Aircraft landing gear assemblies, aircraft including the landing gear assemblies, and methods of deploying landing gear assemblies. The landing gear assemblies include an elongate landing gear strut, a wheel assembly, and a deployment structure. The elongate landing gear strut includes a first strut end region, an opposed second strut end region, and a wheel assembly mount. The wheel assembly is coupled to the wheel assembly mount. The deployment structure is configured to selectively transition the landing gear assembly between a stowed state and a deployed state.
AIRCRAFT LANDING GEAR ASSEMBLIES, AIRCRAFT INCLUDING THE LANDING GEAR ASSEMBLIES, AND METHODS OF DEPLOYING THE LANDING GEAR ASSEMBLIES
2020-11-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2021
|European Patent Office | 2025
|European Patent Office | 2025
|CONFIGURATION OF LANDING GEAR ASSEMBLIES FOR AN AIRCRAFT
European Patent Office | 2020
|