An aircraft (40) comprises an internal combustion engine (10) and a wing (44) comprising a hollow structural member (74, 76, 78). The aircraft (40) comprises an electrical network comprising: at least one alternating current electrical generator (56) configured to be driven by the internal combustion engine (10); an electrical motor (51) configured to drive an aircraft propulsor (46); at least one conductor (80, 82) configured to electrically couple the electrical motor (52) and the electrical generator (56); wherein the electrical conductor (80, 82) is formed of the hollow structural member (74, 76, 78) of the aircraft wing (44).
AIRCRAFT ELECTRICAL NETWORK
FLUGZEUGSTROMNETZ
RÉSEAU ÉLECTRIQUE D'AÉRONEF
27.11.2019
Patent
Elektronische Ressource
Englisch