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Civil aero-propulsion application: effect of thrust rating change on engine time on-wing

机译:民用航空推进应用:推力额定值变化对机上发动机时间的影响

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摘要

Engine fleet management has always been one of the most challenging tasks in any airline as it requires assuring reliability and cost effectiveness of engine operation at all times. The engine maintenance expenses are quite significant and accounts for about one third of the total aircraft maintenance costs. For all airlines with “Labour & Material” type of contractual arrangement with respective OEM / MRO provider, maximizing engine’s Time On-Wing (TOW) is extremely crucial to face lower maintenance costs, while at the same time abiding by governing airworthiness standards. Engine’s TOW is generally limited due to at least one of the following reasons: performance degradation reflected by lower Exhaust Gas Temperature (EGT) margin, hot section hardware life monitored by regular borescope inspections and Life Limited parts (LLP) expiry enforced by OEM or regulatory authority.After introducing relevant aero engine maintenance concepts and terminology, this thesis will serve to provide both qualitative and quantitative assessment of how certain operational factors of flight profile influence engine performance deterioration and maintenance costs. One such factor is the thrust rating of the engine. Higher thrust gives rise to higher internal temperatures, exposing engine hardware to greater mechanical and thermal stresses and therefore leading to faster rate of degradation and earlier engine removal.This thesis will be of interest to airlines having at least two different types of aircraft models in their fleet with different average flight profiles but powered by the same engine model with the required thrust variant. A particular engine may spend some time first on the aircraft that requires higher thrust rating before being switched to the aircraft that requires lower thrust rating or vice versa. This thesis will look into the feasibility of such an operational strategy through different aspects and discuss its effectiveness in retaining the engine performance for a longer time, thereby affecting the operating fuel costs and restoration costs per flying hour expected at the time of shop visit.
机译:发动机机队管理一直是任何航空公司中最具挑战性的任务之一,因为它需要始终确保发动机运行的可靠性和成本效益。发动机维护费用非常可观,约占飞机总维护成本的三分之一。对于所有与各自的OEM / MRO提供商签订了“劳力和材料”类型合同安排的航空公司,最大限度地提高发动机的机上随行时间(TOW)对于降低维修成本至关重要,同时还要遵守适航标准。发动机的TOW通常受以下至少一个原因的限制:排气温度(EGT)较低的缘故反映出性能下降,通过常规内窥镜检查监控的热段硬件寿命以及OEM或法规强制执行的限寿零件(LLP)到期在介绍了相关的航空发动机维护概念和术语之后,本论文将提供定性和定量评估,以评估某些飞行轮廓的运行因素如何影响发动机性能下降和维护成本。这样的因素之一是发动机的推力额定值。更高的推力会导致更高的内部温度,使发动机硬件承受更大的机械应力和热应力,从而导致更快的降级速度和更早地移除发动机。该论文对于在其飞机模型中至少有两种不同类型飞机的航空公司感兴趣具有不同平均飞行曲线但由相同发动机型号提供动力并具有所需推力变体的机队。特定的引擎可能先在需要更高推力额定值的飞机上花费一些时间,然后才切换到需要更低推力额定值的飞机上,反之亦然。本文将通过不同方面探讨这种操作策略的可行性,并讨论其在较长时间内保持发动机性能的有效性,从而影响到车间访问时预期的运行燃料成本和每飞行小时的恢复成本。

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    Shafi Syed Atif;

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  • 年度 2015
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  • 原文格式 PDF
  • 正文语种 en
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