words
A radial aircraft tire according to claim 1 in which the bias angle of the carcass ply is 84 degrees and the aspect ratio of the tire is 67%.
Claim 5
Dependent Claim
26 words
A radial aircraft tire according to claim 1 in which the bias angle of the cords in the layers in the first group is 45 degrees.
Claim 6
Dependent Claim
36 words
A radial aircraft tire according to claim 1 in which the width of the first group is between 70% and 90% of the tread contact width of the tire under the scheduled load and inflation pressure.
Claim 7
Dependent Claim
26 words
A radial aircraft tire according to claim 1 in which the width of the second group is at least 1.03 times that of the first group.
Claim 8
Dependent Claim
33 words
A radial aircraft tire according to claim 1 in which the width of the second group is no greater than 1.20 times the tread contact width under the scheduled load and inflation pressure.
Claim 9
Dependent Claim
63 words
A radial aircraft tire according to claim 1 including a fourth group of plies comprising at least two layers of parallel cords crossing the mid-circumferential plane of the tire at an angle in the range 15 degrees to 60 degrees, each layer being at opposite bias to the adjacent layer in the group, and positioned between the second and third group of layers.
Claim 10
Dependent Claim
22 words
A radial aircraft tire according to claim 8 in which said angle of the fourth group of plies is about 45 degrees.
Claim 11
Dependent Claim
28 words
A radial aircraft tire according to claim 8 in which the width of the fourth group of layers is no greater than the width of the third group.
Claim 12
Dependent Claim
26 words
A radial aircraft tire according to claim 1 in which a group of layers comprises separate rubberized fabric plies each wrapped once around the carcass circumference.
Claim 13
Dependent Claim
31 words
A radial aircraft tire according to claim 1 in which a group of layers comprises one ply, or a small number of plies, wrapped more than once around the carcass circumference.
Claim 14
Dependent Claim
45 words
A radial aircraft tire according to claim 1 in which the cords of any one of the first, second and third group of layers comprises fibers chosen from the group consisting of aromatic polyamide, aliphatic polyamide and a mixture of aromatic and aliphatic polyamide fibers.
Claim 15
Dependent Claim
39 words
A radial aircraft tire according to claim 8 in which the cords of the fourth group of layers comprise fibers chosen from the group consisting of aromatic polyamide, aliphatic polyamide and a mixture of aromatic and aliphatic polyamide fibers.
References Cited (Backward Citations)
US3831656A
Cited
GB2132574A
Cited
US4454903A
Cited
DE3324522A1
Cited
GB2171067A
Cited
US4732199A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1993-08-13 | 1994-02-12 | 1994-08-14 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1997-08-13 | 1998-02-12 | 1998-08-14 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2001-08-13 | 2002-02-12 | 2002-08-14 | $7700.00 | Window Closed / Lapsed |