The present invention pertains to the technical field of electrically powered aircraft. According to the present invention, such an electrically powered aircraft (1) is required to comprise at least one non-retractable main landing gear (2a, 2b), wherein said main landing gear (2a, 2b) comprises a wheel (3) and linkage kinematics (4) for attaching said wheel (3) to a structural component (5) of said aircraft (1), and wherein said structural component (5) supports and transmits the loads exerted by the main landing gear (2a, 2b) to a fuselage of the aircraft (1) as well as performs an aerodynamic stability function.
ELECTRICALLY POWERED AIRCRAFT
ELEKTRISCH ANGETRIEBENES FLUGZEUG
AVION ÉLECTRIQUE
2023-05-24
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2021
|Designing Electrically Powered Actuators for Aircraft
Online Contents | 1997