Abstract: A ventilation system for an aircraft having a structure bearing an exterior wall and an interior covering. At least one duct intended to be installed between the interior covering and the exterior wall. The duct includes one first pipe and at least one second pipe which is able to slide telescopically in relation to the first pipe between a retracted position and an extended position.

Abstract: A module in the form of a pallet or a closed container includes a grouping together of the electrical devices in an avionics bay, in which the electrical devices are interconnected and attached so as to facilitate the mounting and thus limit the time it takes to mount the electrical devices in the avionics bay.

Abstract: A device for interior covering of an aircraft cabin, intended to be fastened to a structure of an aircraft and to extend along a skin of the aircraft, the device comprising a covering panel. The covering panel bears at least one system, possibly through a system support. It advantageously comprises at least one air circulation pipe fastened to an exterior face of the covering panel, each air pipe having an upstream end equipped with a connection device.

Abstract: The invention relates to a device for holding an insulating blanket and for fastening systems in an aircraft, comprising a base having two ends from each of which an arm extends. At least one arm has a U-shaped part having two more or less parallel branches, and in that the said device further comprises at least one support for accommodating a system. The invention also relates to an aircraft fuselage section comprising frames, an outer skin, stabilizers and at least one insulating blanket. This section comprises at least one holding device such as described above, mounted so that a frame is situated between the arms of the holding device so that the blanket is between the frame and the holding device.

Abstract: The invention relates to a device for interior covering (1) of an aircraft cabin, intended to be fastened to a structure of an aircraft and to extend along a skin of the aircraft, the said device comprising a covering panel (2). The covering panel bears at least one system, possibly through a system support. It advantageously comprises at least one air circulation pipe (3), referred to as air pipe, fastened to an exterior face (6) of the covering panel, each air pipe having an end (26), referred to as upstream end, equipped with a connection device (27).

Abstract: This ventilation system is intended for an aircraft comprising a structure bearing an exterior wall and an interior covering. It has at least one duct (1) intended to be installed between the interior covering and the exterior wall. The duct (1) comprises one first pipe (2) and at least one second pipe (4, 6; 8, 10) able to slide telescopically in relation to the first pipe (2) between a retracted position and an extended position.

Abstract: The invention relates to a device for holding an insulating blanket and for fastening systems in an aircraft, comprising a base having two ends from each of which an arm extends. At least one arm has a U-shaped part having two more or less parallel branches, and in that the said device further comprises at least one support for accommodating a system. The invention also relates to an aircraft fuselage section comprising frames, an outer skin, stabilizers and at least one insulating blanket. This section comprises at least one holding device such as described above, mounted so that a frame is situated between the arms of the holding device so that the blanket is between the frame and the holding device.