An aircraft assembly is provided and includes a first member extending from an aircraft airframe, a propeller, which is drivable to rotate and a secondary member on which the propeller is supportable and which is aerodynamically pivotable with respect to the first member.
ROTARY OR FIXED WING AIRCRAFT WITH THRUST VECTORING TAIL
2017-08-10
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Rotary or fixed wing aircraft with thrust vectoring tail
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