A system of a hybrid aircraft (10) includes a first gas turbine engine (20A), a second gas turbine engine (20B), a power source (16), and a controller. The first gas turbine engine (20A) includes a first electric machine (12B). The second gas turbine engine (20B) includes a second electric machine (12B). The controller is operable to determine an operating condition of the first gas turbine engine (20A) and the second gas turbine engine (20B) and to detect a change in a thrust command for the hybrid aircraft (10). The controller is further operable to determine an adjustment to the second electric machine (12B) to compensate for the change in the thrust command while the first gas turbine engine (20A) is operating in a fuel-driven mode and the second gas turbine engine (20B) is operating in an electrically-driven mode. At least a portion of electric power to perform the adjustment to the second electric machine (12B) is extracted from the power source (16).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    POWER CONTROL FOR DESCENT IN A HYBRID ELECTRIC PROPULSION SYSTEM


    Weitere Titelangaben:

    HYBRIDE ELEKTRISCHES ANTRIEBSENERGIEVETEILUNG FÜR SINKFLUG
    GESTION D'ÉNERGIE DE DESCENTE DE 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 EXTRACTION CONTROL FOR DESCENT IN A HYBRID ELECTRIC PROPULSION SYSTEM

    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

    HYBRID ELECTRIC SINGLE ENGINE DESCENT POWER EXTRACTION CONTROL

    AMARI MARTIN RICHARD | Europäisches Patentamt | 2023

    Freier Zugriff