The invention relates to a vertical take-off and landing (VTOL), aircraft (1) comprising a fuselage (2) supporting two main wings (6), a first group of propulsion units (11) mounted fixedly on the aircraft (1) in a vertical thrust generating configuration, and a second group of propulsion units (12) each of which is mounted on the aircraft (1) configurable between a vertical thrust generating configuration and a horizontal thrust generating configuration, wherein the first group is subdivided into two front sets (13) and a rear set (14), wherein the two front sets (13) are mounted at opposite sides of the fuselage (2) ahead of the main wings (6) and the rear set (14) is mounted in the fuselage (2), passing therethrough, and wherein the second group is subdivided into a wing set (15) and a tail set (16), wherein the propulsion units (12) of the wing set (15) are mounted at opposite tips (27) of the main wings (6) and the propulsion units (12) of the tail set (16) are mounted at opposite sides of the fuselage (2).


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    Title :

    VTOL AIRCRAFT


    Additional title:

    SENKRECHTSTART- UND -LANDEFLUGZEUG
    AÉRONEF ADAV


    Contributors:

    Publication date :

    2023-12-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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