IP Library Granted Patent US 11,976,568
Granted Patent B2
US 11,976,568 · App. 18/298,047 · Granted May 7, 2024

Ceramic matrix composite component having low density core and method of making

Inventors: Michael G. McCaffrey (Windsor, CT); Bryan P. Dube (Chepachet, RI)
Assignee: RTX CORPORATION
F01D5/282C04B35/62844C04B35/62884C04B35/80C23C16/045F01D5/18C04B2235/5252C04B2235/614F05D2220/32F05D2230/314F05D2300/6033
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Quick Facts
Patent No.
US 11,976,568
App. No.
18/298,047
Granted
May 7, 2024
Kind
B2
Abstract

Disclosed is a ceramic matrix component having a fibrous core and a ceramic matrix composite shell surrounding at least a portion of the fibrous core. The ceramic matrix composite shell comprises a fibrous preform. The fibrous core has a greater porosity than the fibrous preform. A method of making the ceramic matrix component is also disclosed.

Claims (10)

1. A ceramic matrix component comprising a fibrous core and a ceramic matrix composite shell surrounding at least a portion of the fibrous core, wherein the ceramic matrix composite shell comprises a fibrous preform and the fibrous core has a greater porosity than the fibrous preform and the fibrous core further comprises ceramic foam and the ceramic foam is positioned at a trailing edge of the fibrous core.

2. The ceramic matrix component of claim 1 , wherein a porosity of the fibrous core is 2-3 times greater than a porosity of the fibrous preform.

3. The ceramic matrix component of claim 1 , wherein the fibrous core comprises cooling passages.

4. The ceramic matrix component of claim 3 , wherein the cooling passages are located at a leading edge of the ceramic matrix component.

5. The ceramic matrix component of claim 3 , wherein the cooling passages are located at the trailing edge of the ceramic matrix component.

6. The ceramic matrix component of claim 1 , wherein the ceramic matrix composite shell has a thickness greater than or equal to 0.03 inch.

7. A method of making a ceramic matrix component comprising forming a fibrous core having a first porosity, forming a fibrous preform on the fibrous core wherein the fibrous preform has a porosity less than the first porosity, and forming a ceramic matrix on the fibrous preform using chemical vapor infiltration and the fibrous core further comprises ceramic foam and the ceramic foam is positioned at a trailing edge of the fibrous core.

8. The method of claim 7 , wherein the fibrous core comprises sacrificial fibers.

9. The method of claim 8 , wherein the sacrificial fibers are located at a leading edge of the fibrous core.

10. The method of claim 8 , wherein the sacrificial fibers are located at a trailing edge of the fibrous core.

Assignments (3)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064402/0837 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 10, 2023
From: MCCAFFREY, MICHAEL G.; DUBE, BRYAN P.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 063276/0876 →
CHANGE OF NAME Recorded Apr 10, 2023
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 063282/0554 →
Continuity (2)
Continuation 16797123 · Feb 21, 2020
Related Publication 20230250726A1 · Aug 10, 2023