Please use this identifier to cite or link to this item: http://dx.doi.org/10.14279/depositonce-11470
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Main Title: Structure-system design interdependencies of hybrid-electric aircraft during conceptual design phase
Author(s): Scheunemann, Annika
Jacob, Claire
Bardenhagen, Andreas
Hoffmann, David
Würfel, Philipp
Type: Conference Object
Language Code: en
Abstract: The electro-hybridization of aviation might bring the strongly needed decrease of fuel emissions. As the electrification cannot be evaluated with con-ventional methods, the TuRbo electric Aircraft Design Environment (TRADE) was funded by the EU Clean Sky JTI initiative. The consortium aims to develop a multidisciplinary design platform in order to assess the potential of hybridization on the basis of two sample aircraft. Reference [4] gives a description and evaluation of configuration 1. Configuration 2 is described in this paper. An enhanced wing structure mass calculation based on a proposal by Torenbeek is introduced and assessed. Parametric studies outline the effects of enlarged electric power and thermal systems.
URI: https://depositonce.tu-berlin.de/handle/11303/12663
http://dx.doi.org/10.14279/depositonce-11470
Issue Date: Feb-2020
Date Available: 23-Feb-2021
DDC Class: 600 Technik, Technologie
Subject(s): hybrid aircraft
aircraft structures
aviation
Sponsor/Funder: EC/H2020/755458/EU/Turbo electRic Aircraft Design Environment (TRADE)/TRADE
License: http://rightsstatements.org/vocab/InC/1.0/
Proceedings Title: Aerospace Europe Conference 2020
Publisher: Council of European Aerospace Societies
Publisher Place: Brüssel
Article Number: 00618
Appears in Collections:FG Luftfahrzeugbau und Leichtbau » Publications

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