Shock strut assemblies for landing gear
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.
Public/Granted literature
Information query
Patent Agency Ranking
0/0