Investigation into the effects of operating conditions and design parameters on the creep life of high pressure turbine blades in a stationary gas turbine engine

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dc.contributor.authorEshati, Samir
dc.contributor.authorAbu, Abdullahi Obonyegba
dc.contributor.authorLaskaridis, Panagiotis
dc.contributor.authorHaslam, Anthony
dc.date.accessioned2017-09-25T10:29:32Z
dc.date.available2017-09-25T10:29:32Z
dc.date.issued2011-09
dc.description.abstractA physics–based model is used to investigate the relationship between operating conditions and design parameters on the creep life of a stationary gas turbine high pressure turbine (HPT) blade. A performance model is used to size the blade and to determine its stresses. The effects of radial temperature distortion, turbine inlet temperature, ambient temperature and compressor degradation on creep life are then examined. The results show variations in creep life and failure location along the span of the blade enabling better informed design and maintenance decisions.en_UK
dc.identifier.citationEshati S, Abu A. Laskaridis P. Haslam A. (2011) Investigation into the effects of operating conditions and design parameters on the creep life of high pressure turbine blades in a stationary gas turbine engine. Mechanics and Mechanical Engineering, Volume 15, Issue 3, 2011, pp. 237-247en_UK
dc.identifier.issn1428-1511
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/12543
dc.language.isoenen_UK
dc.publisherTechnical University of Lodzen_UK
dc.subjectLifingen_UK
dc.subjectcreepen_UK
dc.subjectturbineen_UK
dc.subjectbladeen_UK
dc.subjectperformanceen_UK
dc.subjectdegradationen_UK
dc.titleInvestigation into the effects of operating conditions and design parameters on the creep life of high pressure turbine blades in a stationary gas turbine engineen_UK
dc.typeArticleen_UK

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