Airbus Operations (s.a.s.)

Airbus Operations Gmbh

Alexandre Broquet

Fabien Pascal

Yannick Deleris

Fabien Cases

Frank Klimpel

Alexander Solntsev

Holger Bammann

Nicolas Caule

Michel Colin

Pierre Campagne

Raphael Andre

Nicolas Marty

A ram air channel arrangement for ambient air supply into an aircraft comprises a ram air channel which has a ram air inlet channel and a ram air outlet channel arranged downstream of the ram air inlet channel and in fluid communication with the ram air inlet channel. The ram air channel arrangement further comprises a cabin exhaust air line which is adapted to have cabin exhaust air flow therethrough which has been removed from an aircraft cabin and which cabin exhaust air line is connected to the ram air inlet channel and is adapted to lead the cabin exhaust air into the ram air inlet channel.

Ram air channel arrangement and method for operating a ram air channel arrangement

The invention relates to a device aboard an aircraft comprising output means configured to restore information relating to the aircraft status from aircraft systems, the device including a module providing interface between said output means and said aircraft systems, said module being configured to synthesize information from aircraft systems depending on predetermined behavior rules and to transmit said information thus synthesized to said output means.

System aboard an aircraft

A method and a device for managing information in an aircraft, including at least one device for outputting information for the crew and a plurality of equipment items adapted to transmit information items capable of being outputted on the output device. After a plurality of information items from the plurality of equipment items has been acquired and a context has been determined according to a predetermined model, the plurality of information items is filtered according to at least one rule, the at least one rule being associated with the context for selection of at least one information item. At least one selected information item is then outputted on the output device.

Method and device for managing information in an aircraft

The present invention relates to a system () and an associated method for managing audio warning messages in an aircraft. The system () comprises a plurality of monitoring systems () capable of detecting the establishment of at least one warning condition (CA), and comprises a central broadcasting module (), to which each of the monitoring systems is connected and which is capable of broadcasting an audio message (SIG) corresponding to a detected warning condition. In particular, in this system (), the said central broadcasting module () comprises means () for determining at least one priority warning condition among the warning conditions detected by the monitoring systems, and means () for generating at least one audio message (SIG) corresponding to the at least one determined priority warning condition, in order to broadcast it.

System and method for managing audio warning messages in an aircraft

In the method of controlling an aircraft, a device implements the steps consisting in determining a first global value on the basis of only some amongst first individual values calculated by respective applications, modifying at least one parameter to take account of how the determination step took place and determining a second global value on the basis of second individual values calculated by the respective applications and on the basis of the parameter(s).

Method of controlling an aircraft, the method implementing a vote system

A method and a device for detecting a thrust dissymmetry of an aircraft during a landing are disclosed. The detection device () comprises means () for detecting, upon a landing, that at least one of the engine control levers occupies an intermediary position comprised between a position threshold and a maximum speed position, as well as at least another engine control lever occupies an idling position, and means () for triggering a warning when a landing condition is validated and at least one of the control levers occupies said intermediary position, at least another control lever occupying said idling position.

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Toulouse, France

Alexandre Broquet