An aircraft landing gear assembly having a main strut and a bogie beam pivotally coupled to the main strut via a coupling assembly. The coupling assembly is arranged to define a bogie beam pivot axis which is spaced from the landing gear assembly. The coupling assembly includes an arcuate handle portion defined by a first one of the bogie beam and the main strut, and an arcuate passage defined by the other one of the bogie beam and main strut. The arcuate handle portion is slidably housed within the arcuate passage, and the arcuate handle portion and the arcuate passage each define a respective centre point, the respective centre points being coaxial to define the bogie beam pivot axis.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft landing gear assembly


    Beteiligte:
    BENNETT IAN (Autor:in)

    Erscheinungsdatum :

    23.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT LANDING GEAR ASSEMBLY

    BERTHOUD MARCELO / GUIMARAES MAIA LEANDRO / JUESAS PORTOLES JORGE | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT LANDING GEAR ASSEMBLY

    MARK BEVAN / PIERRE-ETIENNE DANDALEIX / JORGE PORTOLES et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    AIRCRAFT LANDING GEAR ASSEMBLY

    WILLIAMS LEE / WIGHT DOUG / MILLINGTON PETER et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    AIRCRAFT LANDING GEAR ASSEMBLY

    GREEN CHRIS / GREEN KAY | Europäisches Patentamt | 2021

    Freier Zugriff

    AIRCRAFT LANDING GEAR ASSEMBLY

    FOSTER NICHOLAS / EVANS SAM | Europäisches Patentamt | 2020

    Freier Zugriff