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

A framework for optimization of hybrid aircraft

Xin, Zhao (författare)
Mälardalens högskola,Framtidens energi
Sahoo, Smruti (författare)
Mälardalens högskola,Framtidens energi,University of Nottingham, Nottingham, United Kingdom
Kyprianidis, Konstantinos (författare)
Mälardalens högskola,Framtidens energi,Modelon Deutschland GmbH, Munich, Germany
visa fler...
Sumsurooah, S. (författare)
University of Nottingham, Nottingham, United Kingdom,University Of Nottingham
Valente, G. (författare)
University of Nottingham, Nottingham, United Kingdom,University Of Nottingham
Rashed, M. (författare)
University of Nottingham, Nottingham, United Kingdom,University Of Nottingham
Vakil, G. (författare)
University of Nottingham, Nottingham, United Kingdom,University Of Nottingham
Hill, C. I. (författare)
University of Nottingham, Nottingham, United Kingdom,University Of Nottingham
Jacob, C. (författare)
Technische Universität Berlin, Berlin, Germany
Gobbin, A. (författare)
Technische Universität Berlin, Berlin, Germany
Bardenhagen, A. (författare)
Technische Universität Berlin, Berlin, Germany
Prölss, K. (författare)
Modelon Deutschland GmbH, Munich, Germany
Sielemann, M. (författare)
Modelon Deutschland GmbH, Munich, Germany
Rantzer, J. (författare)
Modelon AB, Lund, Sweden
Ekstedt, E. (författare)
Modelon AB, Lund, Sweden
visa färre...
 (creator_code:org_t)
American Society of Mechanical Engineers (ASME), 2019
2019
Engelska.
Ingår i: Proceedings of the ASME Turbo Expo. - : American Society of Mechanical Engineers (ASME). - 9780791858608 ; 3
  • Konferensbidrag (refereegranskat)
Abstract Ämnesord
Stäng  
  • 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.

Ämnesord

TEKNIK OCH TEKNOLOGIER  -- Maskinteknik -- Energiteknik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Mechanical Engineering -- Energy Engineering (hsv//eng)
TEKNIK OCH TEKNOLOGIER  -- Maskinteknik -- Rymd- och flygteknik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Mechanical Engineering -- Aerospace Engineering (hsv//eng)
TEKNIK OCH TEKNOLOGIER  -- Naturresursteknik -- Energisystem (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Environmental Engineering -- Energy Systems (hsv//eng)
TEKNIK OCH TEKNOLOGIER  -- Elektroteknik och elektronik -- Annan elektroteknik och elektronik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Electrical Engineering, Electronic Engineering, Information Engineering -- Other Electrical Engineering, Electronic Engineering, Information Engineering (hsv//eng)

Nyckelord

Aircraft manufacture
Airframes
Alternative fuels
Conceptual design
Economic and social effects
Electric power transmission
Gas turbines
Hydrogen fuels
Jet aircraft
Petroleum prospecting
Power generation
Propulsion
Rankine cycle
Simulation platform
Aircraft performance
Design space exploration
Electrical power system
Integration techniques
Physics-based Simulation
Thermal management systems
Transmission systems
Unconventional propulsions
Vehicle performance

Publikations- och innehållstyp

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