A landing gear includes a wheel support portion connected to a fuselage of an aircraft, a wheel rotatably connected to the wheel support portion via a shaft, a stator mounted on the shaft, and a rotor mounted on the wheel spaced apart from the stator.
LANDING GEAR OF AIRCRAFT AND METHOD FOR TAKEOFF AND LANDING USING LANDING GEAR
FAHRWERK EINES FLUGZEUGS UND VERFAHREN ZUM STARTEN UND LANDEN UNTER VERWENDUNG DES FAHRWERKS
TRAIN D'ATTERRISSAGE D'AÉRONEF ET PROCÉDÉ DE DÉCOLLAGE ET D'ATTERRISSAGE UTILISANT LE TRAIN D'ATTERRISSAGE
22.01.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2024
|Europäisches Patentamt | 2023
|Retractable landing gear system for a vertical takeoff and landing (VTOL) aircraft
Europäisches Patentamt | 2021
|RETRACTABLE LANDING GEAR SYSTEM FOR A VERTICAL TAKEOFF AND LANDING (VTOL) AIRCRAFT
Europäisches Patentamt | 2020
|RETRACTABLE LANDING GEAR SYSTEM FOR A VERTICAL TAKEOFF AND LANDING (VTOL) AIRCRAFT
Europäisches Patentamt | 2019
|