Airbus Operations (s.a.s.)

Airbus Operations Gmbh

Laurent Rebolloso

Luc Michelet

Michel Dal-Cin

Maximilien Fauvet

Didier Reynes

Marc Tomasi

Lionel Sabadie

Julie Holvoet

Davide Faggella

Benjamin Lafont

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 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.

Mounting device for aircraft supply systems

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 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.

Device for holding an insulating blanket and for fastening two-parts systems

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Le Gres, France

Laurent Rebolloso