An aircraft is provided and includes an airframe having an upper section and a tail section, a main rotor assembly operably disposed at the upper section and one or more tail rotor assemblies operably disposed at the tail section. The one or more tail rotor assemblies respectively include one or more articulated propellers with thrust vectoring capability that are each independently rotatable about a respective variable rotational axis.
AIRCRAFT WITH THRUST VECTORING TAIL
2016-11-17
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Rotary or fixed wing aircraft with thrust vectoring tail
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