Transverse framework intended for an avionics bay of an aircraft, assembly module and aircraft comprising the said transverse framework

An aircraft comprising:

• an avionics bay separated from a second bay by a rear boundary and a transverse framework for the avionics bay, the avionics bay being delimited by a primary structure and a floor, and wherein the transverse framework comprises:
• vertical connecting rods, positioned in a first transverse plane, which each comprise, at an upper end, a first connection connected to an anchor point provided in the floor and, at a lower end, a second connection connected to an anchor point provided in the primary structure,
• first horizontal transverse members, connecting the vertical connecting rods in pairs, and positioned in the first transverse plane,
• vertical uprights, positioned in a second transverse plane spaced away from the first transverse plane,
• second horizontal transverse members, connecting the vertical uprights in pairs, and positioned in the second transverse plane,
• horizontal longitudinal members oriented perpendicular to the first transverse plane, connecting the vertical connecting rods and the vertical uprights in pairs,
• wherein the vertical connecting rods, the vertical uprights, the first and second transverse members and the longitudinal members are arranged in such a way that the transverse framework forms a mesh structure with square and/or rectangular mesh cells, and
• wherein the transverse framework comprises at least one sliding connection connecting equipment and the transverse framework and configured to allow said equipment translational movement in a direction perpendicular to the first transverse plane with respect to the transverse framework.

An aircraft comprising:

• an avionics bay separated from a second bay by a rear boundary and a transverse framework for the avionics bay, the avionics bay being delimited by a primary structure and a floor, and wherein the transverse framework comprises:
• vertical connecting rods, positioned in a first transverse plane, which each comprise, at an upper end, a first connection connected to an anchor point provided in the floor and, at a lower end, a second connection connected to an anchor point provided in the primary structure,
• first horizontal transverse members, connecting the vertical connecting rods in pairs, and positioned in the first transverse plane,
• vertical uprights, positioned in a second transverse plane spaced away from the first transverse plane,
• second horizontal transverse members, connecting the vertical uprights in pairs, and positioned in the second transverse plane,
• horizontal longitudinal members oriented perpendicular to the first transverse plane, connecting the vertical connecting rods and the vertical uprights in pairs,
• wherein the vertical connecting rods, the vertical uprights, the first and second transverse members and the longitudinal members are arranged in such a way that the transverse framework forms a mesh structure with square and/or rectangular mesh cells,
• wherein the first transverse plane of the transverse framework is positioned perpendicular to a longitudinal direction of the aircraft, at the rear boundary, and
• wherein the transverse framework comprises a pressure bulkhead bearing against the vertical connecting rods and providing sealing between the avionics bay and the second bay, the pressure bulkhead comprising at least one opening and, for each opening, a blowout panel configured to occupy a state of rest in which the blowout panel blanks off the opening and a post-blowout detached state in which the blowout panel at least partially uncovers the opening.