# US 2021/0078366 A1 · Aircraft tire

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- Number: US 2021/0078366 A1
- Document ID: US20210078366A1
- Status: Published application
- Kind: A1
- Application number: 16/772,640
- Filed: 2018-11-21
- Published: 2021-03-18
- Earliest claimed: 2017-12-13
- Assignees: Bridgestone Corporation
- Applicants: Bridgestone Corporation
- Inventors: Kiichiro SUZUMORI
- Web page: https://patentgrep.com/patent/US20210078366A1

## CPC

- B60C 9/08: the cords extend transversely from bead to bead, i.e. radial ply (B60C9/07 takes precedence)
- B60C 15/0018: {not folded around the bead core, e.g. floating or down ply}
- B60C 15/0027: {with low ply turn-up, i.e. folded around the bead core and terminating at the bead core}
- B60C 15/0628: {comprising a bead reinforcing layer}
- D02G 3/48: Tyre cords {(tyre reinforcements B60C9/00; metal cords for reinforcing rubber or plastic articles D07B1/0606)}
- B60C 2015/0639: {between carcass main portion and bead filler not wrapped around the bead core}
- B60C 2015/0642: {between carcass turn-up and bead filler not wrapped around the bead core}
- B60C 2015/065: {at the axially outer side of the carcass turn-up portion not wrapped around the bead core}
- B60C 2015/0685: {Physical properties or dimensions of the cords, e.g. modulus of the cords}
- B60C 2015/0692: {characterised by particular materials of the cords}
- B60C 2200/02: for aircrafts
- B60C: VEHICLE TYRES; TYRE INFLATION; TYRE CHANGING; CONNECTING VALVES TO INFLATABLE ELASTIC BODIES IN GENERAL; DEVICES OR ARRANGEMENTS RELATED TO TYRES
- D02G: CRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS

## Abstract

Provided is an aircraft tire which has both satisfactory light weight and satisfactory separation durability of carcass ply ends. An aircraft tire (10) includes a pair of bead cores (1), and a carcass (2) extending between the pair of the bead cores (1). In this aircraft tire (10), the carcass (2) includes at least one layer of a turn-up ply (2a) which is composed of a main body (2aa) and folded portions (2ab), and at least one layer of a down ply (2b) which covers a tire width-direction outer side of the respective folded portions (2ab) of the turn-up ply (2a) and extends to at least a tire radial-direction inner side of the respective bead cores (1); rubber-cord reinforcing members (6) are each arranged between the main body (2aa) of an outermost turn-up ply (2a) and the folded portion (2ab) of the turn-up ply (2a) extending to a tire radial-direction outermost side, and between the folded portion (2ab) of the turn-up ply (2a) extending to the tire radial-direction outermost side and an innermost down ply (2b); and cords of the rubber-cord reinforcing members (6) have an elongation at break of not less than 30%.

## Claims

### Claim 1

An aircraft tire comprising:
a pair of bead cores; and
a carcass extending between the pair of the bead cores,
wherein
the carcass comprises: at least one layer of a turn-up ply, which is composed of a main body extending between the bead cores, and folded portions that are folded and extend around the respective bead cores from a tire width-direction inner side to an outer side; and at least one layer of a down ply, which covers a tire width-direction outer side of the respective folded portions of the turn-up ply and extends to at least a tire radial-direction inner side of the respective bead cores,
rubber-cord reinforcing members are each arranged between the main body of a tire width-direction outermost turn-up ply and the folded portion of a turn-up ply extending to a tire radial-direction outermost side, and between the folded portion of the turn-up ply extending to the tire radial-direction outermost side and a tire width-direction innermost down ply, and
cords of the rubber-cord reinforcing members have an elongation at break of not less than 30%.

### Claim 2 (depends on 1)

The aircraft tire according to claim 1, wherein the cords of the rubber-cord reinforcing members have a total fineness of 100 to 1,000 dtex.

### Claim 3 (depends on 1)

The aircraft tire according to claim 1, wherein the cords of the rubber-cord reinforcing members have an elongation at break of 30% to 45%.

### Claim 4 (depends on 1)

The aircraft tire according to claim 1, wherein the cords of the rubber-cord reinforcing members have a final twist coefficient of 0.25 to 0.60.

### Claim 5 (depends on 1)

The aircraft tire according to claim 1, wherein the cords of the rubber-cord reinforcing members are made of nylon.

### Claim 6 (depends on 2)

The aircraft tire according to claim 2, wherein the cords of the rubber-cord reinforcing members have an elongation at break of 30% to 45%.

### Claim 7 (depends on 2)

The aircraft tire according to claim 2, wherein the cords of the rubber-cord reinforcing members have a final twist coefficient of 0.25 to 0.60.

### Claim 8 (depends on 2)

The aircraft tire according to claim 2, wherein the cords of the rubber-cord reinforcing members are made of nylon.

### Claim 9 (depends on 3)

The aircraft tire according to claim 3, wherein the cords of the rubber-cord reinforcing members have a final twist coefficient of 0.25 to 0.60.

### Claim 10 (depends on 3)

The aircraft tire according to claim 3, wherein the cords of the rubber-cord reinforcing members are made of nylon.

### Claim 11 (depends on 4)

The aircraft tire according to claim 4, wherein the cords of the rubber-cord reinforcing members are made of nylon.

### Claim 12 (depends on 6)

The aircraft tire according to claim 6, wherein the cords of the rubber-cord reinforcing members have a final twist coefficient of 0.25 to 0.60.

### Claim 13 (depends on 6)

The aircraft tire according to claim 6, wherein the cords of the rubber-cord reinforcing members are made of nylon.

### Claim 14 (depends on 7)

The aircraft tire according to claim 7, wherein the cords of the rubber-cord reinforcing members are made of nylon.

### Claim 15 (depends on 9)

The aircraft tire according to claim 9, wherein the cords of the rubber-cord reinforcing members are made of nylon.

### Claim 16 (depends on 12)

The aircraft tire according to claim 12, wherein the cords of the rubber-cord reinforcing members are made of nylon.
