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: The invention relates to a device for fastening systems in an aircraft. It comprises on the one hand a ring-shaped base (2) and on the other hand arms (4, 6) borne by the ring-shaped base (2), extending outward from the latter and bearing systems supports.

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: A device for holding an insulating blanket and for fastening systems in an aircraft includes a base and at least one support. The base has two ends from each of which there extends an arm. One arm is a jointed arm that is jointed onto the base to be pivotable relative to the base. The at least one support is configured to accommodate a system. The base includes an elongated shape and defines a plane, the base includes two longitudinal edges, and at one end of the base, each longitudinal edge has a flange extending from the base on a same side of the base from which the arms extend.

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 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: The invention relates to a device for fastening systems in an aircraft. It comprises on the one hand a ring-shaped base (2) and on the other hand arms (4, 6) borne by the ring-shaped base (2), extending outward from the latter and bearing systems supports.

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: This device for holding an insulating blanket and for fastening systems in an aircraft comprises a base (2) having two ends from each of which there extends an arm (4, 6). The base (2) of elongated shape defines a plane, referred to as reference plane, comprising two longitudinal edges (8), and at one end of the base (2), each longitudinal edge (8) has a flange (38) extending from the base (2) on the same side as arms (4, 6). An arm (6) is jointed onto the base (2). The said device further comprises at least one support (46, 54) for accommodating a system.