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
26.11.2020
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2021
|Europäisches Patentamt | 2025
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