Described are systems and methods for a nacelle auxiliary landing gear to be utilized as an alternative landing gear in the event of main landing gear non-deployment. The systems described herein include a nacelle auxiliary landing gear that includes a nacelle auxiliary landing gear strut and a nacelle auxiliary landing gear wheel, coupled to the nacelle auxiliary landing gear strut, wherein at least a first portion of the nacelle auxiliary landing gear wheel is configured to be disposed outside of a nacelle of an aircraft propulsor. The nacelle auxiliary landing gear strut is coupled to a core engine. Techniques for use of the nacelle auxiliary landing gear are also described herein.


    Access

    Download


    Export, share and cite



    Title :

    NACELLE AUXILIARY LANDING GEAR


    Contributors:

    Publication date :

    2021-07-08


    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



    Nacelle auxiliary landing gear

    BARAKATAIN MOHAMMAD / BROWNLOW PETE / PIROOZMANDI FARID | European Patent Office | 2022

    Free access

    Aircraft with a nacelle-housed main landing gear

    JOSE MARIA DIAZ PARRILA / ALFONSO GONZALEZ GONZALBO | European Patent Office | 2015

    Free access

    AIRCRAFT WITH A NACELLE-HOUSED MAIN LANDING GEAR

    GONZÁLEZ GONZALBO ALFONSO / DÍAZ PARRILA JOSÉ MARÍA | European Patent Office | 2016

    Free access

    Aircraft with a nacelle-housed main landing gear

    GONZÁLEZ GONZALBO ALFONSO / DÍAZ PARRILA JOSÉ MARÍA | European Patent Office | 2017

    Free access

    Aircraft with a nacelle-housed main landing gear

    GONZALEZ GONZALBO ALFONSO / DÍAZ PARRILLA JOSE MARÍA | European Patent Office | 2019

    Free access