Unmanned aerial vehicle drag augmentation by reverse propeller rotation
View Patent ↗An air vehicle configured to augment effective drag to change the rate of descent of the air vehicle in flight via propeller shaft rotation direction reversal, i.e., thrust reversal.
1. An air vehicle comprising:
at least one propeller, each propeller comprising at least one blade having a constant pitch angle;
at least one propeller motor configured to reverse propeller rotation rate of the at least one propeller while the air vehicle is in flight; and
an autopilot configured to maintain airspeed of the air vehicle above stall conditions using the propeller motor while the air vehicle is in flight.
2. The air vehicle of claim 1 wherein the motor is configured to drive the propeller via a propeller shaft, and wherein the motor is an electrical motor configured to drive the propeller shaft in either of two angular directions.
3. The air vehicle of claim 1 wherein the at least one propeller is at least one forward-mounted tractor propeller.
4. The air vehicle of claim 1 wherein the at least one propeller is at least one aft-mounted pusher propeller.
5. A method of in-flight augmentation of an air vehicle descent rate comprising:
regulating, via an autopilot, an airspeed value of the air vehicle by regulating a motor; and
generating an input to effect a change in the in-flight descent rate of the air vehicle via rotation rate reversal of at least one propeller of the air vehicle, each propeller comprising at least one blade having a constant pitch angle; and
rotating, via the motor and responsive to the input, the propeller shaft in a direction of rotation for generating forward air vehicle thrust.
6. The method of claim 5 wherein the motor driving the at least one propeller is an electrical motor configured to drive the at least one propeller in two angular directions.
7. The air vehicle of claim 5 wherein the at least one propeller is at least one forward-mounted tractor propeller.
8. The air vehicle of claim 5 wherein the at least one propeller is at least one aft-mounted pusher propeller.