Part fabrication utilizing in-situ reaction formation of fiber-reinforced ceramic

Patent metadata

Field	Value
Publication number	US-2025381706-A1
Application number	US-202519240536-A
Country	US
Kind code	A1
Filing date	Jun 17, 2025
Priority date	Jun 17, 2024
Publication date	Dec 18, 2025
Grant date	—

Abstract

A method of additively manufacturing a part by printing the part, layer-by-layer, on a substrate, such that the part is formed of a plurality of layers, each of the layers is built up by simultaneously: (i) directing a fiber feedstock stream, of fiber feedstock, toward a point of deposition on the substrate or a previously deposited layer; (ii) directing one or more precursor streams, of one or more precursors, toward the point of deposition on or near the fiber feedstock stream; and (iii) directing one or more energy sources toward the point of deposition; the one or more precursors reacts to form a ceramic that is deposited on and around the fiber feedstock, thereby forming a ceramic matrix composite that includes the ceramic formed from the one or more precursor streams embedded with fiber from the fiber feedstock; and repeating steps (i) to (iii) until printing the layers is complete.

First claim

What is claimed is:

1 . A method of additively manufacturing a part, comprising:
printing the part, layer-by-layer, on a substrate, such that the part is formed of a plurality of layers, wherein each of the layers is built up by simultaneously: (i) directing a fiber feedstock stream, of fiber feedstock, toward a point of deposition on the substrate or a previously deposited layer; (ii) directing one or more precursor streams, of one or more precursors, toward the point of deposition on or near the fiber feedstock stream; and (iii) directing one or more energy sources toward the point of deposition, whereby the one or more precursors reacts to form a ceramic that is deposited on and around the fiber feedstock, thereby forming a ceramic matrix composite that includes the ceramic formed from the one or more precursor streams embedded with fiber from the fiber feedstock; and repeating steps (i) to (iii) until printing the layers is complete.

2 . The method of claim 1 , wherein:
the one or more precursor streams includes a plurality of precursor streams, wherein the plurality of precursor streams are formed of mutually unique materials configured to react with one another to thereby form the ceramic.

3 . The method of claim 2 , wherein
the plurality of precursor streams includes a first precursor stream and a second precursor stream, wherein the first precursor stream comprises particles, and the method includes: selecting the second precursor stream to form a precursor coating or engage the particles in the first precursor stream, and applying the one or more energy sources at the point of deposition to cause one or more of the plurality of precursor streams to react or engage with the particles to form the ceramic.

4 . The method of claim 2 , wherein:
the one or more precursors includes a plurality of precursors, wherein one of the plurality of precursors includes one or more of silicon; hafnium; zirconium; titanium; tantalum; tungsten; niobium; molybdenum; or rhenium; and another one of the plurality of precursors includes one or more of boron, carbon, oxygen, or nitrogen; or a combination of any one of the plurality of precursors, within and between layers.

5 . The method of claim 1 , further comprising
selecting at least one of the one or more precursor streams and the one or more energy sources and directing the at least one of the one or more precursor streams and the one or more energy sources to the point of deposition on the fiber feedstock to react and form an interface layer; and selecting another one of the one or more precursor streams and another one of the one or more energy sources, and directing the another one of the one or more precursor streams and the another one of the one or more energy sources to the point of deposition on the interface layer, whereby the one or more precursors react to form the ceramic on the interface layer; thereby forming the ceramic matrix composite comprising the fiber feedstock, the ceramic, and the interface layer between the fiber and the ceramic.

6 . The method of claim 1 , wherein:
the fiber comprises one or more of a ceramic fiber, a carbon fiber or silicon carbide fiber; and the ceramic comprises of one or more of a carbon, boron carbide, boron nitride, silicon carbide, silicon nitride, hafnium carbide, or zirconium carbide.

7 . The method of claim 5 , wherein the interface layer comprises one or more of a carbon, or boron nitride.

8 . The method of claim 1 , comprising printing the part as a graded structure by varying, while printing, a relative amount of one or more of silicon, hafnium, zirconium, titanium, tantalum, tungsten, niobium, molybdenum, rhenium, boron, carbon, nitrogen, or oxygen.

9 . The method of claim 3 , comprising
heating the one or more precursor streams with the one or more energy sources to liquify or vaporize the one or more precursors or the precursor coating while forming the ceramic; or so that the one or more precursor streams, or the precursor coating, to remain as solid particulates and form the ceramic.

10 . The method of claim 1 , comprising
directing the one or more energy sources to the substrate through at least one of the one or more precursor streams or the fiber feedstock.

11 . The method of claim 1 , comprising:
printing each one of the layers to comprise lines, wherein: the lines on a layer are oriented parallel to each other; and the lines along successive ones of the layers are disposed at an angle to each other.

12 . The method of claim 1 , further including, after printing the part, one or more of:
applying chemical vapor infiltration (CVI) to the part to decrease porosity of the part; or heating the part to further complete conversion of precursors to product or densify the part by sintering.

13 . A system for additively manufacturing a part, comprising:
a chamber that is filled with an inert gas; a substrate in the chamber; a robotic arm in the chamber, wherein the robotic arm has one or more nozzles, and wherein the robotic arm is configured to produce an energy source; one or more precursor storage units from which the one or more nozzles obtains one or more precursors; and one or more feedstock storage units from which the one or more nozzles obtains fiber feedstock; wherein the robotic arm is configured to print the part, layer-by-layer, on the substrate, such that the part is formed of a plurality of layers, and wherein, within each one of the plurality of layers, the robotic arm is configured to, simultaneously: (i) direct a fiber feedstock stream, of the fiber feedstock, toward a point of deposition on the substrate or a previously deposited layer; (ii) direct one or more precursor streams toward the point of deposition on or near the fiber feedstock stream, and at least one of the one or more precursor streams includes a first precursor; and (iii) direct one or more energy sources toward the point of deposition, whereby the one or more precursors reacts to form a ceramic that is deposited on and around the fiber feedstock, thereby forming a ceramic matrix composite that includes the ceramic formed from the one or more precursor streams embedded with fiber from the fiber feedstock; and repeating steps (i) to (iii) until printing the layers is complete.

14 . The system of claim 13 , wherein:
the one or more precursor streams includes a plurality of precursor streams, wherein the plurality of precursor streams are formed of mutually unique materials configured to react with one another to thereby form the ceramic.

15 . The system of claim 13 , wherein
at least one of the one or more precursor streams, and the one or more energy sources, are configured for being selected, and the at least one of the one or more precursor streams and the one or more energy sources are configured for being directed to the point of deposition on the fiber feedstock to react and form an interface layer; another one of the one or more precursor streams and another one of the one or more energy sources are configured for being selected, and directing the another one of the one or more precursor streams and the another one of the one or more energy sources are configured for directed to the point of deposition on the interface layer, whereby the one or more precursors react to form the ceramic on the interface layer; whereby the ceramic matrix composite is formed, comprising the fiber feedstock, the ceramic, and the interface layer between the fiber and the ceramic.

16 . The system of claim 13 , wherein:
the one o

Assignees

• Raytheon Co

Inventors

• Skiba Tommy
• Singh Prabhjot
• Srinivasan Gajawalli V
• Vedula Venkata R
• De Bedout Juan
• Pujar Vijay V
• Boardman Sarah

Classifications

• C04B2235/614

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

• C04B2235/5248

  Carbon, e.g. graphite · CPC title

• C04B2235/5244

  Silicon carbide · CPC title

• C04B41/0072

  Heat treatment · CPC title

• B33Y40/10

  Pre-treatment · CPC title