2021
DOI: 10.1108/aeat-12-2020-0297
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An analytical model of the replacement costs of aircraft engine life-limited parts

Abstract: Purpose The purpose of this paper is to present novel recursive expressions for modelling the replacement costs of aircraft engine life-limited parts during shop visits to assist engine operators in both evaluating their decisions regarding the applied life-limited parts management strategies and tracking the replacement costs consistently throughout the life of the engine. Design/methodology/approach The replacement costs of aircraft engine life-limited parts are modelled analytically in this research, whic… Show more

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Cited by 5 publications
(2 citation statements)
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“…According to network reliability theory, physical components fail over time, resulting in a reduction or complete stop of flow in the system (Todinov, 2013; Ahmadi, 2016; Louit et al , 2011; Howlan, 1981; Fielding, 1980). The field of reliability engineering recommends using backup or spare components to minimize interruptions in flow due to failures (Kapur and Pecht, 2014; Elsayed, 2021; Schultz, 2004; Selçuk and Ağralı, 2013; Stojiljković et al , 2021). The number of backups or spare components in the network varies depending on expected reliability, cost, flow interruptions and other key metrics.…”
Section: Introductionmentioning
confidence: 99%
“…According to network reliability theory, physical components fail over time, resulting in a reduction or complete stop of flow in the system (Todinov, 2013; Ahmadi, 2016; Louit et al , 2011; Howlan, 1981; Fielding, 1980). The field of reliability engineering recommends using backup or spare components to minimize interruptions in flow due to failures (Kapur and Pecht, 2014; Elsayed, 2021; Schultz, 2004; Selçuk and Ağralı, 2013; Stojiljković et al , 2021). The number of backups or spare components in the network varies depending on expected reliability, cost, flow interruptions and other key metrics.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, reducing the weight of the engine block is the core problem of the R&D process (Pan et al , 2015; Carlucci et al , 2015). Some researchers began to study the development of aviation piston engines and engine life (Glowacki, 2018; Stojiljković et al , 2021). However, blindly changing the structure to reduce the weight will change the mechanical properties of engine parts, such as reducing the fatigue strength of key positions, reducing the overhaul interval and causing the vibration of the engine when working.…”
Section: Introductionmentioning
confidence: 99%