A telescopic spar mechanism is provided. The telescopic spar mechanism comprises a housing, an outer tube rotatably coupled to the housing, and an inner tube received within the outer tube. The outer tube having flat walled threads formed on an inside. The inner tube having a plurality of spaced apart bearings secured to an outside of the inner tube, where the plurality of bearings are received within lands of the threads of the outer tube. The telescopic spar mechanism is used in combination with a wing assembly to increase the wing size of VTOL aircrafts.


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    Titel :

    WING DESIGN FOR VTOL AIRCRAFT LANDING IN CONSTRAINED SPACES


    Beteiligte:
    BRAVERMAN JASON (Autor:in) / KNAFO YURI (Autor:in)

    Erscheinungsdatum :

    2021-07-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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