A system for automated management of in-flight restarting of engines of an aircraft includes controllers, each engine of the aircraft being managed by one of the controllers. A controller that detects an engine that has stopped: cuts off the energy supply of the engine and performs a windmill engine start. If at least one other engine has stopped, prioritization of engine restarting includes: collecting information concerning a state of health of each engine; determining from the information collected information representing a probability of restarting each stopped engine; determining a sequential order of restarting the stopped engines as a function of information representing the probability of restarting each stopped engine. Each stopped engine continues to be windmill started until selection of the engine in question in the sequential order of restarting the stopped engines. Thus, the operational status of the aircraft is improved as quickly as possible.


    Access

    Download


    Export, share and cite



    Title :

    Restarting a plurality of engines of an aircraft



    Publication date :

    2024-08-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Restarting multiple engines of in-flight aircraft

    CONTE CHARLES / FRAMONT-BARTI QUENTIN-ANNE / COLAS XAVIER et al. | European Patent Office | 2022

    Free access

    RESTARTING METHOD FOR RESTARTING A MOTOR VEHICLE

    VYVET LAURENT / KOUBASSI MARYAM | European Patent Office | 2024

    Free access

    RESTARTING DEVICE

    OGAWA HIRONARI | European Patent Office | 2019

    Free access

    Aircraft with a plurality of engines driving a common driveshaft

    SMITH FRICK A | European Patent Office | 2017

    Free access

    Aircraft With A Plurality Of Engines Driving A Common Driveshaft

    SMITH FRICK A | European Patent Office | 2016

    Free access