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Sökning: onr:"swepub:oai:DiVA.org:mdh-46551" > A framework for opt...

LIBRIS Formathandbok  (Information om MARC21)
FältnamnIndikatorerMetadata
00006428naa a2200853 4500
001oai:DiVA.org:mdh-46551
003SwePub
008191216s2019 | |||||||||||000 ||eng|
009oai:research.chalmers.se:51d7683c-5a6c-4228-a2dc-d601bc328788
0247 a https://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-465512 URI
0247 a https://doi.org/10.1115/GT2019-913352 DOI
0247 a https://research.chalmers.se/publication/5209742 URI
040 a (SwePub)mdhd (SwePub)cth
041 a engb eng
042 9 SwePub
072 7a ref2 swepub-contenttype
072 7a kon2 swepub-publicationtype
1001 a Xin, Zhaou Mälardalens högskola,Framtidens energi4 aut0 (Swepub:cth)zxin
2451 0a A framework for optimization of hybrid aircraft
264 1b American Society of Mechanical Engineers (ASME),c 2019
338 a electronic2 rdacarrier
520 a To achieve the goals of substantial improvements in efficiency and emissions set by Flightpath 2050, fundamentally different concepts are required. As one of the most promising solutions, electrification of the aircraft primary propulsion is currently a prime focus of research and development. Unconventional propulsion sub-systems, mainly the electrical power system, associated thermal management system and transmission system, provide a variety of options for integration in the existing propulsion systems. Different combinations of the gas turbine and the unconventional propulsion sub-systems introduce different configurations and operation control strategies. The trade-off between the use of the two energy sources, jet fuel and electrical energy, is primarily a result of the trade-offs between efficiencies and sizing characteristics of these sub-systems. The aircraft structure and performance are the final carrier of these trade-offs. Hence, full design space exploration of various hybrid derivatives requires global investigation of the entire aircraft considering these key propulsion sub-systems and the aircraft structure and performance, as well as their interactions. This paper presents a recent contribution of the development for a physics-based simulation and optimization platform for hybrid electric aircraft conceptual design. Modeling of each subsystem and the aircraft structure are described as well as the aircraft performance modeling and integration technique. With a focus on the key propulsion sub-systems, aircraft structure and performance that interfaces with existing conceptual design frameworks, this platform aims at full design space exploration of various hybrid concepts at a low TRL level.
650 7a TEKNIK OCH TEKNOLOGIERx Maskinteknikx Energiteknik0 (SwePub)203042 hsv//swe
650 7a ENGINEERING AND TECHNOLOGYx Mechanical Engineeringx Energy Engineering0 (SwePub)203042 hsv//eng
650 7a TEKNIK OCH TEKNOLOGIERx Maskinteknikx Rymd- och flygteknik0 (SwePub)203022 hsv//swe
650 7a ENGINEERING AND TECHNOLOGYx Mechanical Engineeringx Aerospace Engineering0 (SwePub)203022 hsv//eng
650 7a TEKNIK OCH TEKNOLOGIERx Naturresursteknikx Energisystem0 (SwePub)207022 hsv//swe
650 7a ENGINEERING AND TECHNOLOGYx Environmental Engineeringx Energy Systems0 (SwePub)207022 hsv//eng
650 7a TEKNIK OCH TEKNOLOGIERx Elektroteknik och elektronikx Annan elektroteknik och elektronik0 (SwePub)202992 hsv//swe
650 7a ENGINEERING AND TECHNOLOGYx Electrical Engineering, Electronic Engineering, Information Engineeringx Other Electrical Engineering, Electronic Engineering, Information Engineering0 (SwePub)202992 hsv//eng
653 a Aircraft manufacture
653 a Airframes
653 a Alternative fuels
653 a Conceptual design
653 a Economic and social effects
653 a Electric power transmission
653 a Gas turbines
653 a Hydrogen fuels
653 a Jet aircraft
653 a Petroleum prospecting
653 a Power generation
653 a Propulsion
653 a Rankine cycle
653 a Simulation platform
653 a Aircraft performance
653 a Design space exploration
653 a Electrical power system
653 a Integration techniques
653 a Physics-based Simulation
653 a Thermal management systems
653 a Transmission systems
653 a Unconventional propulsions
653 a Vehicle performance
7001 a Sahoo, Smrutiu Mälardalens högskola,Framtidens energi,University of Nottingham, Nottingham, United Kingdom4 aut0 (Swepub:mdh)sso01
7001 a Kyprianidis, Konstantinosu Mälardalens högskola,Framtidens energi,Modelon Deutschland GmbH, Munich, Germany4 aut0 (Swepub:mdh)kks01
7001 a Sumsurooah, S.u University of Nottingham, Nottingham, United Kingdom,University Of Nottingham4 aut
7001 a Valente, G.u University of Nottingham, Nottingham, United Kingdom,University Of Nottingham4 aut
7001 a Rashed, M.u University of Nottingham, Nottingham, United Kingdom,University Of Nottingham4 aut
7001 a Vakil, G.u University of Nottingham, Nottingham, United Kingdom,University Of Nottingham4 aut
7001 a Hill, C. I.u University of Nottingham, Nottingham, United Kingdom,University Of Nottingham4 aut
7001 a Jacob, C.u Technische Universität Berlin, Berlin, Germany4 aut
7001 a Gobbin, A.u Technische Universität Berlin, Berlin, Germany4 aut
7001 a Bardenhagen, A.u Technische Universität Berlin, Berlin, Germany4 aut
7001 a Prölss, K.u Modelon Deutschland GmbH, Munich, Germany4 aut
7001 a Sielemann, M.u Modelon Deutschland GmbH, Munich, Germany4 aut
7001 a Rantzer, J.u Modelon AB, Lund, Sweden4 aut
7001 a Ekstedt, E.u Modelon AB, Lund, Sweden4 aut
7102 a Mälardalens högskolab Framtidens energi4 org
7730 t Proceedings of the ASME Turbo Expod : American Society of Mechanical Engineers (ASME)g 3z 9780791858608
7730 t ASME Turbo Expo 2019: Turbomachinery Technical Conference and Expositiond : American Society of Mechanical Engineers (ASME)g 3q 3
8564 u https://mdh.diva-portal.org/smash/get/diva2:1379262/FULLTEXT01.pdfx primaryx Raw objecty fulltext:print
8564 8u https://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-46551
8564 8u https://doi.org/10.1115/GT2019-91335
8564 8u https://research.chalmers.se/publication/520974

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