An aircraft (100) equipped with a distributed unducted fan propulsion system (150) is provided. In one aspect, an aircraft (100) includes a body (102) defining a lateral centerline that separates the body (102) into a first side (114) and a second side (116). One or more first unducted fans (162A) are mounted to the first side (114) of the body (102). The one or more first unducted fans (162A) are rotatable in a first direction. One or more second unducted fans (172A) are mounted to the second side (116) of the body (102). The one or more second unducted fans (172A) are rotatable in a second direction that is opposite the first direction.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT EQUIPPED WITH A DISTRIBUTED COUNTERROTATING UNDUCTED FAN PROPULSION SYSTEM


    Additional title:

    FLUGZEUG MIT VERTEILTER GEGENLÄUFIGER DIFFUSER GEBLÄSEANTRIEBSANLAGE
    AÉRONEF ÉQUIPÉ D'UN SYSTÈME DE PROPULSION À SOUFFLANTE NON CARÉNÉE À CONTRE-ROTATION RÉPARTI


    Contributors:

    Publication date :

    2022-03-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIRCRAFT EQUIPPED WITH A DISTRIBUTED COUNTERROTATING UNDUCTED FAN PROPULSION SYSTEM

    FREELY BRENDAN MICHAEL / MURROW KURT DAVID / MCMAHON MICHAEL JAMES et al. | European Patent Office | 2022

    Free access



    UNDUCTED PROPULSION SYSTEM

    TWEEDT DANIEL L / KHALID SYED ARIF | European Patent Office | 2023

    Free access

    Unducted propulsion system

    TWEEDT DANIEL L / KHALID SYED ARIF | European Patent Office | 2023

    Free access