DEVICE FOR ASSISTING WITH REGULATION OF PROPELLERS OF AERONAUTICAL TURBOMACHINERY

This control device for a propulsion system, which comprises means for computing a blade-pitch setpoint for at least one propeller of the propulsion system, the computing means using a predictive model of the performance of the propeller that takes into account at least one flight speed so as to ada...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	GIANNAKAKIS, Panagiotis, YESILCIMEN, Henri, BINDER, Anthony
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINE PLANTS IN GENERAL HEATING HELICOPTERS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	This control device for a propulsion system, which comprises means for computing a blade-pitch setpoint for at least one propeller of the propulsion system, the computing means using a predictive model of the performance of the propeller that takes into account at least one flight speed so as to adapt a blade-pitch angle setpoint, is characterized in that the predictive model of the performance of the propeller is configured to use polar curves implemented in the form of a mathematical law.