Airbus Operations (s.a.s.)

Airbus Corporation

Airbus (sas)

Airbus France

Pierre Campagne

Baptiste Maylin

Boris Sorbier

Alexandre Broquet

Jerome Treanton

Fabien Daveze

Xavier Geay

Christophe Jotz

Thierry Paya-Arnaud

Jerome Pouyfaucon

Nicolas Marty

Christel Ravier

Laval Louis Chan Kam Fai

A process for managing the activating of emission of a given warning message in an aircraft comprises transmission, from a monitoring system to an authorization-issuing system, of an emission authorization request. The request has a priority attribute known as request priority attribute. The process also includes transmission, from the authorization-issuing system to the monitoring system, of an emission authorization. The transmission of the emission authorization is effected if the request priority attribute is higher than a current priority threshold. In addition, the process includes activation of emission of the given warning message. The activation may be effected if an alert condition associated with the given warning message is detected and if a priority attribute associated with the alert condition is higher than or equal to the request priority attribute.

Process and device for managing the activating of a warning message in an aircraft

A method and a device for accessing the documentation of an aircraft according to alarms generated therein, where the documentation includes at least one document that is modifiable independently of the manufacturer of the aircraft. After having received at least one indication relating to at least one alarm generated by the avionics of the aircraft, at least one datum relating to the at least one alarm, including a link to at least one element of the documentation, is extracted and displayed.

Method and device for accessing the documentation of an aircraft according to alarms generated therein

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.

Method and a device for detecting a thrust dissymmetry of an aircraft during landing

A method for managing an interruption of emission, in an aircraft, of an acoustic message including an information item about a state of part of the said aircraft and/or about its environment, wherein the acoustic message is structured into one or more successive acoustic fragments each representative of the information item, the method includes the steps of: delaying, starting from a given moment, the execution of a decision to interrupt the emission of the acoustic message until the end of emission of an acoustic fragment that is in the course of emission at the given moment; and executing the interruption decision.

Process and system for managing an interruption of a broadcast of a sonorous message in an aircraft

The invention relates to a method for producing an audible warning when an aircraft autopilot is deactivated. The method includes a) transmitting a first sound in the aircraft cockpit during a time ranging from a first predetermined value and a second predetermined value and b) transmitting a second sound in the aircraft cockpit. The invention also relates to an audible warning device having a monitoring unit for monitoring the deactivation of the aircraft autopilot and an activation unit for emitting an audible warning in the cockpit, where the activation unit is constructed such that it activates the first sound emission whose length ranges from the first predetermined value and a second predetermined value and a second sound when the monitoring unit detects the deactivation of the autopilot.

Method and device for audible warning when an aircraft autopilot is deactivated

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Toulouse, France

Pierre Campagne