A boundary layer propulsor comprises a rotor and a plurality of first aerofoil blades. The rotor has an axis of rotation. The plurality of first aerofoil blades extends radially from the rotor and is arranged in a circumferential array around the axis of rotation. Each of the first aerofoil blades has, in a radially outward sequence, a radially proximal portion, a middle portion, and a radially distal portion. The radially proximal portion has a first cambered cross-section, the middle portion has a second uncambered cross-section, and the radially distal portion has a third cambered cross-section. The first cambered cross-section is cambered in an opposite sense to the third cambered cross-section.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    PROPULSOR


    Beteiligte:
    GOODHAND MARTIN N (Autor:in) / MOXON MATTHEW (Autor:in)

    Erscheinungsdatum :

    23.08.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Propulsor

    ANDREW M ROLT / KENNETH F UDALL / ALAN R MAGUIRE | Europäisches Patentamt | 2017

    Freier Zugriff

    PROPULSOR

    OSOKIN ALEKSEJ RUDOLFOVICH | Europäisches Patentamt | 2021

    Freier Zugriff

    PROPULSOR

    BARANOV VLADIMIR NIKOLAEVICH | Europäisches Patentamt | 2019

    Freier Zugriff

    Propulsor

    GOODHAND MARTIN N / MOXON MATTHEW | Europäisches Patentamt | 2020

    Freier Zugriff

    VEHICLE PROPULSOR

    BAGICH GENNADIJ LEONIDOVICH | Europäisches Patentamt | 2016

    Freier Zugriff