A system of a hybrid aircraft includes a first gas turbine engine, a second gas turbine engine, and a controller. The first gas turbine engine includes a first low spool electric machine (12A) and a first high spool electric machine (12B). The second gas turbine engine includes a second low spool electric machine (12A) and a second high spool electric machine (12B). The controller is operable to determine an operating mode of the hybrid aircraft and control power extraction from either or both of the first low spool electric machine (12A) and the first high spool electric machine (12B) while a single engine descent mode is active. Electric power is provided to either or both of the second low spool electric machine (12A) and the second high spool electric machine (12B) while the single engine descent mode is active to balance thrust between the first gas turbine engine and the second gas turbine engine.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    POWER EXTRACTION CONTROL FOR DESCENT IN A HYBRID ELECTRIC PROPULSION SYSTEM


    Weitere Titelangaben:

    LEISTUNGSEXTRAKTIONSSTEUERUNG FÜR DEN SINKFLUG EINER HYBRID-ELEKTRISCHEN ANTRIEBSSYSTEMS
    COMMANDE D'EXTRACTION DE PUISSANCE PENDANT DESCENTE D'UN SYSTÈME PROPULSIF HYBRIDE ÉLECTRIQUE


    Beteiligte:

    Erscheinungsdatum :

    2023-05-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen



    POWER CONTROL FOR DESCENT IN A HYBRID ELECTRIC PROPULSION SYSTEM

    AMARI MARTIN RICHARD / BAIG ZUBAIR AHMED | Europäisches Patentamt | 2023

    Freier Zugriff

    HYBRID ELECTRIC SINGLE ENGINE DESCENT POWER EXTRACTION CONTROL

    AMARI MARTIN RICHARD | Europäisches Patentamt | 2023

    Freier Zugriff

    POWER MANAGEMENT IN A HYBRID-ELECTRIC PROPULSION SYSTEM DURING SINGLE ENGINE FAILURE AT DESCENT

    BAIG ZUBAIR AHMED / DUSHEK MATT / AMARI MARTIN RICHARD | Europäisches Patentamt | 2023

    Freier Zugriff

    Descent operation for an aircraft parallel hybrid gas turbine electric propulsion system

    LENTS CHARLES E / HARDIN LARRY W / RHEAUME JONATHAN et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    DESCENT OPERATION FOR AN AIRCRAFT PARALLEL HYBRID GAS TURBINE ELECTRIC PROPULSION SYSTEM

    LENTS CHARLES E / HARDIN LARRY W / RHEAUME JONATHAN et al. | Europäisches Patentamt | 2018

    Freier Zugriff