Aircraft with thrust vectoring tail
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.
1. An aircraft, comprising:
an airframe having an upper section and a tail section;
a main rotor assembly operably disposed at the upper section and including a main rotor that is rotatable about a rotational axis defined through the airframe;
one or more tail rotor assemblies operably disposed on the tail section and respectively including one or more articulated propellers with thrust vectoring capability that are each independently rotatable about a respective variable rotational axis; and
not more than one controllable wing extending outwardly from a side of the aircraft.
2. The aircraft according to claim 1 , wherein the main rotor comprises a rigid main rotor system.
3. The aircraft according to claim 1 , wherein blades of the one or more articulated propellers are cyclically and collectively controllable for adjustments of aircraft flight controls.
4. The aircraft according to claim 1 , wherein each of the one or more articulated propellers comprises a hub with at least one of offset flapping hinges, a flexible prop-rotor and a teetering hub.
5. The aircraft according to claim 1 , further comprising a variable speed controller coupled to the one or more articulated propellers.
6. The aircraft according to claim 1 , wherein the controllable wing is pivotable about respective longitudinal axes thereof with one or more locking mechanisms to fix the angles of the controllable wings at specified angles.
7. The aircraft according to claim 1 , wherein the controllable wing comprises at least one of a trailing edge trim tab and an aileron surface.
8. The aircraft according to claim 1 , wherein the controllable wing comprises a segmented wing element.
9. The aircraft according to claim 1 , wherein the one or more articulated propellers are each configured to assume at least one or more of a flat pitch mode, a tail rotor mode and a pusher-propeller mode.