A shock strut assembly for a landing gear may comprise a strut cylinder, a strut piston configured to telescope relative to the strut cylinder, and a locking system. The locking system may be configured to restrict rotation of the strut piston relative to the strut cylinder in response to compression of the shock strut assembly.
SHOCK STRUT ASSEMBLIES FOR LANDING GEAR
2022-06-16
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
SELF-SUSTAINING SHIMMY DAMPER SYSTEM FOR LANDING GEAR SHOCK STRUT ASSEMBLIES
European Patent Office | 2023
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