The student will be able to get familiar with topics related to energy storage systems, main technologies, and their active management.
Methodologies to understand electric power generation will be provided.
Knowledge of power converter architectures and their applications to electrified powertrains for propulsion and generation. Fault tolerant characteristics and mode of operations will be part of the course.
Digital Twin real-time simulators will be used to show real cases applications
Methodologies to understand electric power generation will be provided.
Knowledge of power converter architectures and their applications to electrified powertrains for propulsion and generation. Fault tolerant characteristics and mode of operations will be part of the course.
Digital Twin real-time simulators will be used to show real cases applications
scheda docente
materiale didattico
Power converter configurations, fault-tolerance operation.
Electrical machines, operation, architecture, and fault-tolerance capabilities.
Configuration of the on-board electrical grids.
Propulsion architectures and electric power generation on board aircraft, from conventional to hybrid and full-electric powertrains. Hybrid parallel and series. Partially electric series and parallel.
Sizing of storage systems, series, and parallel configurations. Application examples on unmanned aircraft. Battery Management Systems.
Trends in aeronautical electric propulsion.
Ground Power Units (GPU).
Matlab/Simulink as well as National Instruments LabVIEW software will be used during lessons.
Real-Time simulation of electrical systems by Hardware-in-the-loop (HIL) platforms will be shown during the course: from model design to solver deployment.
Haran K, Madavan N, O’Connell TC, eds. Electrified Aircraft Propulsion: Powering the Future of Air Transportation. Cambridge University Press; 2022.
https://ieeexplore.ieee.org/book/8854887
https://ieeexplore.ieee.org/book/7753049
https://ieeexplore.ieee.org/book/8504362
https://ieeexplore.ieee.org/book/9989444
Programma
Energy storage systems and their applications in the aerospace field. High-temperature electrochemical energy storage systems. Supercapacitors. Lithium-based energy storage systems, management, protections, and standards. Hydrogen energy storage.Power converter configurations, fault-tolerance operation.
Electrical machines, operation, architecture, and fault-tolerance capabilities.
Configuration of the on-board electrical grids.
Propulsion architectures and electric power generation on board aircraft, from conventional to hybrid and full-electric powertrains. Hybrid parallel and series. Partially electric series and parallel.
Sizing of storage systems, series, and parallel configurations. Application examples on unmanned aircraft. Battery Management Systems.
Trends in aeronautical electric propulsion.
Ground Power Units (GPU).
Matlab/Simulink as well as National Instruments LabVIEW software will be used during lessons.
Real-Time simulation of electrical systems by Hardware-in-the-loop (HIL) platforms will be shown during the course: from model design to solver deployment.
Testi Adottati
Notes provided by the course manager.Haran K, Madavan N, O’Connell TC, eds. Electrified Aircraft Propulsion: Powering the Future of Air Transportation. Cambridge University Press; 2022.
https://ieeexplore.ieee.org/book/8854887
https://ieeexplore.ieee.org/book/7753049
https://ieeexplore.ieee.org/book/8504362
https://ieeexplore.ieee.org/book/9989444
Bibliografia Di Riferimento
V. Madonna, P. Giangrande and M. Galea, "Electrical Power Generation in Aircraft: Review, Challenges, and Opportunities," in IEEE Transactions on Transportation Electrification, vol. 4, no. 3, pp. 646-659, Sept. 2018, doi: 10.1109/TTE.2018.2834142. T. C. Cano et al., "Future of Electrical Aircraft Energy Power Systems: An Architecture Review," in IEEE Transactions on Transportation Electrification, vol. 7, no. 3, pp. 1915-1929, Sept. 2021, doi: 10.1109/TTE.2021.3052106 Xin Zhao, J. M. Guerrero and Xiaohua Wu, "Review of aircraft electric power systems and architectures," 2014 IEEE International Energy Conference (ENERGYCON), Cavtat, Croatia, 2014, pp. 949-953, doi: 10.1109/ENERGYCON.2014.6850540. M. Ghassemi, A. Barzkar and M. Saghafi, "All-Electric NASA N3-X Aircraft Electric Power Systems," in IEEE Transactions on Transportation Electrification, vol. 8, no. 4, pp. 4091-4104, Dec. 2022, doi: 10.1109/TTE.2022.3158186. P. Kshirsagar et al., "Anatomy of a 20 MW Electrified Aircraft: Metrics and Technology Drivers," 2020 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS), New Orleans, LA, USA, 2020, pp. 1-9. X. Roboam, "New trends and challenges of electrical networks embedded in “more electrical aircraft”," 2011 IEEE International Symposium on Industrial Electronics, Gdansk, Poland, 2011, pp. 26-31, doi: 10.1109/ISIE.2011.5984130.Modalità Frequenza
Attendance is strongly recommended.Modalità Valutazione
Learning is verified through an interview. The student will be asked two questions related to the topics covered during the course.