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
10.08.2017
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Rotary or fixed wing aircraft with thrust vectoring tail
Europäisches Patentamt | 2019
|Fluid thrust vectoring nozzle and wing integrated aircraft
Europäisches Patentamt | 2024
|