Stream Life Cycle Assessment Model for Aircraft Preliminary Design

The growing environmental public awareness and the consequential pressure on every industrial field has made environmental impact assessment increasingly important in the last few years. In this scope, the most established tool used in the specialized literature is the life cycle assessment. Applyin...

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Main Authors: Pietro Vivalda, Marco Fioriti
Format: Article
Language:English
Published: MDPI AG 2024-01-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/11/2/113
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author Pietro Vivalda
Marco Fioriti
author_facet Pietro Vivalda
Marco Fioriti
author_sort Pietro Vivalda
collection DOAJ
description The growing environmental public awareness and the consequential pressure on every industrial field has made environmental impact assessment increasingly important in the last few years. In this scope, the most established tool used in the specialized literature is the life cycle assessment. Applying this method to the life cycle of an aircraft requires it to be broken down into at least four phases: production, operation, maintenance and disposal. In the assessment, the evaluation of the environmental impact of fuel consumption can be performed linearly and has already been studied over many years, while calculating the impact of other life phases is more complicated, and it is still under study. This paper describes a simple and effective method developed to assess the environmental impact of an aircraft at a preliminary design stage and the implemented model that resulted from it. A detailed consideration of all life cycle phases is essential to serve as a reference for the ecological assessment of novel aircraft concepts. Thereby, the developed method is based on some parametric equations that take into account preliminary information, such as the mass breakdown, the technology used and some program considerations. The results obtained have been compared with those of the literature for verification and validation and have proved to be quite reliable. In fact, the comparison with known analyses, conducted on individual aircraft in a very precise manner, has showed that the proposed model is capable of giving results that fell within ±10% of the reference values. This is due to the broad generality of the model, which does not require a large number of specific data as a starting point to obtain reasonably reliable results for use during project development. In the near future, the use of this model can assist the design of aircraft architectures that comply with the European Green Deal of reducing net greenhouse gas emissions by at least 55% by 2030 and of having no net emissions of greenhouse gases by 2050.
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spelling doaj.art-60287d2a20924558b67704ac3c0c06992024-02-23T15:03:17ZengMDPI AGAerospace2226-43102024-01-0111211310.3390/aerospace11020113Stream Life Cycle Assessment Model for Aircraft Preliminary DesignPietro Vivalda0Marco Fioriti1Politecnico di Torino, 10129 Torino, ItalyPolitecnico di Torino, 10129 Torino, ItalyThe growing environmental public awareness and the consequential pressure on every industrial field has made environmental impact assessment increasingly important in the last few years. In this scope, the most established tool used in the specialized literature is the life cycle assessment. Applying this method to the life cycle of an aircraft requires it to be broken down into at least four phases: production, operation, maintenance and disposal. In the assessment, the evaluation of the environmental impact of fuel consumption can be performed linearly and has already been studied over many years, while calculating the impact of other life phases is more complicated, and it is still under study. This paper describes a simple and effective method developed to assess the environmental impact of an aircraft at a preliminary design stage and the implemented model that resulted from it. A detailed consideration of all life cycle phases is essential to serve as a reference for the ecological assessment of novel aircraft concepts. Thereby, the developed method is based on some parametric equations that take into account preliminary information, such as the mass breakdown, the technology used and some program considerations. The results obtained have been compared with those of the literature for verification and validation and have proved to be quite reliable. In fact, the comparison with known analyses, conducted on individual aircraft in a very precise manner, has showed that the proposed model is capable of giving results that fell within ±10% of the reference values. This is due to the broad generality of the model, which does not require a large number of specific data as a starting point to obtain reasonably reliable results for use during project development. In the near future, the use of this model can assist the design of aircraft architectures that comply with the European Green Deal of reducing net greenhouse gas emissions by at least 55% by 2030 and of having no net emissions of greenhouse gases by 2050.https://www.mdpi.com/2226-4310/11/2/113environmental impactlife cycle assessmentenvironmental project requirementsaviation industryaircraft preliminary design
spellingShingle Pietro Vivalda
Marco Fioriti
Stream Life Cycle Assessment Model for Aircraft Preliminary Design
Aerospace
environmental impact
life cycle assessment
environmental project requirements
aviation industry
aircraft preliminary design
title Stream Life Cycle Assessment Model for Aircraft Preliminary Design
title_full Stream Life Cycle Assessment Model for Aircraft Preliminary Design
title_fullStr Stream Life Cycle Assessment Model for Aircraft Preliminary Design
title_full_unstemmed Stream Life Cycle Assessment Model for Aircraft Preliminary Design
title_short Stream Life Cycle Assessment Model for Aircraft Preliminary Design
title_sort stream life cycle assessment model for aircraft preliminary design
topic environmental impact
life cycle assessment
environmental project requirements
aviation industry
aircraft preliminary design
url https://www.mdpi.com/2226-4310/11/2/113
work_keys_str_mv AT pietrovivalda streamlifecycleassessmentmodelforaircraftpreliminarydesign
AT marcofioriti streamlifecycleassessmentmodelforaircraftpreliminarydesign