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49,80 €ISBN 978-3-8440-8209-8Softcover204 pages47 figures305 g21 x 14,8 cmGermanThesis
September 2021
Robert Doering
Rechnergestützter Entwurf lokaler elektrischer Energiesysteme zur Individualisierung der Kabinen-Energieversorgung von Verkehrsflugzeugen
Durch den Einsatz lokaler elektrischer Energiesysteme wird es möglich, die Leistungsfähigkeit der Kabinen-Energieversorgung von Verkehrsflugzeugen individuell an den jeweiligen Bedarf eines Flugzeugs anzupassen. Hierdurch kann für eine Vielzahl von Anwendungsfällen eine gravimetrische Optimierung des elektrischen Systems des Flugzeugs erreicht werden. Zeitgleich nimmt die Zukunftsfähigkeit eines Flugzeugentwurfs zu, da auch im späteren Verlauf eines Flugzeuglebens die Leistungsfähigkeit des elektrischen Systems vergleichsweise einfach angepasst werden kann. Innerhalb dieser Arbeit werden rechnergestützte Methoden und Werkzeuge vorgestellt, welche die Konzeptionierung, Auslegung und Bewertung solcher lokalen elektrischen Energiesystemen ermöglichen.
The use of local electrical power systems allows to individually adapt the performance of the cabin power supply of commercial aircraft to the respective requirements of an aircraft. As a result, gravimetric optimization of the aircraft's electrical system can be achieved for a variety of use cases. Furthermore, the future viability of an aircraft design increases, since even in the later course of an aircraft's life, the performance of the electrical system can be adjusted comparatively easily. Within this thesis, computational methods and tools are presented, which enable the development, design and evaluation of such local electric power systems.
The use of local electrical power systems allows to individually adapt the performance of the cabin power supply of commercial aircraft to the respective requirements of an aircraft. As a result, gravimetric optimization of the aircraft's electrical system can be achieved for a variety of use cases. Furthermore, the future viability of an aircraft design increases, since even in the later course of an aircraft's life, the performance of the electrical system can be adjusted comparatively easily. Within this thesis, computational methods and tools are presented, which enable the development, design and evaluation of such local electric power systems.
Keywords: Flugzeug-Systemtechnik; Kabinen-Energieversorgung; elektrisches System; Modellierung; Simulation; Brennstoffzelle; Batterie; Flugzeugentwurf
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