The invention is directed a trapezoidal panel pin joint for allowing deflection of an aircraft between a fuselage section and a wing section, wherein the pin joint comprises a vertical pin portion, a lug portion, and a clevis portion; wherein at least one vertical flexible tee member is positioned below the pin joint; and wherein the pin joint is coupled to at least two horizontal flexible tee members, such that the pin joint and vertical and horizontal flexible tee members, in combination, release two rotational degrees of freedom.
TRAPEZOIDAL PANEL PIN JOINT ALLOWING FREE DEFLECTION BETWEEN FUSELAGE AND WING
TRAPEZFÖRMIGE TAFELSTECKVERBINDUNG ZUR FREIEN DEFLEKTION ZWISCHEN RUMPF UND TRAGFLÄCHE
JOINT À TENON DE PANNEAU TRAPÉZOÏDAL PERMETTANT UNE DÉFORMATION LIBRE ENTRE UN FUSELAGE ET UNE AILE
2018-06-20
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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