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
- Subject:
- 36 MATERIALS SCIENCE; 42 ENGINEERING
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}
}
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