A tray table (200) for an aircraft and a method of manufacturing the same are disclosed. The tray table (200) comprises a base portion (210), a first tray table portion, and a second tray table portion. A first flexural hinge (240) pivots the first tray table portion relative to the base portion (210). A second flexural hinge (250) pivots the second tray table portion relative to the first tray table portion. The first flexural hinge (240) and the second flexural hinge (250) comprise flexural members (245a-c, 255a-c) which are pliable to enable the respective flexural hinge to pivot. The base portion (210), the first surface portion, the first flexural hinge (240), the second surface portion, and the second flexural hinge (250) are integrally formed to provide a unitary tray table (200) construction.


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    Title :

    INTEGRALLY FORMED TRAY TABLE WITH FLEXURAL HINGES


    Additional title:

    INTEGRAL GEFORMTER SERVIERTISCH MIT BIEGESCHARNIEREN
    TABLE À PLATEAUX FORMÉE D'UN SEUL TENANT AVEC CHARNIÈRES FLEXIBLES



    Publication date :

    2023-10-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60N SEATS SPECIALLY ADAPTED FOR VEHICLES , Sitze besonders für Fahrzeuge ausgebildet / E05D Scharniere oder andere Aufhängevorrichtungen für Türen, Fenster oder Flügel , HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS, OR WINGS



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