A method of assisting the piloting of an aircraft, such as a helicopter, includes determining a limiting power margin of a power plant of the aircraft relative to a power limit at an operating rating of an engine of the power plant. The limiting power margin is transformed into a collective pitch margin for the operating rating. The collective pitch margin represents the margin between a current collective pitch of blades of a main rotor of the aircraft and a collective pitch limit of the blades of the main rotor. The collective pitch limit is determined and then displayed on a display of the aircraft for a pilot to view.
PROCÉDÉ, DISPOSITIF D'AIDE AU PILOTAGE D'UN AÉRONEF, ET AÉRONEF
A METHOD AND A DEVICE FOR ASSISTING THE PILOTING OF AN AIRCRAFT, AND AN AIRCRAFT
VERFAHREN UND HILFSVORRICHTUNG ZUR STEUERUNG EINES LUFTFAHRZEUGS, UND LUFTFAHRZEUG
26.09.2018
Patent
Elektronische Ressource
Französisch
PROCEDE, DISPOSITIF D'AIDE AU PILOTAGE D'UN AERONEF, ET AERONEF
Europäisches Patentamt | 2019
|PROCEDE ET DISPOSITIF D'AIDE AU PILOTAGE D'UN AERONEF
Europäisches Patentamt | 2021
|Procédé et dispositif d’aide au pilotage d’un aéronef
Europäisches Patentamt | 2021
|Europäisches Patentamt | 2021
|