The present invention includes an aircraft drive system (200) comprising a main rotor gearbox (214) comprising a first and a second input; a first drive system comprising a first engine reduction gearbox (216a) connecting a first engine to the first input of the main rotor gearbox (214) at a reduced shaft speed; and a second drive system independent from and redundant with the first drive system, the second drive system comprising a second engine reduction gearbox (216b) connecting a second engine to the second input of the main rotor gearbox (214) at the reduced shaft speed.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT DRIVE SYSTEM


    Additional title:

    FLUGZEUGANTRIEBSSYSTEM
    SYSTÈME DE TRANSMISSION POUR AÉRONEF


    Contributors:

    Publication date :

    2022-07-27


    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 / F16H Getriebe , GEARING



    AIRCRAFT DRIVE SYSTEM

    BACHMANN CHRISTIAN / BERGMANN DOMINIK / MARKMANN HOLGER | European Patent Office | 2021

    Free access

    Aircraft drive system

    BACHMANN CHRISTIAN / BERGMANN DOMINIK / MARKMANN HOLGER | European Patent Office | 2023

    Free access

    AIRCRAFT DRIVE SYSTEM

    POSTER SCOTT DAVID / RILEY WALTER / COPE GARY et al. | European Patent Office | 2020

    Free access

    AIRCRAFT DRIVE SYSTEM

    BACHMANN CHRISTIAN / BERGMAN DAVID / MARKMANN HOLGER | European Patent Office | 2021

    Free access

    Aircraft Drive System

    POSTER SCOTT DAVID / RILEY WALTER / COPE GARY et al. | European Patent Office | 2018

    Free access