An aircraft assembly is disclosed and includes a fuselage including a turbine engine mounted within the aft fuselage. burst zone is defined about the turbine engine and a tail is disposed at least partially with the burst zone. The tail includes primary control surfaces and sacrificial control surfaces. The sacrificial control surfaces can break away in a defined manner to maintain integrity of the primary control surfaces outside of the burst zone.


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    Titel :

    STABILIZER SACRIFICIAL SURFACES


    Beteiligte:

    Erscheinungsdatum :

    17.09.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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