An integrated aerospace requirement setting and risk analysis tool for life cycle cost reduction and system design improvement

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dc.contributor.author Estébanez, L. Ruiz
dc.contributor.author Shehab, Essam
dc.contributor.author Sydor, Piotr
dc.contributor.author Mackley, Tim
dc.contributor.author John, Philip
dc.contributor.author Harrison, A.
dc.date.accessioned 2016-08-25T17:38:35Z
dc.date.available 2016-08-25T17:38:35Z
dc.date.issued 2015-10-27
dc.identifier.citation An integrated aerospace requirement setting and risk analysis tool for life cycle cost reduction and system design improvement en_UK
dc.identifier.issn 2212-8271
dc.identifier.uri http://dx.doi.org/10.1016/j.procir.2015.08.080
dc.identifier.uri https://dspace.lib.cranfield.ac.uk/handle/1826/10456
dc.description.abstract In the early conceptual stage of the service orientated model, decisions regarding the design of a new technical product are largely influenced by Service Requirements. Those decisions, therefore, have to merge both technical and business aspects to obtain desired product reliability and reduced Whole Life Cost (WLC). It is, therefore, critical at that phase to define the risk of potential noncompliance of Service Requirements in order to ensure the right design choices; as these decisions have a large impact on the overall product and service development. This paper presents outcome of research project to investigate different approaches used by companies to analyse Service Requirements to achieve reduced Life Cycle Cost (LCC). Analysis using Weibull distribution and Monte Carlo principle have been proposed here; based on the conducted literature review these are considered as the most widely used techniques in product reliability studies. Based on those techniques, a methodology and its software tool for risk evaluation of failure to deliver a new product against Service Requirements are presented in this paper. This is part of the on-going research project which, apart from analysing the gap between the current Service Requirements achievements and the design targets for a new aircraft engine, it also facilitates an optimisation of those requirements at the minimum risk of nonconformity. en_UK
dc.language.iso en en_UK
dc.publisher Elsevier en_UK
dc.rights Attribution 4.0 International (CC BY 4.0) You are free to: Share — copy and redistribute the material in any medium or format, Adapt — remix, transform, and build upon the material for any purpose, even commercially. The licensor cannot revoke these freedoms as long as you follow the license terms. Under the following terms: Attribution — You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use. Information: No additional restrictions — You may not apply legal terms or technological measures that legally restrict others from doing anything the license permits.
dc.subject Service Requirements en_UK
dc.subject Risk Assessment en_UK
dc.subject Weibull Distribution en_UK
dc.subject Aircraft's Engines en_UK
dc.subject DMTrade en_UK
dc.title An integrated aerospace requirement setting and risk analysis tool for life cycle cost reduction and system design improvement en_UK
dc.type Article en_UK


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