An aircraft engine nacelle spoiler assembly including a number of spoilers and actuators. Each spoiler has a drag surface and a nacelle connection point. The spoilers are shiftable via the actuators between a stowed position and a deployed position such that the drag surfaces are substantially parallel with the direction of relative wind when the spoilers are stowed and exposed to the relative wind when the spoilers are deployed.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Nacelle aerodynamic spoiler


    Beteiligte:

    Erscheinungsdatum :

    27.07.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



    NACELLE AERODYNAMIC SPOILER

    WEST RANDALL RAY | Europäisches Patentamt | 2020

    Freier Zugriff

    CAR PROVIDED WITH REAR SPOILER AND WITH AERODYNAMIC ELEMENTS TO INCREASE AERODYNAMIC EFFICIENCY OF REAR SPOILER

    MATTEO BIANCALANA / SALVATORE SEDDA | Europäisches Patentamt | 2021

    Freier Zugriff

    AERODYNAMIC ELECTRIC MOTOR NACELLE

    KENDALL GREG T | Europäisches Patentamt | 2021

    Freier Zugriff

    AERODYNAMIC ELEMENT FOR AIRCRAFT NACELLE

    BLIN CELINE / STRUB GUILLAUME / REYRON VINCENT | Europäisches Patentamt | 2015

    Freier Zugriff

    Adaptable aerodynamic spoiler for a motor vehicle

    AUDEN JOSHUA R / EZZAT HESHAM A | Europäisches Patentamt | 2016

    Freier Zugriff