A main fitting includes an elongate piston and a cylinder configured to slidingly receive the piston. A first end of the piston extends from a first end of the cylinder, and a second end of the piston extends from a second end of the cylinder. The first end of the cylinder comprises a bearing surface engaging the piston to limit translation of the piston relative to the cylinder to a longitudinal direction.
LANDING GEAR MAIN FITTING WITH INTEGRAL SHOCK ABSORBER
02.05.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
LANDING GEAR MAIN FITTING WITH INTEGRAL SHOCK ABSORBER
Europäisches Patentamt | 2024
|