Method for manufacturing composite fiber preform for disc brakes

Patent metadata

Field	Value
Publication number	US-11655870-B2
Application number	US-201916596585-A
Country	US
Kind code	B2
Filing date	Oct 8, 2019
Priority date	Oct 8, 2019
Publication date	May 23, 2023
Grant date	May 23, 2023

Abstract

A method that includes winding a composite fabric around a mandrel to form a plurality of layers defining an annulus extending along a central longitudinal axis, where the composite fabric includes a plurality of elongate axial fibers extending substantially in an axial direction relative to the longitudinal axis and a plurality of elongate circumferential fibers extending substantially in a circumferential direction relative to the longitudinal axis; and introducing, into at least a portion of the plurality of layers, a plurality of radial fibers extending substantially in the radial direction relative to the longitudinal axis, where the plurality of radial fibers mechanically bind one or more adjacent layers of the plurality of layers.

First claim

What is claimed is:

1. A method comprising:
winding a composite fabric around a first mandrel to form a fiber preform including a plurality of layers defining an annulus extending along a central longitudinal axis, wherein the composite fabric comprises:
a plurality of elongate axial fibers extending substantially in an axial direction relative to the longitudinal axis; and
a plurality of elongate circumferential fibers extending substantially in a circumferential direction relative to the longitudinal axis;

controlling, while winding the composite fabric, a tension of the composite fabric, wherein controlling the tension of the composite fabric includes applying resistive tension to a second mandrel comprising a roll of the composite fabric; and
introducing, into at least a portion of the plurality of layers, 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.

2. The method of claim 1 , wherein controlling the tension of the composite fabric comprises controlling the tension of the composite fabric such that a percent of a fiber volume relative to a total volume of the fiber preform is from about 15% to about 50%.

3. The method of claim 1 , wherein introducing the plurality of radial fibers comprises, during winding, needle-punching the fiber preform.

4. The method of claim 1 , wherein introducing the plurality of radial fibers comprises, during winding, tufting the fiber preform.

5. The method of claim 1 , wherein introducing the plurality of radial fibers further comprises controlling a frequency and a timing of at least one of needle-punching or tufting.

6. The method of claim 1 , further comprising:
pyrolyzing the fiber preform to carbonize at least a portion of the composite fabric; and
densifying the carbonized fiber preform to form a densified carbon-carbon composite material.

7. The method of claim 1 , further comprising:
at least partially densifying the carbon fiber preform; and
sectioning the at least partially densified carbon fiber preform into discs defining composite brake pads.

8. A system comprising:
a composite fabric source comprising a composite fabric;
a mandrel configured to wind the composite fabric around the mandrel to form 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;
a plurality of elongate circumferential fibers extending substantially in the circumferential direction, wherein at least 40% of the plurality of elongate axial 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,

a needler configured to introduce the plurality of radial fibers into selected layers of the plurality of layers, wherein the needler includes a curved member having a plurality of needles extending from the curved member, the curved member being curved about the central longitudinal axis.

9. The system of claim 8 , wherein the mandrel comprises a first mandrel, and wherein the composite fabric source comprises a second mandrel, wherein the composite fabric is wound on the second mandrel.

10. The system of claim 9 , further comprising a tensioner coupled to the second mandrel, wherein the tensioner is configured to, during winding of the composite fabric onto the first mandrel, control a tension of the composite fabric.

11. The system of claim 8 , further comprising:
a motor coupled to the mandrel, wherein the motor is configured to rotate the mandrel; and
a controller communicatively coupled to the motor, wherein the controller is configured to control a speed of rotation of the mandrel.

12. The system of claim 8 , wherein the mandrel comprises a graphite mandrel.

13. The system of claim 8 , wherein the mandrel comprises a metal rod and a graphite ring coupled to at least a portion of the metal rod.

14. The system of claim 8 , further comprising at least one tensioning bar configured to, during winding of the composite fabric onto the first mandrel, control a tension of the composite fabric.

15. The system of claim 8 , wherein the needler is a first needler, the curved member is a first curved member, and the radius of curvature of the first curved member is a first radius of curvature, the system further comprising a second needler configured to introduce the plurality of radial fibers into selected layers of the plurality of layers, wherein the second needler comprises a second curved member having a second radius of curvature, and wherein the second radius of curvature is greater than the first radius of curvature.

16. The system of claim 8 , further comprising a tufting device configured to introduce the plurality of radial fibers into selected layers of the plurality of layers.

17. A system comprising:
a composite fabric source comprising a composite fabric wound around a first mandrel; and
a second mandrel configured to wind the composite fabric from the first mandrel around the second mandrel to form 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;
a plurality of elongate circumferential fibers extending substantially in the circumferential direction, wherein at least 40% of the plurality of elongate axial 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.

18. The system of claim 17 , further comprising a tensioner coupled to the first mandrel, wherein the tensioner is configured to, during winding of the composite fabric onto the second mandrel, control a tension of the composite fabric.

19. The system of claim 17 , wherein the mandrel comprises a metal rod and a graphite ring coupled to at least a portion of the metal rod.

20. The system of claim 17 , wherein the mandrel comprises a graphite mandrel.

Assignees

• Honeywell Int Inc

Inventors

• Shula Brian
• Evans Christopher
• Charles David L
• Fryska Slawomir T

Classifications

• B29C70/32 Primary

  on a rotating mould, former or core · CPC title

• B29L2031/7482

  Brakes · CPC title

• C04B2235/5268

  Orientation of the fibers · CPC title

• F16D2200/0065

  Inorganic, e.g. non-asbestos mineral fibres · CPC title

• B29L2031/16

  Frictional elements, e.g. brake or clutch linings · CPC title