ELECTRICAL GENERATION ARCHITECTURE FOR HYBRIDISED TURBOMACHINE

Electrical architecture for an aircraft with thermal/electrical hybrid propulsion, comprising, for each turbine engine:an aeroplane AC electrical network,at least one first electrical machine mechanically coupled to a high-pressure shaft of the turbine engine;at least one second electrical machine m...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	HADJIDJ, Djemouai
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES ELECTRICITY ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES PARACHUTES PERFORMING OPERATIONS SYSTEMS FOR STORING ELECTRIC ENERGY TRANSPORTING VEHICLES IN GENERAL
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	Electrical architecture for an aircraft with thermal/electrical hybrid propulsion, comprising, for each turbine engine:an aeroplane AC electrical network,at least one first electrical machine mechanically coupled to a high-pressure shaft of the turbine engine;at least one second electrical machine mechanically coupled to a low-pressure shaft of the turbine engine;a reversible AC/AC electrical energy conversion module;switch elements; andan electronic system for controlling the conversion module and the switch elements, configured to put the architecture;in at least one so-called "power distribution hybridisation" operating mode corresponding to a first configuration of the switch elements in which the at least one second machine is coupled to the aeroplane network and at least one first machine is coupled to the aeroplane network via the electrical energy conversion module.