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).
DUCTED FAN ENGINE, ARRAY OF DUCTED FAN ENGINES, AND AIRCRAFT
MANTELGEBLÄSEMOTOR, ANORDNUNG VON MANTELGEBLÄSEMOTOREN UND FLUGZEUG
MOTEUR DE VENTILATEUR À CONDUIT, RÉSEAU DE MOTEURS DE VENTILATEUR À CONDUIT ET AÉRONEF
2023-03-29
Patent
Elektronische Ressource
Englisch
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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