AHP‐IFM Target: An Innovative Method to Define Reliability Target in an Aerospace Prototype Based on Analytic Hierarchy Process. (15th February 2017)

• Record Type: Journal Article
• Authors: Di Bona, Gianpaolo; Silvestri, Alessandro; Forcina, Antonio; Falcone, Domenico
• Is Part Of: Quality and reliability engineering international. Volume 33:Number 8(2017:Dec.)
• Page Start: 1731
• Page End: 1751
• Publication Date: 2017-02-15
• Subjects: reliability allocation -- FMECA -- FTA -- analytic hierarchy process -- multicriteria; Reliability (Engineering) -- Periodicals; Quality control -- Periodicals; High technology -- Periodicals; 620.00452
• DOI: 10.1002/qre.2140
• Languages: English
• ISSNs: 0748-8017

Abstract

Abstract: Reliability target definition is a crucial aspect of any reliability analysis. In literature, there are two types of analysis. The first one, called 'bottom‐up', goes back to the system's target using data of units through a fault tree analysis. Reliability data of components could be only partially available, particularly in the case of innovative systems. In the second type of analysis, called 'top‐down', starting from similar systems, the target of each unit is defined, by applying allocation techniques. Also, in this case, reliability data of similar systems might not be available, and the choice of the most appropriate technique could be tricky. The purpose of the present research is to combine the advantages of both usual approaches. The newly developed approach is based on the integrated factors method, whose values are adjusted trough a multicriteria method, the analytic hierarchy process, depending on the importance of each factor and each unit. The innovation of the proposed model consists in its dynamism, as most of the literature methods use constant weights for the factors involved in reliability allocation. No method takes into account the assignment of a different level of significance (weight) to different units of the system, simultaneously with the considered factors. The developed approach has been applied on an aerospace prototype system. The results show the goodness of the new method and its ability to overcome the problems noted in literature. Copyright © 2017 John Wiley & Sons, Ltd.