Method for controlling energy setting of hybrid propulsion system

The invention relates to a method (200) for controlling a system for generating and controlling power in an aircraft, the system comprising:-a hybrid propulsion system comprising an electrical network and a propulsion energy source,-at least one non-propulsion energy source,-a hybrid propulsion syst...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	DOS SANTOS VICTOR, BIDAN GUILLAUME FRANCOIS DANIEL, HUMMEL ANNA TRUC, BONHOMME DAMIEN JACQUES ARTHUR
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	The invention relates to a method (200) for controlling a system for generating and controlling power in an aircraft, the system comprising:-a hybrid propulsion system comprising an electrical network and a propulsion energy source,-at least one non-propulsion energy source,-a hybrid propulsion system control unit, and-an aircraft total power control unit, the method is characterized in that it comprises:-determining an operability limit of the propulsion energy source,-monitoring (220) the operability of the propulsion energy source using the hybrid propulsion system control unit, and-controlling (220) the propulsion energy source when the operability of the propulsion energy source is below the determined operability limit. The power generated by the propulsion energy source is controlled (232) using an aircraft total power control unit, or the power generated by the propulsion energy source is controlled (250) using a hybrid propulsion system control unit when the operability of the propulsion energy sourc