ABSTRACT 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. Date Recue/Date Received 2021-11-12
SHOCK STRUT ASSEMBLIES FOR LANDING GEAR
ASSEMBLAGES DE JAMBES AMORTISSEUSES POUR UN TRAIN D'ATTERRISSAGE
2022-06-16
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |