An aircraft defining a longitudinal direction and a lateral direction is provided. The aircraft includes a fuselage; an engine mounted at a location spaced from the fuselage of the aircraft, the engine comprising rotor blades; and at least one fuselage shield removably coupled to the fuselage at a location in alignment with the rotor blades along the lateral direction.


    Access

    Download


    Export, share and cite



    Title :

    Removeable fuselage shield for an aircraft



    Publication date :

    2024-10-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64C AEROPLANES , Flugzeuge



    REMOVEABLE FUSELAGE SHIELD FOR AN AIRCRAFT

    CRALL DAVID WILLIAM / KRAY NICHOLAS JOSEPH / WARD DOUGLAS DUANE et al. | European Patent Office | 2021

    Free access

    Cart with removeable basket

    CHOI WARREN WON | European Patent Office | 2020

    Free access

    Layered fuselage shield

    CRALL DAVID WILLIAM / KRAY NICHOLAS JOSEPH / WARD DOUGLAS DUANE et al. | European Patent Office | 2023

    Free access

    Cart with removeable basket

    CHOI WARREN WON | European Patent Office | 2020

    Free access

    LAYERED FUSELAGE SHIELD

    CRALL DAVID WILLIAM / KRAY NICHOLAS JOSEPH / WARD DOUGLAS DUANE et al. | European Patent Office | 2021

    Free access