A shock strut assembly (30, 32, 34) for a landing gear may comprise a strut cylinder (102), a strut piston (104) configured to telescope relative to the strut cylinder (102), and a locking system. The locking system may be configured to restrict rotation of the strut piston (104) relative to the strut cylinder (102) in response to compression of the shock strut assembly (30, 32, 34).
SHOCK STRUT ASSEMBLIES FOR LANDING GEAR
FEDERBEINANORDNUNG FÜR EIN FAHRWERK
ENSEMBLES JAMBES À AMORTISSEUR POUR TRAINS D'ATTERRISSAGE
2022-08-10
Patent
Elektronische Ressource
Englisch