In a Ducted fan engine (1), configured for providing thrust for an aircraft (100), in particular an aircraft (100) having vertical takeoff and landing capability, comprising a fan stator (3) having one or more substantially radially extending vanes (31); a shroud (11) circumferentially surrounding the fan stator (3); a fan rotor (5) rotatably supported by the fan stator (3); at least one electromotor (2) configured for driving the fan rotor (5), wherein in particular the electromotor is arranged within the fan stator (3); it is provided that at least one heat pipe (4) configured for dissipating heat from the electromotor (2) is arranged in at least one vane (31).


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    Title :

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


    Additional title:

    MANTELGEBLÄSEMOTOR, ANORDNUNG VON MANTELGEBLÄSEMOTOREN UND FLUGZEUG
    MOTEUR DE VENTILATEUR À CONDUIT, RÉSEAU DE MOTEURS DE VENTILATEUR À CONDUIT ET AÉRONEF


    Contributors:

    Publication date :

    2023-03-29


    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 / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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