Airbus Operations (s.a.s.)

Airbus Operations Gmbh

Lionel Sabadie

Marc Tomasi

Christian Banis

Michel Dal-Cin

Jean-Claude Briois

Didier Reynes

Laurent Rebolloso

Laurent Bertandeau

Maximilien Fauvet

Natalia Gracheva

Romain Durand

Thomas Bernabe

Guillaume Courtin

Jean Claude Briois

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.

Aircraft ventilation system

The invention relates to a device for fastening systems in an aircraft. It comprises on the one hand a ring-shaped base () and on the other hand arms () borne by the ring-shaped base (), extending outward from the latter and bearing systems supports.

Device for fastening systems for an aircraft, adapted in particular to be used in relation to a window

A device for interior covering of an aircraft cabin, intended to be fastened to a structure of an aircraft and to extend along a skin of the aircraft, the device comprising a covering panel. The covering panel bears at least one system, possibly through a system support. It advantageously comprises at least one air circulation pipe fastened to an exterior face of the covering panel, each air pipe having an upstream end equipped with a connection device.

Interior covering device for an aircraft cabin incorporating at least one system

The invention relates to a device for holding an insulating blanket and for fastening systems in an aircraft, comprising a base having two ends from each of which an arm extends. At least one arm has a U-shaped part having two more or less parallel branches, and in that the said device further comprises at least one support for accommodating a system. The invention also relates to an aircraft fuselage section comprising frames, an outer skin, stabilizers and at least one insulating blanket. This section comprises at least one holding device such as described above, mounted so that a frame is situated between the arms of the holding device so that the blanket is between the frame and the holding device.

Fixation mechanism for installing thermal insulation sheets in an aircraft body

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

Growing community of inventors

Toulouse, France

Lionel Sabadie