A ducted-rotor aircraft includes a fuselage, one or more ducts, and a spindle that rotatably couples the one or more ducts to the fuselage. Each duct includes a hub that is configured to support a rotor, a plurality of stators that are coupled to the hub, a duct ring that is coupled to the plurality of stators, and a fitting that is coupled to a first stator of the plurality of stators. The fitting has a tubular collar that defines a first aperture that extends through the fitting. The collar is configured to receive a portion of the spindle. The first stator includes a rib that is spaced inward from the fitting and that defines a second aperture that is aligned with the first aperture and that is configured to receive an end of the spindle.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Spindle to primary duct stator attachment


    Beteiligte:

    Erscheinungsdatum :

    08.02.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    SPINDLE TO PRIMARY DUCT STATOR ATTACHMENT

    SCHROEDER KARL / CARPENTER JR JOSEPH RICHARD / ZIMMERMAN BRETT | Europäisches Patentamt | 2021

    Freier Zugriff

    DUCT ATTACHMENT BRACKET

    SUGANO MICHIYO | Europäisches Patentamt | 2018

    Freier Zugriff

    HVAC AUXILIARY DUCT ATTACHMENT

    GOSIOCO DELOMER / BELANGER BRIAN | Europäisches Patentamt | 2016

    Freier Zugriff

    Bicycle crank with spindle attachment structure

    DUBOIS GEORGE / PETERS JOEL | Europäisches Patentamt | 2021

    Freier Zugriff

    BICYCLE CRANK WITH SPINDLE ATTACHMENT STRUCTURE

    DUBOIS GEORGE / PETERS JOEL | Europäisches Patentamt | 2017

    Freier Zugriff