IP Library Granted Patent US 10,654,756
Granted Patent B1
US 10,654,756 · App. 15/875,283 · Granted May 19, 2020

Formulations for engineered ceramic matrix composites for high temperature applications

Inventor: Sai V. Raj (Strongsville, OH)
Assignee: United States of America as Represented by the Administrator of National Aeronautics and Space Administration
C04B35/806C04B35/6261C04B35/6264C04B35/657C04B41/009C04B41/5064C04B41/87C04B2235/3826C04B2235/3873C04B2235/3891C04B2235/5244C04B2235/606C04B2235/616C04B2235/728
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Quick Facts
Patent No.
US 10,654,756
App. No.
15/875,283
Granted
May 19, 2020
Kind
B1
Abstract

An engineered ceramic matrix is provided to blunt and self-heal matrix cracks to reduce oxygen ingress into a fiber reinforced composite.

Claims (15)

1. A process for fabricating engineered ceramic matrix composites (E-CMCs) for high temperature applications, comprising:

combining and attrition milling a mixture of silicon carbide (SiC), silicon nitride, and a component selected from the group consisting of CrMoSi, CrMoSiGe, and CrMoSiY;

wet attrition milling the mixture using ethanol and silicon carbide grinding media, grinding the mixture into particles and homogenously mixing the mixture;

slurry preparing the mixture to generate an engineered CMC slurry;

infiltrating a preform with the engineered CMC slurry either under gravity, vacuum, or high pressure to allow particulates to spread uniformly within cavities of the preform; and

melt infiltrating the preform with CrSi 2 , CrSi, Cr 5 Si 3 , or any combination thereof to fill in voids left behind after the slurry infiltration.

2. The process of claim 1 , wherein the component is a chromium silicide alloy having a melting point less than 1550° C., to prevent the fibers from fusing and reacting with the melt.

3. The process of claim 1 , wherein the wet attrition milling of the mixture is between 48 and 64 hours.

4. The process of claim 1 , further comprising:

after the wet attrition milling of the mixture, decanting the ethanol, air drying the mixture and then placing the mixture in an oven to turn the mixture into a dry cake to be grounded using a mortar and pestle to a fine powder.

5. The process of claim 1 , wherein the slurry preparing of the engineered CMC comprises mixing powders in an aqueous alkaline ammonium hydroxide solution containing a dispersant.

6. The process of claim 1 , wherein the melt infiltrating of the preform comprises

melt infiltrating CrSi 2 , CrSi, Cr 5 Si 3 , or any combination into a slurry infiltrated SiC/SiC preform via external melt infiltration.

7. The process of claim 6 , wherein the melt infiltrated SiC/SiC preform comprises voids between fibers that are filled by molten CrSi2, CrSi, Cr 5 Si 3 , or any combination.

8. The process of claim 1 , wherein the mixture further comprises one or more self-healing additives selected from the group consisting of B 4 C, CrB 2 , Ge, Y, ZrB 2 , and ZrSiO 4 .

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 23, 2018
From: RAJ, SAI V., MR.
To: UNITED STATES GOVERNMENT ADMINISTRATOR OF NASA
Reel/Frame 045612/0110 →
Continuity (5)
Continuation In Part 15411375 · Jan 20, 2017
Continuation In Part 13905333 · May 30, 2013
Provisional Application 62449344 · Jan 23, 2017
Provisional Application 62281927 · Jan 22, 2016
Provisional Application 61654311 · Jun 1, 2012