Airbus Operations (s.a.s.)

Aerospatiale Societe Nationale Industrielle

Airbus Operations Gmbh

Luc Michelet

Laurent Rebolloso

Julie Holvoet

Matthieu De Kergommeaux

Didier Reynes

Marc Tomasi

Davide Faggella

Jean-Claude Briois

Benjamin Lafont

Maximilien Fauvet

Michel Eugene

Etienne Gustin

Adrien Pique

Tyron Billington

Philippe Bodin

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.

Double clamping collar fixing system

A tubular element bracket comprises at least one central body elongate along a longitudinal axis, comprising a central portion elongate along the longitudinal axis and a support element configured to receive at least one tubular element, the support element being arranged at one end of the central body, referred to as the upper end, and a fixing plate configured to be fixed to a support, notably of an aircraft. The central portion and the support element are formed in one piece. The support element is in the form of an open fixing collar. The bracket comprises a fixing arrangement configured to make it possible to fix the central body manually and autonomously to the fixing plate by its other end, referred to as the lower end.

Bracket for tubular element, in particular for aircraft

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.

Installation assembly including a fixation rail for attaching devices in an aircraft

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.

Device for holding an insulating blanket and for fastening systems adapted to be mounted in an aircraft

Portions of a sound and thermic insulation mattress are modified so as to retain the water imperviousness of the mattress and its insulation characteristics when it is secured to a support. The mattress is provided with an opening therein and a foam insert arranged in the opening and provided with an orifice. The insert is held in the opening by an adhesive strip which is glued to the foam insert and the mattress.

Sound and thermic insulation mattress having a foam insert for securing

Growing community of inventors

Cornebarrieu, France

Luc Michelet