CPC B64C 1/20 (2013.01) | 10 Claims |
1. An aircraft comprising:
a central wing box;
a front fuselage portion that is positioned, along a longitudinal direction, in front of the central wing box; and
a floor positioned above the central wing box and in the front fuselage portion, the floor comprising at least one rail which extends along the longitudinal direction and has at least one core, wherein the at least one rail comprises:
a first rail portion;
a second rail portion, and
at least one articulation connecting a first end of the core of the first rail portion and a second end of the core of the second rail portion, the articulation comprising:
at least one splice plate having first and second ends,
a pivot pin oriented perpendicularly to the longitudinal direction, passing through the first end of the core of the first rail portion and the first end of the splice plate, and
at least one first complete link connecting the second end of the core of the second rail portion and the second end of the splice plate.
|