Methods and systems are provided for presenting an energy state associated with an aircraft with respect to an operating envelope region for a procedure to restart an engine of the aircraft. One method involves providing a graphical user interface display having a first reference axis corresponding to a first energy state parameter and a second reference axis corresponding to a second energy state parameter different from the first energy state parameter, providing a graphical representation of an operating envelope region associated with a procedure for starting an engine of the aircraft with respect to the first and second reference axes, obtaining current values for the first and second energy state parameters for the aircraft, and providing a graphical representation of the aircraft positioned with respect to the first and second reference axes based on the current values for the first and second energy state parameters.


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    Titel :

    ENGINE RELIGHT VISUALIZATION METHODS AND SYSTEMS


    Beteiligte:
    RAMACHANDRA SRIPATHI (Autor:in) / CARLUCCI GREG (Autor:in) / MUNDEL KAREL (Autor:in) / SNYDER RICHARD (Autor:in) / PEARSON MARK (Autor:in) / ANANTHRAM UDIPI RANGA (Autor:in) / AYYATHURAI PRAVEENKUMAR (Autor:in) / KAR SAMRAT (Autor:in)

    Erscheinungsdatum :

    2021-01-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



    Engine relight visualization methods and systems

    RAMACHANDRA SRIPATHI / CARLUCCI GREG / MUNDEL KAREL et al. | Europäisches Patentamt | 2022

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