Aircraft tire with carcass reinforcement including first and second families of carcass layers

Patent metadata

Field	Value
Publication number	US-9987887-B2
Application number	US-201314397090-A
Country	US
Kind code	B2
Filing date	Apr 15, 2013
Priority date	Apr 24, 2012
Publication date	Jun 5, 2018
Grant date	Jun 5, 2018

Abstract

Aircraft tire comprises carcass reinforcement ( 5 ) comprising a first family of carcass layers extending between two beads ( 3 ), having at least one carcass layer wrapped, within each bead, from the inside towards the outside of the tire, around a bead wire ( 6 ) to form turn-up ( 511 ) having free end (E 1 ) radially outside of radially outermost point (E) of the bead wire. The second family comprises at least two carcass layers, adjacent each to the next, extending, within each bead, from outside towards inside of the tire, as far as their respective ends (E 2 ) which are radially inside of axial straight line (D Y ) through centre (O) of bead wire ( 6 ) and axially inside of a radial straight line (D Z ) through centre (O) at axial distance (d 2 ) at least equal to 5 mm. The carcass layers of the second family are axially inside of at least one turn-up of a carcass layer of the first family.

First claim

The invention claimed is:

1. An aeroplane tire, comprising:
a tread connected by two side walls to two beads, which provide a mechanical connection between the tire and a rim;
a crown reinforcement, radially on the inside of the tread, and a carcass reinforcement radially on the inside of the crown reinforcement;
the carcass reinforcement comprising a first and a second family of carcass layers extending between the two beads;
the first family comprising at least one carcass layer wrapped, within each said bead, from the inside towards the outside of the tire, around a circumferential reinforcing element known as a bead wire to form a turn-up having a free end radially on the outside of the radially outermost point of the bead wire; and
the second family comprising at least two carcass layers, adjacent each to the next, extending, within each said bead, from the outside towards the inside of the tire, as far as their respective ends which are radially on the inside of an axial straight line passing through the centre of the bead wire and axially on the inside of a radial straight line passing through the centre of the bead wire at an axial distance at least equal to 5 mm,
wherein the carcass layers of the second family are axially on the inside of at least one turn-up of a carcass layer of the first family,
wherein each carcass layer comprises mutually parallel reinforcing elements,
wherein the reinforcing elements of each carcass layer are made of textile materials, and
wherein the textile reinforcing elements of each carcass layer being obtained by twisting, in the clockwise direction, at least two overtwists, each overtwist being obtained by twisting, in the anticlockwise direction, a spun fibre consisting of mutually parallel textile filaments, this twisting being defined by a number of turns per meter referred to as overtwisting,
wherein the overtwisting, to obtain the overtwists of the textile reinforcing elements of the carcass layers, is at least equal to 250 turns/meter and at most 290 turns/meter.

2. The aeroplane tire according to claim 1 , wherein the carcass layers of the second family are axially on the inside of all the turn-ups of the carcass layers of the first family.

3. The aeroplane tire according to claim 1 , wherein the overtwists of the textile reinforcing elements of each carcass layer are made of aliphatic polyamide filaments.

4. The aeroplane tire according to claim 1 , wherein the overtwists of the textile reinforcing elements of each carcass layer are made of aromatic polyamide filaments.

5. The aeroplane tire according to claim 1 , wherein the overtwists of the textile reinforcing elements of each carcass layer consist of at least one overtwist made of aliphatic polyamide filaments and at least one overtwist made of aromatic polyamide filaments.

6. The aeroplane tire according to claim 1 , which comprises an additional reinforcing layer wrapped around the bead wire and separating the bead wire from the carcass layers.

7. An aeroplane tire, comprising:
a tread connected by two side walls to two beads, which provide a mechanical connection between the tire and a rim;
a crown reinforcement, radially on the inside of the tread, and a carcass reinforcement radially on the inside of the crown reinforcement;
the carcass reinforcement comprising a first and a second family of carcass layers extending between the two beads;
the first family comprising at least one carcass layer wrapped, within each said bead, from the inside towards the outside of the tire, around a circumferential reinforcing element known as a bead wire to form a turn-up having a free end radially on the outside of the radially outermost point of the bead wire; and
the second family comprising at least two carcass layers, adjacent each to the next, extending, within each said bead, from the outside towards the inside of the tire, as far as their respective ends which are radially on the inside of an axial straight line passing through the centre of the bead wire and axially on the inside of a radial straight line passing through the centre of the bead wire at an axial distance at least equal to 5 mm,
wherein the carcass layers of the second family are axially on the inside of at least one turn-up of a carcass layer of the first family,
wherein each carcass layer comprises mutually parallel reinforcing elements,
wherein the reinforcing elements of each carcass layer are made of textile materials, and
wherein the textile reinforcing elements of each carcass layer being obtained by twisting, in the clockwise direction, at least two overtwists, each overtwist being obtained by twisting, in the anticlockwise direction, a spun fibre consisting of mutually parallel textile filaments, this twisting being defined by a number of turns per meter referred to as overtwisting,
wherein the overtwisting, to obtain the overtwists of the textile reinforcing elements of the carcass layers, of the second family is at least equal to 1.15 times the overtwisting, to obtain the overtwists of the textile reinforcing elements of the carcass layers of the first family.

8. The aeroplane tire according to claim 7 , wherein the carcass layers of the second family are axially on the inside of all the turn-ups of the carcass layers of the first family.

9. The aeroplane tire according to claim 7 , wherein the overtwists of the textile reinforcing elements of each carcass layer are made of aliphatic polyamide filaments.

10. The aeroplane tire according to claim 7 , wherein the overtwists of the textile reinforcing elements of each carcass layer are made of aromatic polyamide filaments.

11. The aeroplane tire according to claim 7 , wherein the overtwists of the textile reinforcing elements of each carcass layer consist of at least one overtwist made of aliphatic polyamide filaments and at least one overtwist made of aromatic polyamide filaments.

12. The aeroplane tire according to claim 7 , which comprises an additional reinforcing layer wrapped around the bead wire and separating the bead wire from the carcass layers.

Assignees

• Michelin & Cie
• Michelin Rech Tech

Inventors

• Caffeau Charlotte
• Boursin Arnaud

Classifications

• B60C2200/02

  for aircrafts · CPC title

• B60C2009/0466

  Twist structures · CPC title

• B60C2009/0092

  Twist structure · CPC title

• B60C15/0632

  using flippers in contact with and wrapped around the bead core and, at least partially, in contact with the bead filler · CPC title

• B60C15/0018

  not folded around the bead core, e.g. floating or down ply · CPC title