Helicopter one-piece door

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/22 (2006.01) B64C 1/14 (2006.01)

Patent

CA 2606946

An aircraft vehicle (100) includes a body (108), including a front portion and a rearward tail portion, a single panel door (105) constructed and arranged to close an access opening defined in a lower portion of the body (108), and a linkage between the body (108) and the door (105) . The linkage is constructed and arranged to move the door (105) generally rearwardly and upwardly when the door is moved from a closed position to an opened position, so that the door is positioned below and adjacent to the rearward tail portion.

L'invention concerne un aéronef (100) comportant un corps (108) présentant une partie frontale, une partie de queue arrière, une porte à panneau individuel (105) conçue pour fermer une ouverture d'accès définie dans une partie inférieure du corps (108), et une connexion entre le corps (108) et la porte (105). La connexion est conçue pour déplacer la porte (105) essentiellement vers l'arrière et vers le haut, de la position fermée vers la position ouverte, de telle manière que la porte est disposée en-dessous de la partie de queue arrière, de façon adjacente à celle-ci.

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