This morphing wing (140) comprises: a link structure capable of expanding in a first direction and retracting in a second direction, which is opposite to the first direction; a plurality of front wing covers (180) mounted frontward, which is one side orthogonal to the first direction in the link structure; and a plurality of flight feathers (160) mounted rearward, which is the other side orthogonal to the first direction in the link structure. The front wing covers (180) and the flight feathers (160) are streamlined from front to back, and when the link structure retracts, flight feathers (160) retract inside adjacent flight feathers (160).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Morphing wing, flight control device, flight control method, and program


    Beteiligte:
    DAICHI WADA (Autor:in)

    Erscheinungsdatum :

    2024-04-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G06N COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS , Rechnersysteme, basierend auf spezifischen Rechenmodellen



    Morphing wing, flight control device, flight control method, and program

    DAICHI WADA | Europäisches Patentamt | 2023

    Freier Zugriff


    MORPHING WING, FLIGHT CONTROL DEVICE, FLIGHT CONTROL METHOD, AND PROGRAM

    WADA DAICHI | Europäisches Patentamt | 2023

    Freier Zugriff

    MORPHING WING, FLIGHT CONTROL DEVICE, FLIGHT CONTROL METHOD, AND PROGRAM

    WADA DAICHI | Europäisches Patentamt | 2021

    Freier Zugriff

    MORPHING WING, FLIGHT CONTROL APPARATUS, FLIGHT CONTROL METHOD, AND PROGRAM

    WADA DAICHI | Europäisches Patentamt | 2023

    Freier Zugriff