Protective crown reinforcement for aeroplane tire

Patent metadata

Field	Value
Publication number	US-10814673-B2
Application number	US-201515534384-A
Country	US
Kind code	B2
Filing date	Dec 2, 2015
Priority date	Dec 8, 2014
Publication date	Oct 27, 2020
Grant date	Oct 27, 2020

Abstract

Protective reinforcement (3) for a tire has a mean radial thickness T at least equal to two times the diameter D of a-12-einforce (4), comprises respectively on its radially interior face (31) and on its radially exterior face (32) parts (7) made of elastomeric compound having an axial width W at least equal to the diameter D of a-12-reinforcer (4), and the path of any-12-reinforce (4), in the circumferential direction (XX′), varies radially between the radially interior first face (31) and the radially exterior second face (32), in such a way that the set of paths of the reinforcers (4) of the protective reinforcement (3) constitutes a three-dimensional lattice. Furthermore, the path of any-12-reinforce (4), in the circumferential direction (XX′), is a zigzag curve extending axially over the entire axial width L of the protective reinforcement (3).

First claim

The invention claimed is:

1. Aircraft tire comprising:
a tread, configured to come into contact with a ground;
a protective reinforcement, radially on an inside of the tread;
the protective reinforcement having a cylindrical structure having as its axis of revolution an axis of rotation of the tire, extending axially from a first axial end as far as a second axial end over an axial width L and extending radially from a radially interior first face as far as a radially exterior second face over a mean radial thickness T;
the protective reinforcement comprising reinforcers coated in an elastomer compound, having a diameter D and having a path in a circumferential direction of the tire;
the protective reinforcement being radially on an outside of a working reinforcement;
the working reinforcement comprising at least two radially superposed working layers made up of reinforcers having a zigzag path in the circumferential direction of the tire;
wherein the protective reinforcement has a mean radial thickness T at least equal to two times the diameter D of a said reinforcer, wherein the protective reinforcement comprises respectively on its radially interior face and on its radially exterior face parts made of elastomeric compound having an axial width W at least equal to the diameter D of a said reinforcer,
wherein the radially interior face of the protective reinforcement is an innermost layer of the reinforcers and the radially exterior face of the protective reinforcement is an outermost layer of the reinforcers,
wherein the path in the circumferential direction of the tire of any said reinforcer of the protective reinforcement, in the circumferential direction of the tire, varies radially between the radially interior first face and the radially exterior second face, in such a way that the set of paths of said reinforcers of the protective reinforcement constitutes a three-dimensional lattice and wherein the path in the circumferential direction of the tire of any said reinforcer of the protective reinforcement, in the circumferential direction of the tire, is a zigzag curve extending axially over the axial width L of the protective reinforcement.

2. The aircraft tire according to claim 1 , wherein the protective reinforcement has a mean radial thickness T at most equal to five times the diameter D of a said reinforcer.

3. The aircraft tire according to claim 1 , wherein the axial width W of the parts made of elastomeric compound, comprised respectively on the radially interior face and on the radially exterior face of the protective reinforcement, is at most equal to ten times the diameter D of a said reinforcer.

4. The aircraft tire according to claim 1 , wherein in any meridian plane, a ratio R, between a sum of the axial widths W of the parts made of elastomeric compound, comprised respectively on the radially interior face and on the radially exterior face of the protective reinforcement, and the axial width L of the protective reinforcement, is at least equal to 0.08.

5. The aircraft tire according to claim 1 , wherein in any meridian plane, a ratio R, between a sum of the axial widths W of the parts made of elastomeric compound, comprised respectively on the radially interior face and on the radially exterior face of the protective reinforcement, and the axial width L of the protective reinforcement, is at most equal to 0.20.

6. The aircraft tire according to claim 1 , wherein the reinforcers of the protective reinforcement are grouped into strips, comprising at least two consecutive reinforcers and having an axial width B.

7. The aircraft tire according to claim 6 , wherein an axial spacing P 1 between two consecutive said strips of said reinforcers each having a path, in the circumferential direction of the tire, that follows a zigzag curve is at least equal to 0.5 times the axial width B of a said strip and at most equal to five times the axial width B of a said strip.

8. The aircraft tire according to claim 1 , wherein the path of any said reinforcer, in the circumferential direction of the tire, is a periodic zigzag curve having an amplitude A equal to the axial width L of the protective reinforcement and having a period P=2ΠR1/K, K being a non-integer number in a range ]N, N+1[ where N is an integer at least equal to 0 and at most equal to 9, and R 1 being a radius of the radially interior first face.

9. The aircraft tire according to claim 1 , wherein the reinforcers of the protective reinforcement are made of at least one textile material.

10. The aircraft tire according to claim 1 , wherein the reinforcers of the protective reinforcement are made of an aliphatic polyamide or of an aromatic polyamide or of a combination of an aliphatic polyamide and of an aromatic polyamide.

11. The aircraft tire according to claim 1 , wherein the axial width W of the parts made of elastomeric compound, comprised respectively on the radially interior face and on the radially exterior face of the protective reinforcement, is at most equal to five times the diameter D of a said reinforcer.

12. The aircraft tire according to claim 1 , wherein, in any meridian plane, a ratio R, between a sum of the axial widths W of the parts made of elastomeric compound, comprised respectively on the radially interior face and on the radially exterior face of the protective reinforcement, and the axial width L of the protective reinforcement, is at least equal to 0.10.

13. The aircraft tire according to claim 12 , wherein, in any meridian plane, the ratio R, between the sum of the axial widths W of the parts made of elastomeric compound, comprised respectively on the radially interior face and on the radially exterior face of the protective reinforcement, and the axial width L of the protective reinforcement, is at most equal to 0.15.

14. The aircraft tire according to claim 1 , wherein the path of any said reinforcer, in the circumferential direction of the tire, is a periodic zigzag curve having an amplitude A equal to the axial width L of the protective reinforcement and having a period P=2ΠR1/K, K being a non-integer number in a range ]N, N+1[ where N is an integer at least equal to 0 and at most equal to 4, and R 1 being a radius of the radially interior first face.

Assignees

• Michelin & Cie
• Michelin Rech Tech

Inventors

• Kiebre Rimyalegdo
• Francois Olivier

Classifications

• B60C2009/2025

  with angle different or variable in the same layer · CPC title

• B60C9/2009

  comprising plies of different materials · CPC title

• B60C9/263 Primary

  further characterised by an endless zigzag configuration in at least one belt ply, i.e. no cut edge being present · CPC title

• B60C2200/02

  for aircrafts · CPC title

• B60C9/1807 Primary

  comprising fabric reinforcements · CPC title