Abstract: A fixing system allowing an element that is to be supported to be fixed to a support element. The fixing system comprises a first fixing element configured to be positioned and fixed on the support element and having a cylindrical exterior surface, a clamping collar configured to be positioned on the element that is to be supported, a connecting piece comprising a first part configured to conform to the shape of the exterior surface and a second part, a first securing arrangement configured to secure the first part and the fixing element, and a second securing arrangement configured to secure the second part and the clamping collar while at the same time allowing the clamping collar to rotate about an axis of rotation. Such a fixing system allows easy installation of the various constituent elements at the time of assembly.

Abstract: A fixing system allowing an element that is to be supported to be fixed to a support element. The fixing system comprises a first fixing element configured to be positioned and fixed on the support element and having a cylindrical exterior surface, a clamping collar configured to be positioned on the element that is to be supported, a connecting piece comprising a first part configured to conform to the shape of the exterior surface and a second part, a first securing arrangement configured to secure the first part and the fixing element, and a second securing arrangement configured to secure the second part and the clamping collar while at the same time allowing the clamping collar to rotate about an axis of rotation. Such a fixing system allows easy installation of the various constituent elements at the time of assembly.

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 fastening assembly for the fastening of systems in an aircraft comprising frames, a skin, and clips between the skin and the frames. The fastening assembly includes: ramps, that extend between two consecutive frames of the aircraft; brackets for fastening the ramps to two of the clips situated respectively on two consecutive frames of the aircraft; system supports, fastened to the ramps, each system support being able to receive at least one system.

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: The invention relates to a fastening assembly for the fastening of systems in an aircraft comprising frames (104), a skin (102) and connecting parts between the skin and the frames, referred to as clips (106), comprising: ramps (2), each ramp being adapted for extending between two consecutive frames of the aircraft; for each ramp, means (4) for fastening the ramp allowing fastening of the said ramp to two clips (106) situated respectively on two consecutive frames of the aircraft, system supports (18, 34), fastened or adapted for being fastened to the ramps, each system support being able to receive at least one system.

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.