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Tip-Clearance Measurement in the First Stage of the Compressor of an Aircraft Engine
In this article, we report the design of a reflective intensity-modulated optical fiber sensor for blade tip-clearance measurement, and the experimental results for the first stage of a compressor of an aircraft engine operating in real conditions. The tests were performed in a ground test cell, whe...
| Autores principales: | , , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
MDPI
2016
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| Materias: | |
| Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5134556/ https://www.ncbi.nlm.nih.gov/pubmed/27845709 http://dx.doi.org/10.3390/s16111897 |