A starting/generating system for an aircraft turbine engine, the starting/generating system comprising at least one brushless drive motor/generator, at least one control module and at least one power module, the power module being configured to supply/receive electric power from the brushless drive motor/generator, the control module being connected to the brushless drive motor/generator by a control cable in order to control its operation, in which system the power module is configured to be mounted in the housing of the non-pressurized zone so as to be located adjacent to the brushless drive motor/generator and the control module is configured to be mounted in a pressurized zone of the aircraft, the control module being connected to the power module by a two-way communication cable in order to control its operation.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Starting/generating system and method for an aircraft turbine engine


    Beteiligte:

    Erscheinungsdatum :

    2023-05-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



    STARTING/GENERATING SYSTEM AND METHOD FOR AN AIRCRAFT TURBINE ENGINE

    LAPALUS PHILIPPE / NIERLICH FLORENT | Europäisches Patentamt | 2021

    Freier Zugriff

    Hybrid aircraft turbine engine starting system and method

    JENSEN CHRIS L / OMOHUNDRO THOMAS W | Europäisches Patentamt | 2020

    Freier Zugriff

    HYBRID AIRCRAFT TURBINE ENGINE STARTING SYSTEM AND METHOD

    JENSEN CHRIS L / OMOHUNDRO THOMAS W | Europäisches Patentamt | 2017

    Freier Zugriff

    Turbine engine starting system

    KAHN WILLIAM C / POLANSKY STEVE J / WEHRWEIN CHRISTOPHER G | Europäisches Patentamt | 2016

    Freier Zugriff

    Aircraft starting and generating system

    HUANG HAO | Europäisches Patentamt | 2019

    Freier Zugriff