An aircraft, such as a drone or a single-seat aircraft, includes a body and a pair of wing portions, each wing portion including a front wing and a rear wing, where the front wing and the rear wing each include a first end connected to the body and a second end, where the second end of the front wing is connected to the second end of the rear wing. The main body is located between the pair of wing portions, each wing portion including a propulsion unit located between a front wing and a rear wing of the wing portion. Each propulsion unit may include a first rotor and a second rotor that are pivotable relative to the remainder of the aircraft.

    一种飞机例如无人驾驶飞机或单座飞机,包括主体和一对机翼部分,每个机翼部分包括前翼和后翼,其中前翼和后翼各自包括第一端以及第二端,第一端连接到主体,其中前翼的第二端连接到后翼的第二端。主体位于所述一对机翼部分之间,每个机翼部分包括位于机翼部分的前翼和后翼之间的推进单元。每个推进单元可以包括第一旋翼和第二旋翼,它们能够相对于飞机的其余部分枢转。


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    Titel :

    Vertical take-off and landing aircraft with parallel wings


    Weitere Titelangaben:

    并式机翼垂直起降飞机


    Beteiligte:

    Erscheinungsdatum :

    11.03.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge




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