A rotorcraft engine starting system includes a starting system controller 13 in communication with a flight control computer; an electric engine starter 9; an electronic engine controller 2 in communication with the electric engine starter; an electrical power distributor 8; and a plurality of power sources coupled to the electrical power distributor; the starting system controller selecting at least one of the plurality of power sources and instructing the electrical power distributor to use the at least one of the plurality of power sources to power the electric engine starter.


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    Title :

    Engine starting system for rotorcraft in flight


    Additional title:

    Motorstartsystem für Drehflügler im Flug
    Système de démarrage de moteur pour giravions en vol


    Contributors:

    Publication date :

    2018-11-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02N STARTING OF COMBUSTION ENGINES , Anlassen von Brennkraftmaschinen



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