IP Library Granted Patent US 12,338,182
Granted Patent B2
US 12,338,182 · App. 18/678,649 · Granted Jun 24, 2025

Through thickness reinforcement

Inventor: Olivier H. Sudre (Glastonbury, CT)
Assignee: RTX Corporation
C04B35/80C04B35/62863C04B35/62884C04B35/652C04B35/657F01D5/284F01D9/02F01D11/00F23R3/002C04B2235/3826C04B2235/5244C04B2235/5252C04B2235/614C04B2235/616F05D2220/32F05D2240/12F05D2240/30F05D2240/35F05D2240/55F05D2300/20
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,338,182
App. No.
18/678,649
Granted
Jun 24, 2025
Kind
B2
Abstract

A method for making a ceramic matrix composite component includes densifying a fibrous preform of the component with a ceramic matrix to form an intermediate component; infiltrating a hole in the intermediate component with an infiltrate material comprising a solid and a metallic alloy whose reaction forms a carbide, silicide, boride or combination thereof, heating the infiltrate material to a temperature in excess of a melting point of the metallic alloy; and sequentially cooling regions of the hole starting from an interior end of the hole to the outer surface of the intermediate component to form a solidified through-thickness reinforcement element. The hole extends in a through-thickness direction and is open to an exterior surface of the intermediate component.

Claims (20)

1. A ceramic matrix composite component comprising:

a ceramic matrix;

a plurality of ceramic fibers embedded in the ceramic matrix; and

a reinforcement element disposed through the ceramic matrix and ceramic fibers,

wherein the reinforcement element comprises a carbide, silicide, boride or combination thereof, and

wherein an average crystal size of the reinforcement element is greater than an average crystal size of the ceramic matrix.

2. The ceramic matrix composite component of claim 1 , wherein the reinforcement element is a polycrystalline, eutectic, or single crystal ceramic.

3. The ceramic matrix composite component of claim 1 , wherein the reinforcement element comprises silicon carbide.

4. The ceramic matrix composite component of claim 3 , wherein the reinforcement element further comprises aluminum, boron, chromium, hafnium, iron, molybdenum, niobium, rare earth metals, scandium, tantalum, titanium, tungsten, vanadium, yttrium, zirconium, or a combination thereof.

5. The ceramic matrix composite component of claim 1 , wherein the reinforcement element extends through a full thickness of the component.

6. The ceramic matrix composite of claim 1 , wherein the reinforcement element extends through a partial thickness of the component.

7. The ceramic matrix composite component of claim 1 , wherein the ceramic fibers of the plurality of ceramic fibers are arranged in woven fiber layers and wherein the reinforcement element extends through a plurality of woven fiber layers.

8. The ceramic matrix composite component of claim 1 , wherein an interphase material is disposed between the reinforcement element and the matrix.

9. The ceramic matrix composite component of claim 1 , wherein the reinforcement element is cylindrical.

10. The ceramic matrix composite component of claim 9 , wherein the reinforcement element has a diameter greater than 300 micrometers.

11. The ceramic matrix composite component of claim 9 , wherein the reinforcement element has a diameter within the range of 50 to 100 micrometers.

12. The ceramic matrix composite component of claim 1 , further comprising a plurality of reinforcement elements selectively located in the ceramic matrix composite component.

13. The ceramic matrix composite component of claim 12 , wherein the plurality of reinforcement elements makes up at least 5 volume percent of the ceramic matrix composite component.

14. The ceramic matrix composite component of claim 12 , wherein reinforcement elements of the plurality of reinforcement elements are angled relative to an outer surface.

15. The ceramic matrix composite component of claim 12 , wherein ceramic fibers of the plurality of ceramic fibers are arranged in a plurality of woven fiber layers and wherein the plurality of reinforcement elements extend through the plurality of woven fiber layers.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 31, 2024
From: SUDRE, OLIVIER H.
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 067579/0707 →
CHANGE OF NAME Recorded May 31, 2024
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 067596/0968 →
Continuity (2)
Division 17339185 · Jun 4, 2021
Related Publication 20240308924A1 · Sep 19, 2024
References Cited (12)
US 6280550B1 · Steibel et al. · 2001 [cited by applicant]
US 10384981B2 · Hall et al. · 2019 [cited by applicant]
US 10618848B2 · Luthra et al. · 2020 [cited by applicant]
US 20040192534A1 · Nixon · 2004 [cited by examiner]
US 20060019087A1 · Mazzola · 2006 [cited by examiner]
US 20060283014A1 · Subramanian · 2006 [cited by examiner]
US 20090214845A1 · Corman et al. · 2009 [cited by applicant]
US 20130184141A1 · Ogasawara et al. · 2013 [cited by applicant]
US 20180312442A1 · Shinavski et al. · 2018 [cited by applicant]
US 20190185384A1 · Shim · 2019 [cited by examiner]
Extended European Search Report for EP Application No. 22170120.4, dated Sep. 21, 2022, 7 pages. [cited by applicant]
W.-T. Chen, et al., “Directionally Solidified Boride and Carbide Eutectic Ceramics”, from J. Am. Ceram. Soc., 99 [6], pp. 1837-1851 (2016). [cited by applicant]