An electric aircraft includes a propeller, an electric motor, and a controller. The electric motor is configured to supply power to the propeller. The controller is configured to control the electric motor. The controller is disposed inside a leading-edge portion of a wing to cause heat to be transmitted to a skin of the wing. The heat is generated by the controller when the controller controls the electric motor.
ELECTRIC AIRCRAFT AND ANTI-ICING APPARATUS FOR ELECTRIC AIRCRAFT
2021-03-04
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Electric aircraft and anti-icing apparatus for electric aircraft
European Patent Office | 2022
|NTIS | 1971