Abstract:PurposeThe purpose of this paper is to focus on an optimizing maintenance policy with repair limit time for a new type of aircraft component, in which the lifetime is assumed to be an uncertain variable due to no historical operation data, and the repair time is a random variable that can be described by the experimental data.Design/methodology/approachTo describe this repair limit time policy over an infinite time horizon, an extended uncertain random renewal reward theorem is firstly proposed based on chance… Show more
“…Xie et al (2020) investigated the implications of cascading failures of a particular system, as well as the effects of safety barriers on preventing failures from occurring. Zhang et al (2022) studied optimizing aliment policy with fix-up limit time for a latest class of airliner unit with an estimated lifespan, and the outcomes of this study provides a helping guidance for airliner program and plays vital usage in engineering practice. Zhao et al (2017) developed some analytical replacement cost rates under two proposed policies considering random mission durations time, so as to avoid preventive replacement during mission period.…”
Among all reasonable dynamic replacement strategies, the age replacement strategy is the best. Furthermore, when compared to optimal replacement time of the other alternative formations, the optimal replacement time of system with series formation is shorter. For such reason, this paper compared the optimal replacement times obtained under the standard age replacement policy (SARP) with optimal replacement times obtained under some proposed two replacement policies (policy A and policy B) for some four multicomponent systems. Two numerical examples are provided for simple illustrations of the replacement policies under SARP, policy A and policy B, so as to select and apply the best replacement policy with respect to a particular system in making a projected precautionary replacement maintenance action of the system.
“…Xie et al (2020) investigated the implications of cascading failures of a particular system, as well as the effects of safety barriers on preventing failures from occurring. Zhang et al (2022) studied optimizing aliment policy with fix-up limit time for a latest class of airliner unit with an estimated lifespan, and the outcomes of this study provides a helping guidance for airliner program and plays vital usage in engineering practice. Zhao et al (2017) developed some analytical replacement cost rates under two proposed policies considering random mission durations time, so as to avoid preventive replacement during mission period.…”
Among all reasonable dynamic replacement strategies, the age replacement strategy is the best. Furthermore, when compared to optimal replacement time of the other alternative formations, the optimal replacement time of system with series formation is shorter. For such reason, this paper compared the optimal replacement times obtained under the standard age replacement policy (SARP) with optimal replacement times obtained under some proposed two replacement policies (policy A and policy B) for some four multicomponent systems. Two numerical examples are provided for simple illustrations of the replacement policies under SARP, policy A and policy B, so as to select and apply the best replacement policy with respect to a particular system in making a projected precautionary replacement maintenance action of the system.
This paper focus on a (N, T) preventive maintenance (PM) policy with lifetime reduction discount rate. In our consideration, the lifetime of component is assumed to be an uncertain variable due to the absence of historical operational data, an uncertain (N, T) PM model with the lifetime reduction in a certain proportion is proposed based on uncertain renewal process. Accordingly, the uncertain model, which minimizes the expected maintenance cost rate, is formulated to find the optimal replacement cycle length T∗ and the number N∗ of preventive maintenance. Finally, a numerical example with sensitivity analysis of parameters is provided to illustrate the proposed model, the results imply that the parameters of cost and lifetime can significantly affect the optimal solutions N∗ and T∗, which can provide a useful reference and guidance for aircraft maintenance decision.
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