A nose gear spin down apparatus includes a spin down device and a resistance device. The spin down device is rotatable about a central longitudinal axis. The spin down device rotates about the central longitudinal axis after engagement with a spinning nose gear wheel of an aircraft. The resistance device contacts the spin down device without imparting a resistance to the spin down device. The resistance device imparts the resistance to the spin down device after conditions are met.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Nose Gear Spin Down Apparatus


    Beteiligte:
    ADAMS JOSHUA P (Autor:in)

    Erscheinungsdatum :

    24.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    NOSE GEAR STEERING APPARATUS FOR SHIPBOARD OPERATIONS

    HOVAN WILLIAM E / VARGA ANDREW / BRESH CHRISTOPHER A et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    NOSE GEAR STEERING APPARATUS FOR SHIPBOARD OPERATIONS

    HOVAN WILLIAM E / VARGA ANDREW / BRESH CHRISTOPHER A et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    Retractable Nose Landing Gear

    R. C. Churchill | NTIS | 1979


    Aircraft nose landing gear

    ZHANG TIANCHUANG / LIU ZHIWEI / WANG SHAONING et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Nose landing gear retraction

    Emerald Group Publishing | 2000