Airbus Operations (s.a.s.)

Airbus (sas)

Philippe Perrin

Matthias Eberle

Patrice Rouquette

Jerôme Bazile

Manfred Birnfeld

Jean-Philippe Cottet

Hubert Patris

Stephan Ducarroir

A method and device for assisting initiation of a flare maneuver of an aircraft during a landing. The device includes an acquisition unit for acquiring current values of flight parameters of the aircraft, including the current height of the aircraft with respect to the ground, a computation unit for computing a first reference height and a second reference height, corresponding to a height starting from which the aircraft attains a current start of flare height while maintaining its current descent conditions over a predetermined first duration and over a predetermined second duration respectively, and an acoustic emission unit for emitting at least two sound signals in the cockpit of the aircraft, namely a first sound signal when the current height of the aircraft attains the first reference height during the descent and a second sound signal when the current height of the aircraft attains the second reference height during descent.

Method and device for assisting the intiation of a flare maneuver of an aircraft during a landing of the aircraft

A device for assisting in the landing of an aircraft in a flare phase comprising a control stick, a first unit for acquiring current flight parameters of the aircraft, a second unit for acquiring a current deflection angle of the control stick, a computation unit for computing a difference between the current deflection angle of the control stick and a target deflection angle of the control stick, and an acoustic emission unit configured to automatically emit a warning or guidance sound signal in the cockpit of the aircraft, according to the difference between the current deflection angle and the target deflection angle of the control stick.

Method and device for assisting in the landing of an aircraft in a flare phase

A method and device for aiding the monitoring of a turbine engine of an aircraft, which displays on one and the same indicator of a of a display indication elements illustrating as a percentage the engine start progression or the current sub-idle state of the turbine engine, a margin to a limit temperature of the turbine engine, a margin to a maximum temperature of the turbine engine and a margin to a possible failure of the start that is generated by a too low speed increase of the turbine engine.

Method and device for aiding the monitoring of a turbine engine of an aircraft

Growing community of inventors

Toulouse, France

Philippe Perrin