A base assembly (210) for an aircraft seat (200) is disclosed. The base assembly may include one or more leg sub-assemblies (216). Each leg sub-assembly may include a front leg (218), a rear leg (220), and a link beam (226) configured to couple the front leg to a portion of the rear leg. At least one of the front leg or the rear leg being at least partially formed of a hybrid composite structure. The link beam being at least partially formed of the hybrid composite structure. The hybrid composite structure formed of at least a first material and a second material, where the first material is different from the second material, the first material including a thermoplastic material configured to provide ductility for the base assembly, the second material being a composite material configured to provide strength for the base assembly.
AIRCRAFT SEAT BASE ASSEMBLY
FLUGZEUGSITZBASISANORDNUNG
ENSEMBLE BASE DE SIÈGE D'AVION
11.09.2024
Patent
Elektronische Ressource
Englisch