This article proposes a power hybridization factor-dependent DC supply grid layout and fault protection for hybrid electric aircraft. It is based on a regulatory review and an analysis of the grid components regarding their impact on grid layout and protection. The findings are applicable to medium-voltage DC and high-temperature superconductor-based electrical drive trains.
DC supply structure and protection concept for (hybrid) electric CS-25 aircraft
CEAS Aeronaut J
CEAS Aeronautical Journal ; 11 , 3 ; 623-632
2020-09-01
10 pages
Article (Journal)
Electronic Resource
English
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