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Metallic and Ceramic Thin Film Thermocouples for Gas Turbine Engines

Temperatures of hot section components in today's gas turbine engines reach as high as 1,500 °C, making in situ monitoring of the severe temperature gradients within the engine rather difficult. Therefore, there is a need to develop instrumentation (i.e., thermocouples and strain gauges) for th...

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Detalles Bibliográficos
Autores principales: Tougas, Ian M., Amani, Matin, Gregory, Otto J.
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Molecular Diversity Preservation International (MDPI) 2013
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC3871097/
https://www.ncbi.nlm.nih.gov/pubmed/24217356
http://dx.doi.org/10.3390/s131115324