A device supplying electricity power to and actuating equipments of a gas turbine airplane engine, including an electricity power supply circuit dedicated to the engine and distinct from an electricity network on board the plane and excitation, control or servo circuits for pieces of electrical equipment of the engine. The engine electrical power supply circuit includes a first bus distributing DC or AC voltage to excitation, control or servo circuits for first pieces of electrical equipment of the engine, a second bus distributing DC or AC voltage to excitation, control or servo circuits for other pieces of electrical equipment of the engine requiring higher electrical power compared with the first pieces of equipment, and a third bus connected to receive power from an electricity source such as an airplane on-board electricity distribution network or an electricity generator dedicated to the engine and driven thereby. The third bus supplies the first and second bus with electricity power.


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    Titel :

    ALIMENTATION ÉLECTRIQUE D'ÉQUIPEMENTS D'UN MOTEUR D'AVION À TURBINE À GAZ


    Weitere Titelangaben:

    ELECTRIC SUPPLY FOR AN AIRCRAFT GAS TURBINE ENGINE EQUIPMENT
    STROMVERSORGUNG FÜR EINE GASTURBINENTRIEBWERKANLAGE FÜR LUFTFAHRZEUGE


    Beteiligte:
    DUBOIS GILLES (Autor:in) / MEURET RÉGIS (Autor:in) / VERNOCHET MAURICE (Autor:in)

    Erscheinungsdatum :

    18.11.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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