A diverter duct for a propeller includes a second duct element having a semi-annular wedge shape, which is pivotably coupled to the first duct element, a first drive structure configured to drive a pivoting of the second duct element relative to the first duct element and a second drive structure configured to drive a rotation of the first and second duct elements about an axis of rotation of the propeller.
Propeller diverter duct
2020-01-21
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Cycloid propeller duct power device and aircraft applying cycloid propeller duct power device
European Patent Office | 2022
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