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Title: Formulations for engineered ceramic matrix composites for high temperature applications

Abstract

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

Inventors:
Issue Date:
Research Org.:
National Aeronautics and Space Administration (NASA), Washington, DC (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1650915
Patent Number(s):
10654756
Application Number:
15/875,283
Assignee:
The United States of America as represented by the Administrator of the National Aeronautics and Space Administration (Washington, DC)
Patent Classifications (CPCs):
C - CHEMISTRY C04 - CEMENTS C04B - LIME, MAGNESIA
Resource Type:
Patent
Resource Relation:
Patent File Date: 01/19/2018
Country of Publication:
United States
Language:
English

Citation Formats

Raj, Sai V. Formulations for engineered ceramic matrix composites for high temperature applications. United States: N. p., 2020. Web.
Raj, Sai V. Formulations for engineered ceramic matrix composites for high temperature applications. United States.
Raj, Sai V. Tue . "Formulations for engineered ceramic matrix composites for high temperature applications". United States. https://www.osti.gov/servlets/purl/1650915.
@article{osti_1650915,
title = {Formulations for engineered ceramic matrix composites for high temperature applications},
author = {Raj, Sai V.},
abstractNote = {An engineered ceramic matrix is provided to blunt and self-heal matrix cracks to reduce oxygen ingress into a fiber reinforced composite.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2020},
month = {5}
}

Patent:

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Works referenced in this record:

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