In this work we present novel ultra-high-temperature ceramics matrix composites (UHTCMCs) for aerospace featuring optimized fiber/matrix interfaces and fibers distribution. The microstructures were produced by electrophoretic deposition of ZrB2 on unidirectional carbon fibers followed by slurry infiltration and consolidation by hot pressing. Different matrix and coating compositions were tested. The microstructure and properties are discussed. Typical values of flexural strength and fracture toughness are 330 MPa and 14 MPa m1/2, respectively.

Novel UD UHTCMCs produced by EPD and sintering

SFailla;L Zoli;P Galizia;D Sciti
2018

Abstract

In this work we present novel ultra-high-temperature ceramics matrix composites (UHTCMCs) for aerospace featuring optimized fiber/matrix interfaces and fibers distribution. The microstructures were produced by electrophoretic deposition of ZrB2 on unidirectional carbon fibers followed by slurry infiltration and consolidation by hot pressing. Different matrix and coating compositions were tested. The microstructure and properties are discussed. Typical values of flexural strength and fracture toughness are 330 MPa and 14 MPa m1/2, respectively.
2018
Istituto di Scienza, Tecnologia e Sostenibilità per lo Sviluppo dei Materiali Ceramici - ISSMC (ex ISTEC)
UHTCMC
Fracture toughness
Electrophoretic deposition
Zirconium diboride
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.14243/343431
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