Structural frame for an aircraft fuselage

Details Structural frame for an aircraft fuselage Structural frame for an aircraft fuselage

B - Operations, Transporting

64

C

B64C 1/06 (2006.01)

Patent

CA 2585869

The invention relates to a structural frame for an aircraft fuselage, comprising a lower arched structure (1), a cross-piece (2), supporting a floor element (3) and a connecting lattice (4), between the lower arch (1) and the cross-piece (2). More particularly, said connecting lattice (4) may comprise bars (4a, 4b), the ends of which are spliced to the cross-piece (2) and the lower arch (1).

L'objet de l'invention est un cadre de structure de fuselage comportant un élément de cintre inférieur (1), une traverse (2), de soutien d'un élément de plancher (3) et un treillis de liaison (4) entre le cintre inférieur (1) et la traverse (2), le treillis de liaison (4) pouvant plus particulièrement être constitué de barres (4a, 4b) dont les extrémités sont éclissées sur la traverse (2) et sur le cintre inférieur (1).

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