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US5509455A Expired / Lapsed US ⏱️ 0.0 years remaining

Aircraft tire including reinforcement inserts

Assignee: Goodyear Tire and Rubber Co
•
Filing: 1994-04-12
•
Granted: 1996-04-23
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Expires: 2014-04-12
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Abstract

Abstract An aircraft tire 10 has at least two circumferentially extending reinforcement inserts. At least one pair of reinforcement inserts 90 is located on each side of the tire. Each insert 90 preferably has two cord reinforced members 91, 92 having bias angled cords. The cords are equal but opposite in orientation relative to the cords of the adjacent member. The pairs of reinforced members 91, 92 extend from the bead portions 18, 20 and terminate in a radially upper portion of the sidewalls 14A, 16A. In the preferred embodiment, each bead portion 18, 20 includes three substantially inextensible bead cores 50, 52 and 54. Each pair of members 91, 92 is interposed between a pair of carcass plies 36, 37, 38, 39, 40, 41, 42, 43 on the ply side of the tire 10. This structure can increase tire durability while at the same time achieve a significant weight reduction.

Inventors

  • 👤 John T. Warchol
  • 👤 Raymond W. Millmier
  • 👤 Gordon B. Bryant

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-04 17:05
CPC Classifications
B; B60; B60C; B60C15/00; B60C15/04; B60C15/05; B60C15/0009; B60C15/0081; B60C15/06; B60C9/00; B60C9/02; B60C9/04; B60C9/08; B60C9/09; B60C9/18; B60C2009/1878; Y; Y10; Y10T; Y10T152/00; Y10T152/10; Y10T152/10495; Y10T152/10513; Y10T152/10855; Y10T152/10864

Claims Analysis

Total Claims: 19
Claim 1
Independent Claim 132 words
An aircraft tire having a tread pattern, a pair of sidewall portions, a pair of spaced apart bead portions having at least one substantially inextensible bead core disposed side by side and spaced apart axially, and a plurality of carcass plies extending circumferentially about the tire from bead portion to bead portion, each ply having a ply side extending between the bead cores of opposite bead portions, the improvement comprising: at least two circumferentially extending reinforcement inserts, at least one reinforcement insert on each side of the tire, the reinforcement inserts extending from the bead portions and terminating in a radially upper portion of the sidewalls, each reinforcement insert having a pair of axially adjacent cord reinforced members, each insert being interposed between a pair of carcass plies on the ply side.
Claim 2
Dependent Claim 132 words
An aircraft tire having a tread pattern, a pair of sidewall portions, a pair of spaced apart bead portions having at least one substantially inextensible bead core disposed side by side and spaced apart axially, and a plurality of carcass plies extending circumferentially about the tire from bead portion to bead portion, each ply having a ply side extending between the bead cores of opposite bead portions, the improvement comprising: at least two circumferentially extending reinforcement inserts, at least one reinforcement insert on each side of the tire, the reinforcement inserts extending from the bead portions and terminating in a radially upper portion of the sidewalls, each reinforcement insert having a pair of axially adjacent cord reinforced members, each insert being interposed between a pair of carcass plies on the ply side.
Claim 3
Dependent Claim 33 words
The aircraft tire of claim 1, wherein the cord reinforced members have bias angled cords, the cords being equal but opposite in orientation relative to the cords of the adjacent cord reinforced member.
Claim 4
Dependent Claim 30 words
The aircraft tire of claim 1 wherein the cords of the carcass plies and the cords of the reinforced members are of a textile material having the same percent elongation.
Claim 5
Dependent Claim 21 words
The aircraft tire of claim 3, wherein the cords of the plies and the cords of the reinforced members are nylon.
Claim 6
Dependent Claim 21 words
The aircraft tire of claim 1 wherein the pair of axially adjacent cord reinforced members of each insert are radial plies.
Claim 7
Dependent Claim 16 words
The aircraft tire of claim 5 wherein the cords of the reinforced members are nylon cords.
Claim 8
Dependent Claim 14 words
The aircraft tire of claim 1 wherein the carcass plies have radially extending cords.
Claim 9
Dependent Claim 25 words
The aircraft tire of claim 1 wherein the carcass plies have bias angled cords and are wrapped about at least two substantially inextensible bead cores.
Claim 10
Dependent Claim 14 words
The aircraft tire of claim 1 wherein the tire has two inserts per side.
Claim 11
Dependent Claim 14 words
The aircraft tire of claim 1 wherein the tire has three inserts per side.
Claim 12
Dependent Claim 14 words
The aircraft tire of claim 1 wherein the tire has four inserts per side.
Claim 13
Dependent Claim 150 words
An aircraft tire having a tread pattern, a pair of sidewall portions, a pair of spaced apart bead portions having at least two substantially inextensible bead cores disposed side by side and spaced apart axially, and a plurality of carcass plies extending circumferentially about the tire from bead portion to bead portion, each ply having a ply side extending between the bead cores of opposite bead portions, the improvement comprising: at least two circumferentially extending pairs of cord reinforced members, at least one pair on each side of the fire, each member having bias angled cords, the cords being equal but opposite in orientation relative to the cords of the adjacent member, the pairs of cord reinforced members extending from the bead portions and terminating in a radially upper portion of the sidewalls, each pair of reinforced members being interposed between a pair of carcass plies on the ply side.
Claim 14
Dependent Claim 150 words
An aircraft tire having a tread pattern, a pair of sidewall portions, a pair of spaced apart bead portions having at least two substantially inextensible bead cores disposed side by side and spaced apart axially, and a plurality of carcass plies extending circumferentially about the tire from bead portion to bead portion, each ply having a ply side extending between the bead cores of opposite bead portions, the improvement comprising: at least two circumferentially extending pairs of cord reinforced members, at least one pair on each side of the fire, each member having bias angled cords, the cords being equal but opposite in orientation relative to the cords of the adjacent member, the pairs of cord reinforced members extending from the bead portions and terminating in a radially upper portion of the sidewalls, each pair of reinforced members being interposed between a pair of carcass plies on the ply side.
Claim 15
Dependent Claim 20 words
The improved tire of claim 12, wherein the plies and the reinforced members have cords of the same textile material.
Claim 16
Dependent Claim 21 words
The aircraft tire of claim 12 wherein the cords of the plies and the cords of the reinforced members are nylon.
Claim 17
Dependent Claim 19 words
The aircraft tire of claim 12 wherein the tire has two pairs of cord reinforced members per tire side.
Claim 18
Dependent Claim 18 words
The tire of claim 12 wherein the tire has three pairs of cord reinforced members per tire side.
Claim 19
Dependent Claim 18 words
The tire of claim 12 wherein the tire has four pairs of cord reinforced members per tire side.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1999-04-23 1999-10-23 2000-04-23 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2003-04-23 2003-10-23 2004-04-23 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2007-04-23 2007-10-23 2008-04-23 $7700.00 Window Closed / Lapsed

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