elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Application of a turbo electric aircraft design environment for boosted turbofan aircraft configuration studies

Hecken, Tobias and Iwanizki, Michael and Arzberger, Max Josef and Silberhorn, Daniel and Plohr, Martin (2020) Application of a turbo electric aircraft design environment for boosted turbofan aircraft configuration studies. DLRK 2020 - Deutscher Luft- und Raumfahrtkongress, 01.-03. Sep. 2020, Online.

[img] PDF - Only accessible within DLR
1MB

Abstract

The current activities at the German Aerospace Center (DLR) and the associated consortium related to conceptual design studies of a Boosted Turbo fan configuration for a typical short range commission are presented. The Boosted Turbofan incorporates parallel hybrid architecture consisting of gas turbine, electric machines and batteries that add electric power to the fans of the engines. Furthermore, even though the fuel is substituted by electrical energy -at the cost of higher battery mass- the airframe of the aircraft is not notably impacted by the HEP system. Hence, it is a reasonable step towards hybrid electric aircraft due to less development risk. These current conceptual aircraft design activities regarding hybrid electric propulsion are organized within the scope of the project “Advanced Engine and Aircraft Configurations” (ADEC) of Clean Sky 2 at the DLR and the “Turbo electric Aircraft Design Environment” (TRADE) consortium consisting of the University of Nottingham, University of Märladalen, Technische Universität Berlin and coordinator Modelon Deutschland GmbH also part of Clean Sky 2. The DLR developed a conceptual aircraft sizing workflow built in the DLR’s “Remote Component Environment” (RCE) incorporating tools that are based on semi-empirical and low level physics based methods to evaluate hybrid electric aircraft. In contrast, the TRADE consortium developed a simulation and optimization design platform with physics-based models of higher fidelity for the analysis and optimization of individual systems and structural components. In contrast to ADEC, no overall aircraft design (OAD) is performed. Their optimization and assessment is based on an A320-like aircraft with a fixed airframe. There is interest to integrate the high-fidelity models into the DLR’s overall aircraft sizing workflow.

Item URL in elib:https://elib.dlr.de/137268/
Document Type:Conference or Workshop Item (Speech)
Title:Application of a turbo electric aircraft design environment for boosted turbofan aircraft configuration studies
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Hecken, TobiasTobias.Hecken (at) dlr.deUNSPECIFIED
Iwanizki, MichaelMichael.Iwanizki (at) dlr.deUNSPECIFIED
Arzberger, Max JosefMax.Arzberger (at) dlr.deUNSPECIFIED
Silberhorn, DanielDaniel.Silberhorn (at) dlr.deUNSPECIFIED
Plohr, MartinMartin.Plohr (at) dlr.dehttps://orcid.org/0000-0002-6165-0838
Date:3 September 2020
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:conceptual aircraft design, overall aircraft design, hybrid electric propulsion, boosted turbofan, Clean Sky, ADEC, TRADE
Event Title:DLRK 2020 - Deutscher Luft- und Raumfahrtkongress
Event Location:Online
Event Type:national Conference
Event Dates:01.-03. Sep. 2020
Organizer:DGLR - Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal Oberath e.V.
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Concepts and Integration (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Institute for Aerodynamics and Flow Technology > Transport Aircraft
Institute of System Dynamics and Control > Aircraft System Dynamics
Institute of Propulsion Technology > Engine
Institute of System Architectures in Aeronautics > Aircraft Design and System Integration
Deposited By: Hecken, Tobias
Deposited On:09 Nov 2020 07:42
Last Modified:27 Jan 2021 15:55

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.