Ultrahigh-temperature particle-incorporated composite and methods of manufacturing thereof

Patent metadata

Field	Value
Publication number	US-2025249656-A1
Application number	US-202418433845-A
Country	US
Kind code	A1
Filing date	Feb 6, 2024
Priority date	Feb 6, 2024
Publication date	Aug 7, 2025
Grant date	—

Abstract

A prepreg that is embedded with ultrahigh-temperature particles by coating one or more veil carrier with ultrahigh-temperature particles, and then incorporating the one or more of the modified veil layer with one or more fabric layer to form a reinforced fabric for a prepreg to enable the formation of layups with tailored amounts of the ultrahigh-temperature particles that vary through the thickness of the reinforced fabric to enable a functionally graded composite that can withstand ultrahigh temperatures.

First claim

What is claimed is:

1 . A reinforced fabric for prepregs, comprising:
one or more of a modified veil layer that comprises a nonwoven veil carrier coated with ultrahigh-temperature particles; and one or more of a fabric layer abutting a surface of the modified veil layer to form a reinforced fabric that is configured to be incorporated into a prepreg.

2 . The reinforced fabric of claim 1 , wherein the ultrahigh-temperature particles comprise ceramic particles.

3 . The reinforced fabric of claim 2 , wherein the ceramic particles are selected from the group consisting of titanium carbide particles, hafnium carbide particles, and a combination thereof.

4 . The reinforced fabric of claim 1 , wherein the nonwoven veil carrier comprises a thermoplastic nonwoven veil.

5 . The reinforced fabric of claim 1 , wherein the modified veil layer is provided in between first and second fabric layers, and further wherein one surface of the modified veil layer abuts a first fabric layer, and a second surface of the modified veil layer abuts a second fabric layer.

6 . The reinforced fabric of claim 1 , wherein the modified veil layer includes two or more coatings comprising ultrahigh-temperature particles.

7 . A method to manufacture a reinforced fabric for prepregs, comprising:
preparing a modified veil layer by coating a nonwoven veil carrier with ultrahigh-temperature particles; layering the modified veil layer onto a surface of a fabric layer; and forming a reinforced fabric that is configured to be incorporated into a prepreg.

8 . The method of claim 7 , wherein preparing the modified veil layer includes submerging the nonwoven veil carrier into a coating solution comprising the ultrahigh-temperature particles and a carrier fluid.

9 . The method of claim 7 , wherein the ultrahigh-temperature particles comprise ceramic particles.

10 . The method of claim 9 , wherein the ceramic particles comprise titanium carbide particles, hafnium carbide particles, or a combination thereof.

11 . The method of claim 7 , wherein preparing the modified veil layer includes pretreating the nonwoven veil carrier to impart a positive or negative charge onto the nonwoven veil carrier.

12 . The method of claim 7 , wherein preparing the modified veil layer further comprises submerging the nonwoven veil carrier in more than one coating solutions and rinsing the nonwoven veil carrier in at least one rinse bath in between submerging the nonwoven veil carrier in each of the more than one coating solutions.

13 . The method of claim 12 , wherein the at least one rinse bath is comprised of the same carrier fluid as the coating solution immediately prior to the at least one rinse bath.

14 . The method of claim 7 , further comprising mechanically compressing the modified veil layer with the fabric layer to form the reinforced fabric.

15 . The method of claim 7 , further comprising heat-treating the reinforced fabric using an oven.

16 . A method to manufacture a prepreg, comprising:
preparing a modified veil layer by coating a nonwoven veil carrier with ultrahigh-temperature particles; layering the modified veil layer onto a surface of a fabric layer; forming a reinforced fabric; heat-treating the reinforced fabric; decompose the nonwoven veil carrier; and embedding the ultrahigh-temperature particles into the fabric layer.

17 . The method of claim 16 , wherein the reinforced fabric is heated using an oven.

18 . The method of claim 16 , wherein the ultrahigh-temperature particles comprise ceramic particles.

19 . The method of claim 16 , wherein preparing the modified veil layer further comprises submerging the nonwoven veil carrier into a coating solution with the ultrahigh-temperature particles.

20 . The method of claim 16 , wherein preparing the modified veil layer further comprises submerging the nonwoven veil carrier in more than one coating solutions and rinsing the nonwoven veil carrier in at least one rinse bath in between submerging the nonwoven veil carrier in each of the more than one coating solutions.

Assignees

• Boeing Co

Inventors

• Tsotsis Thomas Karl

Classifications

• B32B2307/306

  Resistant to heat · CPC title

• B32B2260/046

  Synthetic resin · CPC title

• B32B2260/023

  Two or more layers · CPC title

• B32B5/265 Primary

  characterised by one fibrous or filamentary layer being a non-woven fabric layer · CPC title

• B32B5/022

  Non-woven fabric · CPC title