TY - GEN
T1 - Resilient multi-bus distribution in more electric aircraft by means of dual active bridges
AU - Buticchi, Giampaolo
AU - Costa, Levy
AU - Liserre, Marco
N1 - Publisher Copyright:
© 2017 IEEE.
PY - 2017/8/3
Y1 - 2017/8/3
N2 - The actuation system of an aircraft relies heavily on hydraulic actuation. In order to improve the reliability of the system while improving the power density, researchers have investigated the possibility to increase the penetration of electric system. In this scenario, the electrical power distribution system (EPDS) becomes very important This paper proposes an architecture of the EPDS based on dual active bridge converters, virtual resistors are used to share the power and to handle faults. Simulation results show the good behavior of the EPDS, that can withstand faults in the buses and still supply the critical loads.
AB - The actuation system of an aircraft relies heavily on hydraulic actuation. In order to improve the reliability of the system while improving the power density, researchers have investigated the possibility to increase the penetration of electric system. In this scenario, the electrical power distribution system (EPDS) becomes very important This paper proposes an architecture of the EPDS based on dual active bridge converters, virtual resistors are used to share the power and to handle faults. Simulation results show the good behavior of the EPDS, that can withstand faults in the buses and still supply the critical loads.
UR - http://www.scopus.com/inward/record.url?scp=85029896611&partnerID=8YFLogxK
U2 - 10.1109/ISIE.2017.8001535
DO - 10.1109/ISIE.2017.8001535
M3 - Conference contribution
AN - SCOPUS:85029896611
T3 - IEEE International Symposium on Industrial Electronics
SP - 1874
EP - 1878
BT - Proceedings - 2017 IEEE International Symposium on Industrial Electronics, ISIE 2017
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 26th IEEE International Symposium on Industrial Electronics, ISIE 2017
Y2 - 18 June 2017 through 21 June 2017
ER -