A base assembly for an aircraft seat is disclosed. The base assembly may include one or more leg sub-assemblies. Each leg sub-assembly may include a front leg, a rear leg, and a link beam 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.


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    Title :

    Aircraft seat base assembly


    Contributors:

    Publication date :

    2024-11-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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