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Study on a Fault Mitigation Scheme for Rub-Impact of an Aero-Engine Based on NiTi Wires

The aim of this study was to solve the frequently occurring rotor-stator rub-impact fault in aero-engines without causing a significant reduction in efficiency. We proposed a fault mitigation scheme, using shape memory alloy (SMA) wire, whereby the tip clearance between the rotor and the stator is a...

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Detalles Bibliográficos
Autores principales: Pan, Qiang, He, Tian, Liu, Wendong, Liu, Xiaofeng, Chen, Haibing
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8914907/
https://www.ncbi.nlm.nih.gov/pubmed/35270945
http://dx.doi.org/10.3390/s22051796