An aircraft for fixed pitch lift includes a fuselage, a plurality of flight components attached to the fuselage, wherein the plurality of flight components further comprises at least a lift propulsor component, wherein the lift propulsor component comprises a plurality of blades configured at a fixed angle of attack, and a pusher component, wherein the pusher component is configured to produce a forward thrust.

    Un aéronef pour une portance à tangage fixe comprend un fuselage, une pluralité de composants de vol fixés au fuselage, la pluralité de composants de vol comprenant en outre au moins un composant de propulseur de portance, le composant propulseur de portance comprenant une pluralité de pales agencées à un angle d'attaque fixe, et un composant poussoir, le composant poussoir étant conçu pour produire une poussée vers l'avant.


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    Title :

    AIRCRAFT FOR FIXED PITCH LIFT AND METHOD OF USE


    Additional title:

    AÉRONEF POUR PORTANCE À TANGAGE FIXE ET PROCÉDÉ D'UTILISATION



    Publication date :

    2022-11-24


    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



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