A gate departure system for an aircraft includes an electric traction motor for driving a wheel of a main landing gear assembly of the aircraft on only one side of the aircraft; and a controller selectively connected to a starter-generator of an auxiliary power unit (APU) and to the traction motor to control flow of electrical power to either the starter-generator for starting of the APU or the electric traction motor for driving the wheel.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    GATE DEPARTURE SYSTEM FOR AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    04.05.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Gate departure system for aircraft

    LAZAROVICH DAVID / MORCOV NICOLAE / PLENICEANU MARIUS | Europäisches Patentamt | 2017

    Freier Zugriff

    Improved Prediction of Gate Departure Times Using Pre-Departure Events

    Cook, Lara / Atkins, Stephen / Jung, Yoon | AIAA | 2008


    Improved Prediction of Gate Departure Times Using Pre-Departure Events

    Cook, L. / Atkins, S. / Jung, Y. et al. | British Library Conference Proceedings | 2008


    Zipline departure gate operating method

    CHOI BYOUNG GIL | Europäisches Patentamt | 2022

    Freier Zugriff

    Improving aircraft departure time predictability

    Vanderson, William W. (William Walter), 1977- | DSpace@MIT | 2000

    Freier Zugriff