Thrust rebalance to extend engine time on-wing with consideration of engine degradation and creep life consumption

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dc.contributor.authorda Mota Chiavegatto, Rafael
dc.contributor.authorLi, Yi-Guang
dc.date.accessioned2023-10-26T13:18:35Z
dc.date.available2023-10-26T13:18:35Z
dc.date.issued2023-09-28
dc.description.abstractOver the years, airlines have consistently attempted to lower their operational costs and improve aircraft availability by applying various technologies. Engine maintenance expenses are one of the most substantial costs for aircraft operations, accounting for around 30% of overall aircraft operational costs. So, maximizing aircraft time between overhaul is crucial to lowering the costs. The engine time on-wing is often limited by the expiration of Life Limiting Parts, performance deterioration, maintenance schedule, etc. This paper presents a novel method of rebalancing the thrust of engines of an aircraft to maximize the time between overhauls of the aircraft considering the performance degradation and creep life consumption of the engines. The method is applied to a model aircraft fitted with two model engines similar to GT90 115B to test the feasibility of the method with one engine degraded and the other engine undegraded. The obtained results demonstrate that for the aircraft flying between London and Toronto with 5,000 nominal flight cycles given to the engines, the time on-wing of the degraded engine could drop from 5,000 to 2,460 flight days due to its HP turbine degradation (1% efficiency degradation 3% flow capacity degradation), causing the same level of drop of time between overhauls of the aircraft. The time on-wing of the degraded engine could increase from 2,460 flight days without thrust rebalance to 3,410 flight days with thrust rebalance, i. e. around 38.6% potential improvement for the time between overhauls of the aircraft at the expenses of increased creep life consumption rate of the clean engine. The proposed method could be applied to other aircraft and engines.en_UK
dc.identifier.citationda Mota Chiavegatto R, Li Y-G. (2023) Thrust rebalance to extend engine time on-wing with consideration of engine degradation and creep life consumption. In: ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition, 26-30 June 2023, Boston, MA, USAen_UK
dc.identifier.isbn978-0-7918-8693-9
dc.identifier.urihttps://doi.org/10.1115/GT2023-102238
dc.identifier.urihttps://asmedigitalcollection.asme.org/GT/proceedings-abstract/GT2023/86939/V001T01A021/1167762
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/20456
dc.language.isoenen_UK
dc.publisherAmerican Society of Mechanical Engineers (ASME)en_UK
dc.rightsAttribution 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/*
dc.subjectgas turbineen_UK
dc.subjectengineen_UK
dc.subjectthrust rebalanceen_UK
dc.subjectcreep lifeen_UK
dc.subjectperformance degradationen_UK
dc.subjectthrust balance factoren_UK
dc.titleThrust rebalance to extend engine time on-wing with consideration of engine degradation and creep life consumptionen_UK
dc.typeConference paperen_UK

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