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 (51); 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.
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
2022-05-18
Patent
Elektronische Ressource
Englisch
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