In some embodiments, an aircraft includes a fuselage having a forward portion and an aft portion. First and second ducted fans are supported by the forward portion of the fuselage. The first and second ducted fans are tiltable relative to the fuselage between a generally horizontal orientation, in a vertical takeoff and landing mode, and a generally vertical orientation, in a forward flight mode. A tailboom having an aft station extends from the aft portion of the fuselage. A cross-flow fan is disposed in the aft station of the tailboom and is operable to generate a pitch control moment.
Tilting ducted fan aircraft generating a pitch control moment
2018-10-23
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
TILTING DUCTED FAN AIRCRAFT GENERATING A PITCH CONTROL MOMENT
European Patent Office | 2019
|TILTING DUCTED FAN AIRCRAFT GENERATING A PITCH CONTROL MOMENT
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|Tilting Ducted Fan Aircraft Generating a Pitch Control Moment
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