Life cycle assessment of a regional hybridelectric aeroplane
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Författare
Typ
Examensarbete för masterexamen
Master's Thesis
Master's Thesis
Modellbyggare
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Sammanfattning
This thesis presents a life cycle assessment (LCA) of a hybrid electric aeroplane
based on the ES-30 currently under development by Heart Aerospace. The thesis
and the LCA aim to answer the following questions: (i) How large are the environmental
impacts of the hybrid-electric aeroplane?, (ii) Which part of the life cycle
has the largest environmental impact?, (iii) Where are the largest uncertainties in
the inventory data?, (iv) How would changes in the base-case assumptions alter the
overall results of the study?, and (v) Are the environmental impacts different from
those of a similar-sized aeroplane with a conventional propulsion system?
The LCA is performed with a cradle-to-grave perspective where the life cycle is
divided into production, use phase and end-of-life. The production is modelled
with help from published literature, experts at Heart Aerospace and datasets from
Ecoinvent 3.9.1. The use phase investigates different flight scenarios concerning
flight distance, type of fuel and electricity mixes for charging. The end-of-life only
includes dismantling and sorting of materials since the built-in cut-off approach in
the Ecoinvent 3.9.1 database was used to conduct the LCA.
The largest uncertainties lie in the aeroplane production since the actual ES-30 is
still under development with changes being made to the design and material choices
through the duration of this thesis. However, the results of the LCA indicate that
the use phase is the dominating phase for all impact categories included in this study.
Most of the impacts can be allocated to fuel production and combustion as well as
the production and use of batteries. By changing the fuel to alternative aviation
fuel, there are reduction potentials in mainly climate change impact and particulate
matter formation. Although the future role of alternative aviation fuels is uncertain
and may lead to negative impact in other impact categories. Still in the base case
with fossil kerosene and Swedish electricity mix, the ES-30 is environmentally beneficial
compared to a similar-sized conventional aeroplane. The one impact category
where the ES-30 most probably will perform worse than a conventional reference
aeroplane is mineral resource scarcity due to the use of rare metals for batteries and
power electronics
Beskrivning
Ämne/nyckelord
Life cycle assessment, LCA, Aeroplane, Aviation, Hybrid-electric, Climate change, Lithium-ion battery, Turboprop, Electric motor, Inverter