Ducted fan engine (1) configured for providing thrust for an aircraft (100), in particular an aircraft having vertical takeoff and landing capability, comprising: a shroud (3) having a substantially circular cross section; a stator (5) having one or more substantially radially extending stator vanes; and a rotor (7) rotatably supported by the shroud; wherein the rotor comprises at least 19 rotor blades (71), in particular at least 25 rotor blades.

    Moteur à soufflante carénée (1) configuré pour produire une poussée destinée à un aéronef (100), en particulier un aéronef ayant une capacité de décollage et d'atterrissage verticaux, comprenant : un carénage (3) ayant une section transversale sensiblement circulaire ; un stator (5) ayant une ou plusieurs aubes de stator s'étendant sensiblement radialement ; et un rotor (7) supporté rotatif par le carénage ; le rotor comprenant au moins 19 pales de rotor (71), en particulier au moins 25 pales de rotor.


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    Title :

    DUCTED FAN ENGINE, ARRAY OF DUCTED FAN ENGINES, AND AIRCRAFT


    Additional title:

    MOTEUR À SOUFFLANTE CARÉNÉE, RÉSEAU DE MOTEURS À SOUFFLANTE CARÉNÉE, ET AÉRONEF


    Contributors:

    Publication date :

    2022-09-01


    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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