A system (100A, 100B) of a hybrid aircraft (10) includes a first gas turbine engine (20) including a fan (42), a high speed spool (32), and a low spool motor (12A) configured to drive rotation of the fan. The system also includes a second gas turbine engine (20) and a controller (256). The controller is operable to determine an operating mode of the hybrid aircraft, control the low spool motor (12A) to drive rotation of the fan of the first gas turbine engine (20) responsive to a thrust command (270) while the second gas turbine engine is driven by commanding fuel combustion based on the operating mode, and accelerate the high speed spool (32) of the first gas turbine engine (20) and command fuel combustion at the first gas turbine engine based on a transition of the operating mode to perform a starting operation of the first gas turbine engine.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ASYMMETRIC HYBRID AIRCRAFT IDLE


    Weitere Titelangaben:

    ASYMMETRISCHER HYBRIDER FLUGZEUGLEERLAUF
    RALENTI D'AÉRONEF HYBRIDE ASYMÉTRIQUE


    Beteiligte:

    Erscheinungsdatum :

    2023-08-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    Asymmeiric hybrid aircraft idle

    TERWILLIGER NEIL | Europäisches Patentamt | 2023

    Freier Zugriff

    HYBRID ELECTRIC IDLE TRANSITION FOR AIRCRAFT

    GREENBERG MICHAEL D / SMITH LANCE L / URBAN JUSTIN R | Europäisches Patentamt | 2022

    Freier Zugriff

    HYBRID ELECTRIC IDLE AND BRAKING FOR AN AIRCRAFT

    GILSON JONATHAN / BAIG ZUBAIR AHMED / AMARI MARTIN RICHARD et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT ENGINE IDLE SUPPRESSOR AND METHOD

    EPSTEIN ALAN H | Europäisches Patentamt | 2020

    Freier Zugriff

    Hybrid vehicle idle and creep control

    WANG XIAOYONG / YAMAZAKI MARK STEVEN / LIANG WEI et al. | Europäisches Patentamt | 2019

    Freier Zugriff