Design Decisions for a Powertrain Combination of Electric Motor and Propeller for an Electric Aircraft

RJ Keuter, B Kirsch, J Friedrichs, B Ponick - IEEE Access, 2023 - ieeexplore.ieee.org
For the sizing of an electric motor, the diameter and length of the installation space are
important parameters that significantly influence and limit the characteristics of the electric …

The impact of multi-stack fuel cell configurations on electrical architecture for a Zero Emission Regional aircraft

B Zaghari, T Zhou, HB Enalou, E Pontika… - AIAA SCITECH 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-1593. vid All-electric aircraft can
eliminate greenhouse gas emissions during aircraft mission, but the low predicted energy …

Technical status and development of electric vertical take-off and landing aircraft

D Jinghui - Acta Aeronautica et Astronautica Sinica, 2024 - sciopen.com
The development of electric Vertical Take-off and Landing (eVTOL) aircraft is greatly
promoted for the advances in battery and motor technologies and the application of …

Integrated mission performance analysis of novel propulsion systems: Analysis of a fuel cell regional aircraft retrofit

E Pontika, B Zaghari, T Zhou, HB Enalou… - AIAA SCITECH 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0840. vid This paper presents the
development and application of an integrated, higher-fidelity framework developed within …

Conceptual estimation of the noise reduction potential of electrified aircraft engines

TF Geyer, L Enghardt - Acta Acustica, 2023 - acta-acustica.edpsciences.org
The advent of electrified propulsion systems for civil aircraft promises not only notable
reductions of CO 2 and NO x emissions, but also of perceived noise. In an attempt to …

[PDF][PDF] Assessment of Aeroacoustic Optimisation Schemes for a Tilt-Propeller Application in Hover and Cruise

O Bergmann, D Frey - 49th European Rotorcraft Forum, 2023 - researchgate.net
Balancing propeller optimisation between cruise and hover conditions is a key challenge in
eco-friendly aircraft design. This paper presents a novel multidisciplinary propeller …

Mission-Oriented Electrified Aircraft Propulsion System Design and Verification Using Model-Based Systems Engineering

Z Hu, J Chen, J Lu, H Zhang - … of Engineering for …, 2024 - asmedigitalcollection.asme.org
The concept of electrified aircraft propulsion (EAP) has garnered substantial attention and
investigation due to its potential for mitigating fuel consumption, emissions, and noise …

Set-based design space exploration to investigate the effect of energy storage durability on the energy management strategy of a hybrid-electric aircraft

A Spinelli, GP Krupa, T Kipouros - AIAA SCITECH 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-0837. vid To investigate the key
enabling technologies for hybrid-electric regional aircraft, several assumptions about the …

Application of Model-Based Systems Engineering for the Integration of Electric Engines in Electrified Aircraft

A Kiran, B Zaghari, T Kipouros… - Journal of Physics …, 2023 - iopscience.iop.org
The objective of green, carbon-neutral flights is propelling the innovation of newer
propulsion systems. With this increased development of an interdisciplinary form of …

Take-off performance of a single engine battery-electric aeroplane

GB Gratton, T Delaney, B Zaghari… - The Aeronautical …, 2024 - cambridge.org
This paper investigates the take-off performance of a single engine battery-electric
aeroplane, using the example of the 300kg Sherwood eKub. It shows analysis of take-off …