A method of constructing a reduced drag wing, including: providing a top wing surface panel; coupling a top surface external leading-edge panel to the external surface of the top wing surface panel, wherein the top surface external leading-edge panel extends forward from the top wing surface panel and extends rearward covering at least partially the top surface external leading-edge panel; coupling internal rib elements to the interior surface of the top wing surface panel; coupling the top surface external leading-edge panel to a sleeve element; coupling the rear sleeve element to a bottom wing surface panel; coupling the internal rib elements to the interior surface of the bottom wing surface panel; and coupling the top surface external leading-edge panel and the sleeve element to a releasable mechanical mechanism. A reduced drag wing for a wingsuit. A wingsuit including a reduced drag wing.


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    Title :

    REDUCED DRAG WINGSUIT


    Contributors:

    Publication date :

    2020-02-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / A41D Oberbekleidung , OUTERWEAR




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