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Thesis

Oxide based ceramic matrix composites for high temperature aerospace sealing applications

Abstract:

This thesis looks at the viability of using oxide based ceramic matrix composites for high temperature gas turbine sealing applications. Two material systems namely Nextel312/SiOC, Nextel 312 fibre with SiOC matrix, and Nextel720/Alumina, Nextel 720 fibre with alumina matrix, were studied in detail and modified in order to produce CMC variants that could perform adequately as seals materials.

Nextel 312/SiCO composites were optimised for sealing applications at service temperature...

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Institution:
University of Oxford
Division:
MPLS
Department:
Materials
Sub department:
Materials
Oxford college:
Linacre College
Role:
Author

Contributors

Role:
Supervisor
ORCID:
0000-0001-6120-9826
Role:
Supervisor



Type of award:
DPhil
Level of award:
Doctoral
Awarding institution:
University of Oxford

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