A rotorcraft engine starting system includes a starting system controller in communication with a flight control computer; an electric engine starter; an electronic engine controller in communication with the electric engine starter; an electrical power distributor; 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.


    Access

    Download


    Export, share and cite



    Title :

    Engine starting system for rotorcraft in flight



    Publication date :

    2016-02-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    Engine starting system for rotorcraft in flight

    SMILEY ALFRED RUSSEL / STRAUSS MICHAEL PETER / CYCON JAMES PETER | European Patent Office | 2018

    Free access

    CONTROL SYSTEM FOR ROTORCRAFT IN-FLIGHT ENGINE RESTARTING

    STRAUSS MICHAEL PETER / DEVITA MICHAEL JOSEPH / BYSTRY JR MARK DENTON et al. | European Patent Office | 2019

    Free access

    CONTROL SYSTEM FOR ROTORCRAFT IN-FLIGHT ENGINE RESTARTING

    STRAUSS MICHAEL PETER / DEVITA MICHAEL JOSEPH / BYSTRY JR MARK DENTON et al. | European Patent Office | 2018

    Free access

    Control system for rotorcraft in-flight engine restarting

    STRAUSS MICHAEL PETER / DEVITA MICHAEL JOSEPH / BYSTRY JR MARK DENTON et al. | European Patent Office | 2020

    Free access

    CONTROL SYSTEM FOR ROTORCRAFT IN-FLIGHT ENGINE RESTARTING

    STRAUSS MICHAEL PETER / DEVITA MICHAEL JOSEPH / BYSTRY JR MARK DENTON et al. | European Patent Office | 2017

    Free access