An aircraft landing gear wheel-drive system includes a first wheel drive unit for driving a first landing gear wheel of the aircraft and a second wheel drive unit for driving a second landing gear wheel of the aircraft. The first wheel drive unit has a first range of torque to speed (T/S) ratios. The second wheel drive unit has a second range of T/S ratios. The first range of T/S ratios is greater than the second range of T/S ratios.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft landing gear wheel-drive system


    Contributors:
    LO CHARLES (author) / STEVES ALLAN (author)

    Publication date :

    2017-04-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B60W CONJOINT CONTROL OF VEHICLE SUB-UNITS OF DIFFERENT TYPE OR DIFFERENT FUNCTION , Gemeinsame Steuerung oder Regelung von Fahrzeug-Unteraggregaten verschiedenen Typs oder verschiedener Funktion



    AIRCRAFT LANDING GEAR WHEEL-DRIVE SYSTEM

    LO CHARLES / STEVES ALLAN | European Patent Office | 2017

    Free access

    Aircraft landing gear drive wheel identification system

    JAN VANA / JOSEPH J COX / ISAIAH W COX et al. | European Patent Office | 2017

    Free access

    Aircraft Landing Gear Drive Wheel Identification System

    VANA JAN / COX JOSEPH J / COX ISAIAH W et al. | European Patent Office | 2016

    Free access

    Aircraft landing gear drive wheel identification system

    VANA JAN / COX JOSEPH J / COX ISAIAH W et al. | European Patent Office | 2017

    Free access

    AIRCRAFT LANDING GEAR WHEEL WITH INTEGRAL GEAR DRIVE

    CHRISTENSEN DONALD JEFFREY / MITCHELL ROBERT | European Patent Office | 2016

    Free access