Airbus Operations (s.a.s.)

Airbus (sas)

Airbus Operations Gmbh

Airbus Operations Sl

Airbus Corporation

Julien Laverne

Thomas Deforet

Kotaro Fukasaku

Jérôme Milliere

Nicholas West

Alistair Forbes

Emmanuel Vardelle

Jonathan Landolt

Bruno Estebe

Andrew Booth

Thomas Andrieu

Frédéric Sick

Thomas Wesoly

A device for connection of double-wall pipes including an interior connection system connecting the first and second interior pipes and an exterior connection system including a first part that cooperates with an end section of the first exterior pipe and a second part that cooperates with an end section of the second exterior pipe. The exterior connection system is configured so that at a first temperature at least one of the first and second parts exerts a contact force on the end section of the corresponding first or second exterior pipe greater than at a second temperature higher than the first temperature.

Device for connection of two double-wall pipes and hydrogen line including said connection device

A tank system comprising a tank, a drainage line fixed in the bottom part of the tank and having a drainage port at each end and, for each drainage port, a funnel having a wall through which at least one window passes, a body that can move in translation, for each funnel, a plug that is secured to the body and arranged to be able to move inside said funnel between an open position and a closed position, and an arm, a first end of which is mounted in an articulated manner to the top part of the tank and a second end of which is mounted in an articulated manner on the body.

Tank system with a valve in the form of a pendulum system

An aircraft comprising a fuselage, first and second wings positioned on either side of the fuselage, wherein each wing includes an inner part connected to the fuselage and an outer part continuing the inner part, the end of each inner part connected to the fuselage having a height greater than half the height of the fuselage and extending over a length greater than or equal to half of a distance separating the nose and the tail of the fuselage.

Aircraft comprising a fuselage and wings each having an outer part and a widened inner part between the fuselage and the outer part

A tank suitable for storing a product at a cryogenic temperature, including a fluid tight interior barrier, a fluid tight exterior barrier, surrounding the first interior barrier, an intermediary volume interposed between the interior and exterior barriers and at least one insulating layer positioned in the intermediary volume and including at least one thermal insulation mat, with very low thermal conductivity. The intermediary volume contains microspheres outside of the thermal insulation mats and has an enhanced level of vacuum. This solution makes it possible to maintain satisfactory performance in terms of thermal insulation even in the event of a loss of vacuum in the intermediary volume.

Tank having enhanced insulation combining thermal insulation mats with microspheres, and method of manufacturing such a tank

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Toulouse, France

Julien Laverne