A hybrid electric propulsion (HEP) system of an aircraft includes a gas turbine engine configured to generate rotational power, and an electric propulsion system configured to generate at least one of thrust or lift for operation of the aircraft. The propulsion system includes a propulsor and an electric motor configured to drive the propulsor. A controller is in signal communication with the gas turbine engine and the electric propulsion system. The controller operates the gas turbine engine based on an on-board engine model (OEM), monitors electrical parameters of the electric propulsion system, and updates the OEM in response to changes to the electrical parameters.


    Access

    Download


    Export, share and cite



    Title :

    OVERALL AIRCRAFT SYSTEM DATA COLLECTOR FOR PROGNOSTICS AND HEALTH MANAGEMENT


    Contributors:
    AMARI MARTIN (author) / WU XIN (author) / HAYES TYLER W (author)

    Publication date :

    2024-10-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    OVERALL AIRCRAFT SYSTEM DATA COLLECTOR FOR PROGNOSTICS AND HEALTH MANAGEMENT

    AMARI MARTIN / WU XIN / HAYES TYLER W | European Patent Office | 2024

    Free access

    Aircraft Prognostics Health System

    CONRAD KEVIN | European Patent Office | 2015

    Free access

    Aircraft prognostics health system

    CONRAD KEVIN | European Patent Office | 2017

    Free access

    Aircraft prognostics health system

    CONRAD KEVIN | European Patent Office | 2017

    Free access

    Aircraft Prognostics Health System

    CONRAD KEVIN | European Patent Office | 2015

    Free access