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dc.rights.licenseopenen_US
dc.relation.isnodoubledc6cde57-55e7-4a72-95f8-22943280b7c9*
hal.structure.identifierLaboratoire des Composites Thermostructuraux [LCTS]
dc.contributor.authorSIMON, Coraline
hal.structure.identifierLaboratoire des Composites Thermostructuraux [LCTS]
dc.contributor.authorREBILLAT, Francis
hal.structure.identifierLaboratoire des Composites Thermostructuraux [LCTS]
dc.contributor.authorCAMUS, Gérald
dc.date.accessioned2021-07-21T08:56:43Z
dc.date.available2021-07-21T08:56:43Z
dc.date.issued2017-06-01
dc.identifier.issn1359-6454en_US
dc.identifier.urioai:crossref.org:10.1016/j.actamat.2017.04.070
dc.identifier.urioadoi:https://hal.archives-ouvertes.fr/hal-01629867/document
dc.identifier.urioadoi:https://hal.archives-ouvertes.fr/hal-01629867/file/Simon2017_Acta2_Publi%20Electrical%20monitoring%20oxidizing%20conditions_HAL.pdf
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/110138
dc.description.abstractEnThe introduction of Ceramic Matrix Composites parts in civil aeronautics requires a thorough understanding of their evolution under the oxidizing environments present within the engines. In this respect, a SiCf/PyC/[Si-B-C]m material has been tested in fatigue at 450 °C and 100 MPa (which is a typical stress during take-off) under two types of environmental conditions: ambient air, and moist air with an imposed water pressure of 10 kPa. Static fatigue and cyclic fatigue at a frequency of 1 Hz were both performed with these two conditions. As expected, the additional presence of moisture contributes to increase the degradation of the mechanical properties of the material, leading to shorter lifetimes and higher increases in electrical resistivity. It is shown that the pyrocarbon interphases are the main electrical conductors in this material: the electrical resistance can therefore be an accurate indicator of the damage state of these interphases, which are sensitive to the oxidizing environment. The global resistance increase presents two distinct phases of evolution in the four tests performed, with a transition around 35–40% of the time to failure. A model is proposed to account for this global resistance change, which proves to be in good agreement with experimental results. Moreover, the evolution of the electrical resistivity during the interposed unload-reload cycles can give key information about the state of the fiber/matrix interfaces which are critical for mechanical properties. Finally, electrical resistance monitoring seems to provide information on the damage state of the material complementary to acoustic emission results, allowing an unprecedented assessment of the evolution of the interphases state during ageing under oxidizing environments.
dc.language.isoENen_US
dc.rightsAttribution 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by/3.0/us/*
dc.sourcecrossref
dc.sourceoadoi_repo
dc.subject.enCeramic Matrix Composites (CMCs)
dc.subject.enElectrical resistivity
dc.subject.enThermo-mechanical ageing
dc.subject.enOxidizing environment
dc.title.enElectrical resistivity monitoring of a SiC/[Si-B-C] composite under oxidizing environments
dc.typeArticle de revueen_US
dc.identifier.doi10.1016/j.actamat.2017.04.070en_US
dc.subject.halChimie/Matériauxen_US
bordeaux.journalActa Materialiaen_US
bordeaux.page586-597en_US
bordeaux.volume132en_US
bordeaux.hal.laboratoriesLaboratoire des Composites Thermo Structuraux (LCTS) - UMR 5801en_US
bordeaux.institutionUniversité de Bordeauxen_US
bordeaux.institutionCNRSen_US
bordeaux.institutionCEAen_US
bordeaux.peerReviewedouien_US
bordeaux.inpressnonen_US
bordeaux.import.sourcedissemin
hal.identifierhal-01629867
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