A method of determining parameters that are characteristics of the operation of a vehicle having a power plant with at least one engine and mechanical transmission means, sensors, and display means. During the method, various items of information about the aircraft, its state and/or its operation and/or its environment are measured, and then, for at least one parameter Pi relating to the state and the operation of the aircraft there are determined a first limit value Pi_lim for the parameter Pi, a second value Pi_X for each parameter Pi to enable the aircraft to perform a predetermined maneuver X, and an instantaneous third value Pi_inst for each parameter Pi. Thereafter, each first, second, and third values Pi_lim, Pi_X, Pi_inst is displayed simultaneously in order to show up the relative position of second and third values Pi_X and Pi_inst relative to a first value Pi_lim for each parameter Pi.
PROCEDE ET DISPOSITIF DE DETERMINATION ET D'OPTIMISATION DE PARAMETRES CARACTERISTIQUES DU FONCTIONNEMENT D'UN AERONEF A VOILURE TOURNANTE
A METHOD AND A DEVICE FOR DETERMINING AND OPTIMIZING PARAMETERS THAT ARE CHARACTERISTIC OF THE OPERATION OF A ROTARY WING AIRCRAFT
VERFAHREN UND VORRICHTUNG ZUR BESTIMMUNG UND OPTIMIERUNG VON KENNWERTEN DER BETRIEBSFUNKTION EINES DREHFLÜGELFLUGZEUGS
22.08.2018
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte |
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