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 mounting device for aircraft supply systems comprises a cross member and at least one support module including a body having a shape complementary to that of a cross member. The body includes a structure for securing an aircraft supply system, an opening, and a pin, wherein the opening forms a guide that is able to receive a portion of the pin. The cross member includes grooves that are regularly spaced apart in the direction of elongation of said cross member. The pin has a shape complementary to that of the grooves and has a lip transverse to the direction of elongation of the pin. The support module is anchored to the cross member by the pin being inserted into the opening, the pin engaging with one of the grooves, as far as an anchoring position in which the lip is in contact with the support module.

Abstract: A mounting device for aircraft supply systems comprises a cross member and at least one support module including a body having a shape complementary to that of a cross member. The body includes a structure for securing an aircraft supply system, an opening, and a pin, wherein the opening forms a guide that is able to receive a portion of the pin. The cross member includes grooves that are regularly spaced apart in the direction of elongation of said cross member. The pin has a shape complementary to that of the grooves and has a lip transverse to the direction of elongation of the pin. The support module is anchored to the cross member by the pin being inserted into the opening, the pin engaging with one of the grooves, as far as an anchoring position in which the lip is in contact with the support module.

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: 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.