A case study of vibration fault diagnosis applied at Rolls-Royce T-56 turboprop engine

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dc.contributor.author Skliros, Christos
dc.date.accessioned 2020-02-11T20:14:07Z
dc.date.available 2020-02-11T20:14:07Z
dc.date.issued 2020-01-22
dc.identifier.citation Skliros C (2020) A case study of vibration fault diagnosis applied at Rolls-Royce T-56 turboprop engine. Aviation, Volume 23, Issue 3, pp. 78-82. en_UK
dc.identifier.issn 1648-7788
dc.identifier.uri https://doi.org/10.3846/aviation.2019.11900
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/15121
dc.description.abstract Gas turbine engines include a plethora of rotating modules, and each module consists of numerous components. A component’s mechanical fault can result in excessive engine vibrations. Identification of the root cause of a vibration fault is a significant challenge for both engine manufacturers and operators. This paper presents a case study of vibration fault detection and isolation applied at a Rolls-Royce T-56 turboprop engine. In this paper, the end-to-end fault diagnosis process from starting system faults to the isolation of the engine’s shaft that caused excessive vibrations is described. This work contributes to enhancing the understanding of turboprop engine behaviour under vibration conditions and highlights the merit of combing information from technical logs, maintenance manuals and engineering judgment in successful fault diagnosis. en_UK
dc.language.iso en en_UK
dc.publisher Taylor & Francis en_UK
dc.rights Attribution 4.0 International *
dc.rights.uri http://creativecommons.org/licenses/by/4.0/ *
dc.subject Gas turbines en_UK
dc.subject Vibration en_UK
dc.subject Diagnostics en_UK
dc.subject Condition-based maintenance en_UK
dc.subject Fault detection en_UK
dc.subject Fault isolation en_UK
dc.title A case study of vibration fault diagnosis applied at Rolls-Royce T-56 turboprop engine en_UK
dc.type Article en_UK


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