Energy flexibility in aerospace manufacturing: the case of low carbon intensity production

Date published

2024-05-17

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Elsevier

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Article

ISSN

0278-6125

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Citation

Haddad Y, De Bonneval EG, Afy-Shararah M, et al., (2024) Energy flexibility in aerospace manufacturing: the case of low carbon intensity production. Journal of Manufacturing Systems. Volume 74, June 2024, pp. 812-825

Abstract

In this paper, the prospects of energy flexibility in mitigating the environmental impact of aerospace manufacturing are explored. In collaboration with a UK-based aerospace manufacturing enterprise, demand response, in particular production time, is explored under different stochastic scenarios. This is done through a decision-support framework that consists of a stochastic discrete-event simulation model that tests different scenarios under a full factorial design of experiments framework. The simulation model tests various improvement strategies pertaining to prioritisation rules, production start-up rules, and operating hours. The model aids in scheduling energy-intensive processes, so the time of performing such processes can coincide with times of the day when the energy’s carbon intensity is at its lowest. The use case constitutes a family of aluminium structural aerospace components that are characterised by high production rate. Results demonstrate promising potential of the proposed approach, with the best-case scenario resulting in a 7% reduction in CO2e emissions. Analysis of the results demonstrate that operational decisions that do not require infrastructural changes or capital expenditures can contribute favourably to achieving net-zero targets. This research offers useful insights on leveraging operational short-term decisions to meet the aerospace manufacturing’s sector decarbonisation targets.

Description

Software Description

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Github

Keywords

Sustainable manufacturing, Energy flexibility, Demand response, Aerospace manufacturing, Discrete-event simulation

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Attribution 4.0 International

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This work was carried out as part of the Metallic Aerospace Structures Technologies for Eco-social Returns (MASTER) project, under UKRI ATI grant number 103040.