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, wherethe fairing trailing edge is configured with matching angles and contours as the aft portion of the fuselage at the second location.

    一种具有机身、机翼和翼根整流罩的飞行器上的翼身整流罩。该翼身整流罩包括前缘和后缘。前缘被构造为定位成邻近翼根整流罩的后部的第一预定位置。后缘被构造为定位成邻近机身的后部的第二预定位置。整流罩的凸形前部被构造为符合在第一预定位置的翼根整流罩的后部。整流罩的凹形后部被构造为符合在第二预定位置的机身的后部。翼身整流罩的外表面被梯度优化以使曲率最小化,其中整流罩后缘被构造为具有与在第二位置的机身的后部相匹配的角度和轮廓。


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    Titel :

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


    Weitere Titelangaben:

    翼身后缘整流罩及其制造方法


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

    Erscheinungsdatum :

    2020-12-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    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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