An aircraft includes a fuselage coupled to a wing having a root section and first and second outboard sections each having first and second wing layers pivotably coupled to respective outboard ends of the root section. A thrust array is coupled to the wing. A power system is operably associated with the thrust array to provide power to each of a plurality of propulsion assemblies. A flight control system is operably associated with the thrust array and the wing. The flight control system is operable to control the thrust output from the propulsion assemblies and the configuration of the wing. In a thrust-borne vertical lift mode, the wing has a split wing configuration such that the thrust array forms a two dimensional thrust array. In the wing-borne forward flight mode, the wing has a monoplane configuration such that the thrust array forms a one dimensional thrust array.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft having split wing and monoplane configurations


    Beteiligte:

    Erscheinungsdatum :

    2020-12-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Aircraft having Split Wing and Monoplane Configurations

    GAFFNEY SEAN ROBERT / GRAHAM JR ROBERT REX | Europäisches Patentamt | 2019

    Freier Zugriff

    Monoplane wing layout

    Huchison, H.H. | Engineering Index Backfile | 1934


    High wing cabin monoplane

    Engineering Index Backfile | 1929


    Fairchild 21 low-wing monoplane

    Engineering Index Backfile | 1929


    Fairchild 21 low-wing monoplane

    Engineering Index Backfile | 1929