Abstract: This invention proposes an insulation blanket for an aircraft, the said blanket coming in the form of a strip of insulation material of elongated shape having two more or less parallel longitudinal edges (12). This blanket comprises: at least one bar (14) extending over one face of the insulation blanket (6), from one longitudinal edge (12) to the other thereof, as well as means for holding (18) the said bar (14), and the bar (14) bears at least one system support intended to receive a system (30, 32).

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 for an aircraft including aircraft frames, a skin, and connecting pieces between the skin and the frames, the connecting pieces including clips, includes two brackets and a member that contours at least a portion of one of the aircraft frames. Each bracket has a first branch configured to be fastened to one of the clips and a second branch provided with a slot. The member that contours at least a portion of one of the aircraft frames includes a base and two arms. Each arm has a free end forming a securing lug configured to be inserted into the slot of one of the brackets with a flange which forms a stop countering displacement of the securing lug once the latter is inserted into the slot. Each arm further includes at least one support configured to accommodate a system.

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 invention proposes an insulation blanket for an aircraft, the said blanket coming in the form of a strip of insulation material of elongated shape having two more or less parallel longitudinal edges (12). This blanket comprises: at least one bar (14) extending over one face of the insulation blanket (6), from one longitudinal edge (12) to the other thereof, as well as means for holding (18) the said bar (14), and the bar (14) bears at least one system support intended to receive a system (30, 32).

Abstract: This device is intended for an aircraft comprising frames, a skin and connecting pieces between the skin and the frames, referred to as clips. It comprises: two brackets (30), each bracket having a first branch (32) intended to be fastened to a clip of the aircraft and a second branch (34) provided with a slot (36), a stirrup-shaped clip (1) comprising a base (2) and two arms (4, 6), each arm (4, 6) having at its free end a securing lug (17) adapted for being able to be inserted in the slot (36) of one of the said brackets with a flange (19) that forms a stop countering displacement of the securing lug once the latter is inserted into the said slot, each arm (4, 6) further comprising at least one support (14, 22) for accommodating a system.