The invention provides a supporting device for an aircraft engine nacelle. The supporting device is shorter in processing period, lower in processing cost and better in rigidity when lateral load is borne in the strength test loading process. The technical scheme adopted by the invention is that the supporting device comprises a center shaft, a section part and a connecting part, wherein the center shaft penetrates through the aircraft engine nacelle; the front end and the rear end of the center shaft are respectively connected with a front beam and a rear beam which are fixed; the section part is in threaded connection with the circumferential direction of the center shaft; one side of the connecting part is in threaded connection with the section part, the other side of the connecting part is connected with the supporting end of the aircraft engine nacelle.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Supporting device for aircraft engine nacelle


    Beteiligte:
    LI QI (Autor:in)

    Erscheinungsdatum :

    10.06.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AIRCRAFT ENGINE NACELLE

    WILLIAMS GEOFFREY / SALISBURY ROSS / PEACOCK ANTONY | Europäisches Patentamt | 2020

    Freier Zugriff

    AIRCRAFT ENGINE NACELLE

    NAMGOONG HOWOONG | Europäisches Patentamt | 2019

    Freier Zugriff

    Aircraft engine nacelle

    GRALL LOÏC / SERISET MÉLODY / HEAU ALEXIS et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT ENGINE NACELLE

    WILLIAMS GEOFFREY RICHARD / SALISBURY ROSS / PEACOCK ANTONY | Europäisches Patentamt | 2021

    Freier Zugriff

    AIRCRAFT ENGINE NACELLE

    GRALL LOÏC / SERISET MÉLODY / HEAU ALEXIS et al. | Europäisches Patentamt | 2020

    Freier Zugriff