Airbus Operations (s.a.s.)

Airbus Deutschland Gmbh

Airbus Corporation

Aerospatiale Societe Nationale Industrielle

Airbus Societe Par Actions Simplifiees

Zecools Zeolite Cooling Systme

Airbus Operations Gmbh

Airbus (sas)

Zecools Zeolite Cooling System

Bruno Alquier

Gérard Millet

Bruno Saint-Jalmes

Jason Zaneboni

Bernard Rumeau

Lars Rowold

Bodo Wisch

Martin Geldien

Luc Leroy

Thomas Menage

Olaf Von Wieding

Paul Devienne

Olivier Belou

Thierry Martin

Jerome Javelle

Joachim Voelkner

Clément Rivera

Bertrand Halphen

Roland Tevels

Jérôme Javelle

A drain configured to evacuate leaks of fluid, such as fuel, from a leak collecting system of an aircraft, the drain comprising a rigid tube secured to a plate, the plate being configured to be attached to an external wall of the aircraft, a flexible pipe configured to join the collecting system to the rigid tube, one end of the flexible pipe being received within the rigid tube. The rigid tube comprises a channel, the channel being configured to allow separation of the rigid tube from the plate at the location of the channel.

Drain configured to evacuate leaks of fluid, such as fuel, from a leak collecting system of an aircraft, and associated aircraft

A connection comprising a first duct, a second duct, a flexible tube which comprises a first end configured to cover part of the first duct, and a second end configured to cover part of the second duct, a first clamping system configured to clamp the first end of the flexible tube around the first duct, and a second clamping system configured to clamp the second end of the flexible tube around the second duct.

Connection device comprising a flexible tube for collection of a liquid in the event of leakage or oozing

A support for a pipe which comprises a body which comprises a through-orifice for the pipe. The through-orifice has a diameter which is greater than an external diameter of the pipe. At least one base of the support is configured so as to be in contact with and connected to a fixing surface. A first ring and a second ring each have an eccentric orifice and are configured so as to be fitted one into the other in the orifice of the body about the pipe when the support is put in position. By rotating at least one of the first and second rings, the position of the axis of the pipe may be adjusted radially relative to the support.

Support for a conduit

A front portion of a fuselage of an aircraft including a cockpit, a washroom, an access corridor to the cockpit alongside the washroom, and a rest compartment with at least one berth for at least one pilot. The corridor alongside the washroom includes a mechanism separating the corridor from the cockpit and a door for blocking access to the passenger cabin. The rest compartment can be accessed from the access corridor to the cockpit, between the separation mechanism between the corridor and the cockpit and the corridor door. The washroom includes two access doors, a first access door for accessing the washroom from the access corridor to the cockpit in the area located between the separation mechanism between the corridor and the cockpit and the corridor door, and a second access door for accessing the washroom from the passenger cabin.

Front portion for an aircraft including a rest compartment for at least one pilot

This device is provided for a luggage compartment designed to be placed overhead. The compartment comprises a mobile part () between an open position and a closed position and a mechanism for acting on said mobile part () to promote its closing. Said mobile part () presents an opening () designed for introducing and retrieving luggage as well as a lower exterior surface (). The control device comprises detection means reacting when pressure is exerted on a predetermined zone of the lower exterior surface () of the mobile part () as well as for sending a control signal to the mechanism acting on the mobile part () to close the part when pressure is exerted on said detection means. The detection means are disposed at the lower exterior surface () of the mobile part ().

Luggage compartment actuation

Refrigerated trolley for an aircraft. According to the invention:

Process for keeping chilled the food on board aircraft and means for implementing

A system for providing an emergency exit in a wall of an aircraft includes a pyrotechnic device disposed against the wall, and capable of cutting a desired opening in the wall, an igniter for the pyrotechnic device, a controller for the igniter, and a manometric safety device which receives the pressures inside and outside the aircraft and inhibits the action of the igniter when the difference between the pressures inside and outside the aircraft is greater than a predetermined value.

Pyrotechnic system for providing an emergency exit in an aircraft

Growing community of inventors

Blagnac, France

Bruno Alquier