An aircraft safety system comprises an aircraft body 1 with an ejectable deceleration device provided within an openable cabin 2 on top of the body. A telescopic damping mechanism 5 provided on the bottom of the body is capable of extending to a position below the aircraft wheel body to buffer an impact force. The damping mechanism may comprise at least two vertical hydraulic struts 52 connected to the aircraft body, with a deformable elastic component (53, Figure 9) connecting the struts to a friction plate 51 that contacts the ground at impact. The plate may extend along the length direction of the body. A hydraulic inclined strut (54) may be arranged obliquely between the bottom of the aircraft battle and a telescopic end of the vertical strut. The deceleration device may comprise parachutes (31, Figure 6) located on the fuselage and tail, each comprising one or more layers. A propeller located on the fuselage with a generator may be connected to a battery. Deceleration wings with an arc structure protruding toward the nose may be fixedly or rotatably connected to the aircraft body.


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    Titel :

    Aircraft safety lifesaving system


    Beteiligte:
    DI DU (Autor:in) / YANG DU (Autor:in) / TONG DU (Autor:in)

    Erscheinungsdatum :

    07.12.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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