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An Architecture for On-Line Measurement of the Tip Clearance and Time of Arrival of a Bladed Disk of an Aircraft Engine

Safety and performance of the turbo-engine in an aircraft is directly affected by the health of its blades. In recent years, several improvements to the sensors have taken place to monitor the blades in a non-intrusive way. The parameters that are usually measured are the distance between the blade...

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Detalles Bibliográficos
Autores principales: Gil-García, José Miguel, Solís, Alejandro, Aranguren, Gerardo, Zubia, Joseba
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2017
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5677360/
https://www.ncbi.nlm.nih.gov/pubmed/28934105
http://dx.doi.org/10.3390/s17102162