Composite fiber preform for disc brakes

Patent metadata

Field	Value
Publication number	US-11293507-B2
Application number	US-201916596557-A
Country	US
Kind code	B2
Filing date	Oct 8, 2019
Priority date	Oct 8, 2019
Publication date	Apr 5, 2022
Grant date	Apr 5, 2022

Abstract

A fiber preform defining an annulus extending along a central longitudinal axis. The fiber preform includes a plurality of layers extending in an axial direction and a circumferential direction relative to the longitudinal axis. Each layer of the plurality of layers includes a plurality of elongate fibers. The plurality of elongate fibers include a plurality of elongate axial fibers extending substantially in the axial direction and a plurality of elongate circumferential fibers extending substantially in the circumferential direction. The fiber preform also includes a plurality of radial fibers extending substantially in the radial direction. The plurality of radial fibers mechanically bind one or more adjacent layers of the plurality of layers. At least 40% of the plurality of elongate fibers extend substantially in the axial direction.

First claim

What is claimed is:

1. A fiber preform defining an annulus extending along a central longitudinal axis, the fiber preform comprising:
a plurality of layers extending in an axial direction and a circumferential direction relative to the longitudinal axis, wherein each layer of the plurality of layers comprises a plurality of elongate fibers comprising:
a plurality of elongate axial fibers extending substantially in the axial direction; and
a plurality of elongate circumferential fibers extending substantially in the circumferential direction,

wherein at least 40% of the plurality of elongate fibers extend substantially in the axial direction; and
a plurality of radial fibers extending substantially in the radial direction relative to the longitudinal axis, wherein the plurality of radial fibers mechanically bind one or more adjacent layers of the plurality of layers,
wherein the annulus comprises:
an inner radial section comprising at least an inner layer of the plurality of layers defining an inner preform diameter, the inner radial section having a first percentage of fibers of the plurality of radial fibers;
an outer radial section comprising at least an outer layer of the plurality of layers defining an outer preform diameter, the outer radial section having a second percentage of fibers of the plurality of radial fibers; and
a central radial section between the inner radial section and the outer radial section, the central radial section having a third percentage of fibers of the plurality of radial fibers,
wherein at least one of the first percentage or the second percentage is greater than the third percentage.

2. The fiber perform of claim 1 , wherein at least 40% of the plurality of elongate fibers extend in the circumferential direction.

3. The fiber perform of claim 1 , wherein less than 20% of all fibers of the fiber preform extend in the radial direction.

4. The fiber preform of claim 1 , wherein a volume of the plurality of elongate fibers is about 15% to about 50% a total volume of the fiber preform.

5. The fiber preform of claim 1 , wherein the plurality of elongate fibers comprises continuous elongate fibers.

6. The fiber preform of claim 1 , wherein each layer of the plurality of layers comprises a first layer comprising a continuous fiber fabric and a second layer comprising a nonwoven fiber fabric.

7. The fiber preform of claim 6 , wherein the nonwoven fiber fabric comprises a plurality of web fibers.

8. The fiber preform of claim 1 , wherein each layer of the plurality of layers comprises a duplex fabric.

9. The fiber preform of claim 1 , wherein the plurality of elongate fibers comprise a plurality of elongate carbon fibers.

10. The fiber preform of claim 1 , wherein the plurality of layers comprises between 30 layers and 520 layers.

11. The fiber preform of claim 1 , wherein a thickness of the fiber preform is about 2.54 centimeters to about 7.62 centimeters.

12. A fiber preform defining a cylinder extending along a central longitudinal axis, the fiber preform comprising:
a plurality of fibrous layers extending in an axial direction and a circumferential direction relative to the cylinder, wherein each layer of the plurality of fibrous layers comprises a woven fabric comprising:
a plurality of elongate axial fibers extending substantially in the axial direction; and
a plurality of elongate circumferential fibers extending substantially in the circumferential direction,
wherein at least 40% of fibers of the woven fabric extend substantially in the axial direction;

a plurality of radial fibers extending substantially in the radial direction relative to the cylinder, wherein the plurality of radial fibers mechanically bind one or more adjacent layers of the plurality of fibrous layers;
an inner radial section defining an inner preform diameter, comprising at least an inner layer of the plurality of fibrous layers and a first percentage of fibers of the plurality of radial fibers;
an outer radial section defining an outer preform diameter, comprising at least an outer layer of the plurality of fibrous layers and a second percentage of fibers of the plurality of radial fibers; and
a central radial section between the inner radial section and the outer radial section, comprising at least one layer of the plurality of fibrous layers between the inner layer and the outer layer and a third percentage of fibers of the plurality of radial fibers,
wherein at least one of the first percentage or the second percentage is greater than the third percentage.

13. A carbon-carbon composite disc brake defining an annulus extending along a central longitudinal axis, the carbon-carbon composite disc brake comprising:
a plurality of layers extending in an axial direction and a circumferential direction relative to the longitudinal axis, wherein each layer of the plurality of layers comprises a plurality of elongate carbon fibers comprising:
a plurality of elongate axial fibers extending substantially in the axial direction; and
a plurality of elongate circumferential fibers extending substantially in the circumferential direction,
wherein at least 40% of the plurality of elongate carbon fibers extend substantially in the axial direction; and

a plurality of radial carbon fibers extending substantially in the radial direction relative to the longitudinal axis, wherein the plurality of radial fibers mechanically bind one or more adjacent layers of the plurality of layers,
wherein the annulus comprises:
an inner radial section comprising at least an inner layer of the plurality of layers defining an inner preform diameter, the inner radial section having a first percentage of carbon fibers of the plurality of radial carbon fibers;
an outer radial section comprising at least an outer layer of the plurality of layers defining an outer preform diameter, the outer radial section having a second percentage of carbon fibers of the plurality of radial carbon fibers; and
a central radial section between the inner radial section and the outer radial section, the central radial section having a third percentage of carbon fibers of the plurality of radial carbon fibers,
wherein at least one of the first percentage or the second percentage is greater than the third percentage.

14. The carbon-carbon composite disc brake of claim 13 , wherein at least 40% of the plurality of elongate carbon fibers extend in the circumferential direction.

15. The carbon-carbon composite disc brake of claim 13 , wherein less than 20% of all fibers of the fiber preform extend in the radial direction.

16. The carbon-carbon composite disc brake of claim 13 , wherein a percentage of a volume of the plurality of elongate carbon fibers to a volume of the fiber preform is from about 15% to about 50%.

17. The carbon-carbon composite disc brake of claim 13 , wherein the plurality of elongate carbon fibers comprises continuous elongate carbon fibers.

18. The carbon-carbon composite disc brake of claim 13 , wherein each layer of the plurality of layers comprises a first layer comprising a continuous carbon fiber fabric and a second layer comprising a nonwoven carbon fiber fabric.

Assignees

• Honeywell Int Inc

Inventors

• Shula Brian

Classifications

• C04B2235/77

  Density · CPC title

• C04B2235/6567

  Treatment time · CPC title

• C04B2235/614

  Gas infiltration of green bodies or pre-forms · CPC title

• C04B2235/6028

  Shaping around a core which is removed later · CPC title

• C04B2235/5268

  Orientation of the fibers · CPC title