The invention relates to an aircraft, comprising: a cell (2), which is designed to accommodate a plurality of electric drive devices (12, 46) and through which a through-channel (60) extends; and a first electric motor (46), which comprises a motor housing (45) and a drive shaft (54) rotatably mounted in the motor housing (45) and which is arranged at least partly in the through-channel (60), the drive shaft (54) or the motor housing (45) being connected to a rotor assembly (35) arranged outside the through-channel (60), the motor housing (45) or the drive shaft (54) being connected to an impeller (55) arranged in the through-channel (60), and the motor housing (45) and the drive shaft (54) being rotatably mounted on the cell (2), whereby a restoring-torque-free drive system results.
Fluggerät
2022-08-25
Patent
Elektronische Ressource
Deutsch
IPC: | B64C AEROPLANES , Flugzeuge |