Adjustable motor fairings for aerial vehicles
Systems and methods to reduce aerodynamic drag and/or affect flight characteristics of an aerial vehicle may include adjustable fairings associated with one or more components of the aerial vehicle. The adjustable fairings may be coupled to and at least partially surround a motor, propulsion mechanism, motor arm, strut, or other component of an aerial vehicle. In addition, the adjustable fairings may be passively movable between two or more positions responsive to airflow around the fairings, and/or the adjustable fairings may be actively moved between two more positions to affect flight characteristics. Further, the adjustable fairings may include actuatable elements to alter a portion of an outer surface of the fairings to thereby affect flight characteristics. In this manner, adjustable fairings associated with various components of an aerial vehicle may reduce aerodynamic drag and/or may improve control and safety of an aerial vehicle.
1. An aerial vehicle, comprising:
a body;
a plurality of motor arms extending from the body;
a plurality of motors, each motor coupled to a respective motor arm of the plurality of motor arms;
a plurality of propellers, each propeller coupled to and rotated by a respective motor of the plurality of motors; and
a plurality of motor fairings, each motor fairing movably coupled to and completely surrounding a respective motor of the plurality of motors, wherein each motor fairing as a whole is movable relative to a respective motor to which each motor fairing is coupled.
2. The aerial vehicle of claim 1 , wherein each motor fairing is rotatable relative to an axis of a respective motor arm to which the respective motor is coupled.
3. The aerial vehicle of claim 1 , wherein each motor fairing is rotatable in substantially 360 degrees of rotational freedom relative to the respective motor.
4. The aerial vehicle of claim 1 , wherein each motor fairing includes at least one of a vane, a fin, or a tail.
5. A propulsion apparatus, comprising:
a propulsion mechanism; and
a fairing movably coupled to and completely surrounding the propulsion mechanism, wherein the fairing as a whole is movable relative to the propulsion mechanism;
wherein the fairing is movable between at least two positions.
6. The propulsion apparatus of claim 5 , wherein the fairing is movably coupled to the propulsion mechanism by a rotatable joint defining an axis of rotation; and
wherein the fairing is rotatable between the at least two positions relative to the axis of rotation.
7. The propulsion apparatus of claim 5 , wherein the fairing is movably coupled to the propulsion mechanism by a spherically rotatable joint; and
wherein the fairing is rotatable between the at least two positions relative to the spherically rotatable joint.
8. The propulsion apparatus of claim 5 , wherein a first position of the at least two positions of the fairing is associated with a vertical flight configuration, and wherein a second position of the at least two positions of the fairing is associated with a horizontal flight configuration.
9. The propulsion apparatus of claim 5 , wherein the fairing includes at least one of a vane, a fin, a tail, a flap, or a tab.
10. The propulsion apparatus of claim 5 , further comprising:
an actuator coupled to the fairing and configured to move the fairing between the at least two positions.
11. The propulsion apparatus of claim 10 , wherein the actuator is configured to move the fairing to alter an aerodynamic characteristic associated with the propulsion apparatus.
12. The propulsion apparatus of claim 5 , further comprising:
at least one actuatable element associated with an outer surface of the fairing and configured to alter the outer surface of the fairing.
13. The propulsion apparatus of claim 12 , wherein the at least one actuatable element includes at least one of a vane, a fin, a tail, a flap, or a tab.
14. The propulsion apparatus of claim 12 , wherein the at least one actuatable element is movable between a retracted position substantially flush with the outer surface of the fairing and an extended position at least partially protruding from the outer surface of the fairing.
15. The propulsion apparatus of claim 14 , wherein in the retracted position, the at least one actuatable element forms a portion of a tapered end at a trailing surface of the fairing.
16. The propulsion apparatus of claim 14 , wherein in the extended position, the at least one actuatable element forms a portion of cross shape at a trailing surface of the fairing.
17. A method to operate an aerial vehicle, comprising:
instructing adjustment, by an actuator, of a fairing associated with a propulsion mechanism, the fairing movably coupled to and completely surrounding the propulsion mechanism, wherein the fairing as a whole is movable relative to the propulsion mechanism;
wherein the adjustment of the fairing alters an aerodynamic characteristic associated with the aerial vehicle.
18. The method of claim 17 , wherein instructing adjustment of the fairing comprises changing a position of the fairing relative to the aerial vehicle.
19. The method of claim 17 , wherein instructing adjustment of the fairing comprises modifying an outer surface of the fairing by at least one actuatable element.
20. The method of claim 19 , wherein the at least one actuatable element includes at least one of a vane, a fin, a tail, a flap, or a tab.