An aircraft canopy comprises first and second canopy portions, wherein the first canopy portion includes a leading edge having a sawtooth shape and wherein the second canopy portion has a trailing edge complementary to the shape of the front bow edge. An interconnect structure is disposed between the leading edge and the trailing edge and maintains the first and second canopy portions in assembled relationship.


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    Titel :

    AIRCRAFT CANOPY WITH IMPROVED PERFORMANCE AND REDUCED LIFECYCLE COST


    Beteiligte:

    Erscheinungsdatum :

    01.08.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT CANOPY WITH IMPROVED PERFORMANCE AND REDUCED LIFECYCLE COST

    BERGER THADDEUS STEVEN / YEH THOMAS C | Europäisches Patentamt | 2024

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