A wing-to-body fairing on an aircraft having a fuselage, wing, and a wing root fairing. The wing-to-body fairing includes forward and trailing edges. The forward edge is configured for positioning adjacent a first predetermined location of an aft portion of the wing root fairing. The trailing edge is configured for positioning adjacent a second predetermined location of the aft portion of the fuselage. A convex-shaped forward portion of the fairing is configured to conform to the aft portion of the wing root fairing at the first predetermined location. A concave-shaped aft portion of the fairing is configured to conform to the aft portion of the fuselage at the second predetermined location. An exterior surface of the wing-to-body fairing is gradient optimized to minimize curvature, where the fairing trailing edge is configured with matching angles and contours as the aft portion of the fuselage at the second location.


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    Titel :

    WING-TO-BODY TRAILING EDGE FAIRING AND METHOD OF FABRICATING SAME


    Weitere Titelangaben:

    FLÜGEL-ZU-RUMPF-HINTERKANTENVERKLEIDUNG UND VERFAHREN ZUR HERSTELLUNG DAVON
    CARÉNAGE DE BORD DE FUITE DE JONCTION AILE-FUSELAGE ET SON PROCÉDÉ DE FABRICATION


    Beteiligte:
    SANDERS LEE (Autor:in) / AHLSTROM ERIC A (Autor:in) / WILSON MATTHEW DAVID (Autor:in)

    Erscheinungsdatum :

    2021-01-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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