B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/26 (2006.01)
Patent
CA 2658847
The invention is directed a trapezoidal panel pin joint (10) for allowing deflection of an aircraft between a fuselage section (14) and a wing section (12), wherein the pin joint comprises a vertical pin portion (16), a lug portion (18), and a clevis portion (20); wherein at least one vertical flexible tee member (26) 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.
L'invention concerne un joint à tenon de panneau trapézoïdal pour permettre la déformation d'un avion entre une section de fuselage et une section d'aile, le joint à tenon comportant une partie de tenon verticale, une partie d'oreille et une partie de manille; au moins un élément souple vertical à tenon en t est positionné en dessous du joint à tenon; le joint à tenon étant couplé à au moins deux éléments souples horizontaux en t, de sorte que le joint à tenon et les éléments souples verticaux et horizontaux en t, en combinaison, libèrent deux degrés de liberté de rotation.
Estell Patricia
Polk John H.
Smart & Biggar
The Boeing Company
LandOfFree
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