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Conceptual Design S...
Conceptual Design Studies of “Boosted Turbofan” Configuration for short range
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- Hecken, Tobias (författare)
- Mälardalens högskola,German Aerospace Center, Goettingen, 37083, Germany
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- Zhao, Xin, 1986 (författare)
- Chalmers tekniska högskola,Chalmers University of Technology,German Aerospace Center, Goettingen, 37083, Germany
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- Iwanizki, Michael (författare)
- Deutsches Zentrums für Luft- und Raumfahrt (DLR),German Aerospace Center (DLR),German Aero Space Center, Braunschweig, 38108, Germany
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- Arzberger, Max (författare)
- Deutsches Zentrums für Luft- und Raumfahrt (DLR),German Aerospace Center (DLR),German Aero Space Center, Oberpfaffenhofen, 82234, Germany
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- Silberhorn, Daniel (författare)
- Deutsches Zentrums für Luft- und Raumfahrt (DLR),German Aerospace Center (DLR),German Aero Space Center, Hamburg, 21129, Germany
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- Plohr, Martin (författare)
- Deutsches Zentrums für Luft- und Raumfahrt (DLR),German Aerospace Center (DLR),German Aero Space Center, Koeln, 51147, Germany
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- Sahoo, Smruti (författare)
- Mälardalens högskola,Framtidens energi,University of Nottingham, Nottingham, NG9 2RD, United Kingdom
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- Kyprianidis, Konstantinos (författare)
- Mälardalens högskola,Framtidens energi
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- Sumsurooah, Sharmila (författare)
- University Of Nottingham
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- Valente, Giorgio (författare)
- University Of Nottingham,University of Nottingham, Nottingham, NG9 2RD, United Kingdom
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- Sielemann, Michael (författare)
- Modelon Deutschland GmbH, München, 80992, Germany
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- Coïc, Clément (författare)
- Modelon Deutschland GmbH, München, 80992, Germany,Technische Universität Berlin, Berlin, 10623, Germany
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- Bardenhagen, Andreas (författare)
- Technische Universität Berlin,Technische Universität Berlin, Berlin, 10623, Germany
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- Scheunemann, Annika (författare)
- Technische Universität Berlin,Technische Universität Berlin, Berlin, 10623, Germany
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- Jacobs, Claire (författare)
- Technische Universität Berlin
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(creator_code:org_t)
- 2020-01-05
- 2020
- Engelska.
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Ingår i: AIAA 2020-0506 Session: Hybrid Electric Aircraft Design Under Clean Sky 2 (LPA WP1.6.1.4). - Reston, Virginia : American Institute of Aeronautics and Astronautics.
- Relaterad länk:
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https://zenodo.org/r...
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https://research.cha...
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https://doi.org/10.2...
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https://urn.kb.se/re...
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Abstract
Ämnesord
Stäng
- This paper describes the current activities at the German Aerospace Center (DLR) and an associated consortium related to conceptual design studies of an aircraft configuration with hybrid electric propulsion for a typical short range commercial transport mission. The work is implemented in the scope of the European Clean Sky 2 program in the project “Advanced Engine and Aircraft Configurations” (ADEC) and “Turbo electric Aircraft Design Environment” (TRADE). The configuration analyzed incorporates parallel hybrid architecture consisting of gas turbines, electric machines, and batteries that adds electric power to the fans of the engines. A conceptual aircraft sizing workflow built in the DLR’s “Remote Component Environment” (RCE) incorporating tools of DLR that are based on semi-empirical and low level physics based methods. The TRADE consortium developed a simulation and optimization design platform with analysis models of higher fidelity for an aircraft with hybrid electric propulsion architecture. An implementation of the TRADE simulation and optimization design platform into the DLR’s RCE workflow by replacing the DLR models was carried out. The focus of this paper is on the quantitative evaluation of the “Boosted Turbofan” configuration utilizing the resulting workflow. In order to understand the cooperation between the DLR and TRADE consortium, a brief overview of the activities is given. Then the multi-disciplinary overall aircraft sizing workflow for hybrid electric aircraft built in RCE is shown. Hereafter, the simulation and optimization models of the TRADE design platform are described. Subsequently, an overview of the aircraft configuration considered in the scope of this work is given. The design space studies of the “Boosted Turbofan” configuration are presented. Finally, the deviations of the results between the workflows with and without the TRADE modules are discussed.
Ämnesord
- TEKNIK OCH TEKNOLOGIER -- Maskinteknik -- Rymd- och flygteknik (hsv//swe)
- ENGINEERING AND TECHNOLOGY -- Mechanical Engineering -- Aerospace Engineering (hsv//eng)
- TEKNIK OCH TEKNOLOGIER -- Maskinteknik (hsv//swe)
- ENGINEERING AND TECHNOLOGY -- Mechanical Engineering (hsv//eng)
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- Av författaren/redakt...
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Hecken, Tobias
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Zhao, Xin, 1986
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Iwanizki, Michae ...
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Arzberger, Max
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Silberhorn, Dani ...
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Plohr, Martin
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Sahoo, Smruti
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Kyprianidis, Kon ...
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Sumsurooah, Shar ...
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Valente, Giorgio
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Sielemann, Micha ...
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Coïc, Clément
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Bardenhagen, And ...
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Scheunemann, Ann ...
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Jacobs, Claire
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- Om ämnet
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- TEKNIK OCH TEKNOLOGIER
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TEKNIK OCH TEKNO ...
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och Maskinteknik
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och Rymd och flygtek ...
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- TEKNIK OCH TEKNOLOGIER
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TEKNIK OCH TEKNO ...
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och Maskinteknik
- Artiklar i publikationen
- AIAA 2020-0506 S ...
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AIAA Scitech 202 ...
- Av lärosätet
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Chalmers tekniska högskola
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Mälardalens universitet