The present lift generating fuselage (1) for aircraft mainly comprises of: a novel aerofoil shaped fuselage (1A); or a novel aerofoil shaped fuselage body (2); and integral webs (3); or a novel aerofoil shaped fuselage body (2); integral webs (3) and overhead central wing (4).

    La présente invention concerne un fuselage de génération de portance (1) pour un aéronef principalement composé des éléments suivants: un fuselage en forme de plan de sustentation innovant (1A); ou un corps de fuselage en forme de plan de sustentation innovant (2); et des âmes solidaires (3); ou un corps de fuselage en forme de plan de sustentation innovant (2); des âmes solidaires (3) et une aile centrale supérieure.


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    Title :

    LIFT GENERATING FUSELAGE FOR AIRCRAFT


    Additional title:

    FUSELAGE DE GÉNÉRATION DE PORTANCE POUR AÉRONEF


    Contributors:

    Publication date :

    2017-04-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B60V Luftkissenfahrzeuge , AIR-CUSHION VEHICLES / B64C AEROPLANES , Flugzeuge



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