Flying vehicle systems and methods
An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a power supply mounted to the chassis, a control system operable to receive power from the power supply, at least one rotor operable to generate lift under control of the control system, and a winch mounted to the chassis. The winch includes a reel and a motor. The reel has a line wound thereon, the line having a free end. The reel includes a circumferential channel in which a wound portion of the line is wound onto the reel. The circumferential channel includes an inner portion, an outer portion, and a passage connecting the inner portion and the outer portion. The motor is operable to rotate the reel under control of the control system to thereby cause the line to wind onto and off of the reel, thereby causing the free end of the line to raise and lower.
1. A method, comprising:
securing an attachment mechanism to a delivery load such that the delivery load is operable to be lifted by exertion of a lifting force on the attachment mechanism, wherein the attachment mechanism comprises a ring and a base to which the ring is mounted, and wherein securing the attachment mechanism to the delivery load comprises adhering the base to the delivery load; and
receiving a portion of a hook within the ring, wherein the hook is attached to an unmanned aerial vehicle (UAV) such that the UAV is operable to lift the delivery load by exerting the lifting force.
2. The method of claim 1 , wherein the delivery load is lifted by the UAV subsequent to the ring receiving the portion of the hook.
3. The method of claim 1 , further comprising removing a protective film from an adhesive region of the base;
wherein adhering the base to the delivery load comprises engaging the adhesive region with the delivery load.
4. The method of claim 1 , wherein the hook is a gravity hook that comprises a lever movable between a first position and a second position; and
wherein the method further comprises moving, by the ring, the lever from the first position to the second position against a biasing force urging the lever toward the first position.
5. The method of claim 1 , wherein securing the attachment mechanism to the delivery load comprises securing the attachment mechanism to the delivery load via one or more tethers.
6. A method of operating an unmanned aerial vehicle (UAV), the method comprising:
sensing a position of an armature of the UAV;
in response to sensing the position as a first position, determining that the UAV has been loaded with a delivery load; and
in response to sensing the position as a second position, determining that the delivery parcel has been unloaded from the UAV.
7. The method of claim 6 , wherein the armature is limited to movement between the first position and the second position.
8. The method of claim 6 , wherein the armature is biased toward one of the first position or the second position.
9. The method of claim 6 , wherein the UAV further comprises a line onto which the delivery load can be loaded; and
wherein the line drives the armature from the second position to the first position when at least a portion of a weight of the delivery load is borne by the line.
10. The method of claim 9 , wherein the line passes through the armature.
11. The method of claim 6 , wherein sensing the position of the armature comprises sensing the position via a snap-action switch.
12. The method of claim 6 , further comprising, with the delivery load coupled to a free end of a line, selectively operating a winch to lower the free end of the line and the delivery load based at least in part upon sensing the position as the first position.
13. The method of claim 12 , further comprising selectively operating the winch to raise the free end of the line based at least in part upon sensing the position as the second position.
14. An unmanned aerial vehicle, comprising:
a chassis;
a power supply mounted to the chassis;
a control system operable to receive power from the power supply;
at least one rotor operable to generate lift under control of the control system;
a line operable to bear weight of a delivery load;
an armature having a first position and a second position, wherein the armature is configured to adopt the first position when the line bears the weight of the delivery load, and wherein the armature is configured to adopt the second position when the line does not bear the weight of the delivery load; and
a sensor operable to sense at least one position of the armature;
wherein the control system is configured to determine a loaded/unloaded state of the line based upon information generated by the sensor.
15. The unmanned aerial vehicle of claim 14 , wherein the sensor is a snap action switch.
16. The unmanned aerial vehicle of claim 14 , wherein the line passes through the armature.
17. The unmanned aerial vehicle of claim 14 , further comprising a winch operable to adjust a height of a free end of the line;
wherein the control system is configured to selectively operate the winch based at least in part upon the information generated by the sensor.
18. The unmanned aerial vehicle of claim 14 , wherein the armature is limited to movement between the first position and the second position.
19. The unmanned aerial vehicle of claim 14 , wherein the armature is biased toward one of the first position or the second position.