A duct (107) for a ducted-rotor aircraft (101) includes a hub (119), a duct ring (149), and a plurality of stators (121) that extend outward from the hub (119). The hub (119) may be configured to support a motor. The duct ring (149) defines a trailing edge (155). The duct ring (149) is coupled to each of the plurality of stators (121) such that all or substantially all of each of the plurality of stators (121) is located aft of the trailing edge (155) of the duct ring (149).
STATORS LOCATED AFT OF DUCT RING
HINTER EINEM KANALRING ANGEORDNETE STATOREN
STATORS SITUÉS À L'ARRIÈRE D'UN ANNEAU DE CONDUIT
2021-07-14
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |