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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    Title :

    AIRCRAFT CANOPY WITH IMPROVED PERFORMANCE AND REDUCED LIFECYCLE COST


    Contributors:

    Publication date :

    2024-08-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT CANOPY WITH IMPROVED PERFORMANCE AND REDUCED LIFECYCLE COST

    BERGER THADDEUS STEVEN / YEH THOMAS C | European Patent Office | 2024

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