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, a line having one end coupled to the chassis and an opposite free end, wherein the free end is positioned below the chassis, and a severing mechanism operable to sever the line under control of the control system.
1. 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 winch mounted to the chassis, the winch comprising:
a reel having a line wound on the reel, the line having a free end; and
a motor 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; and
a severing mechanism operable to sever the line under control of the control system;
wherein the severing mechanism comprises a heating tube through which the line extends, the heating tube configured to sever the line by causing the line to burn and/or melt; and
wherein the line within the heating tube is transverse to a vertical axis of the chassis.
2. The unmanned aerial vehicle of claim 1 , wherein the control system is further configured to determine a fault condition based upon information received from one or more electronic components of the unmanned aerial vehicle, and to activate the severing mechanism to sever the line in response to the fault condition.
3. The unmanned aerial vehicle of claim 2 , further comprising a sensor array;
wherein the sensor array comprises at least one of:
an inertial sensor;
a gyroscopic sensor; or
a current sensor operable to sense current drawn by the motor; and
wherein the control system is configured to determine the fault condition based upon information received from the sensor array.
4. The unmanned aerial vehicle of claim 1 , wherein the severing mechanism is mounted to an armature through which the line extends;
wherein the armature is biased toward a home position and is configured to move toward a shifted position in response to a load borne by the line;
wherein the winch further comprises a position sensor operable to detect a home/shifted position of the armature; and
wherein the control system is configured to determine a loaded/unloaded state of the winch based upon the home/shifted position sensed by the position sensor.
5. An unmanned aerial vehicle, comprising:
a chassis extending along a vertical axis;
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 having one end coupled to the chassis and an opposite free end, wherein the free end is positioned below the chassis; and
a heating tube operable to sever the line under control of the control system by causing the line to burn and/or melt, wherein a portion of the line extends through the heating tube, and wherein the heating tube extends in a direction transverse to the vertical axis.
6. The unmanned aerial vehicle of claim 5 , wherein the direction transverse to the vertical axis is perpendicular to the vertical axis.
7. The unmanned aerial vehicle of claim 5 , wherein the direction transverse to the vertical axis is a horizontal direction.
8. The unmanned aerial vehicle of claim 5 , further comprising a sensor array;
wherein the control system is configured to determine a fault condition based upon information received from the sensor array, and to activate the heating tube to sever the line in response to the fault condition.
9. The unmanned aerial vehicle of claim 8 , wherein the sensor array comprises an inertial sensor; and
wherein the control system is configured to determine the fault condition based upon information received from the inertial sensor.
10. The unmanned aerial vehicle of claim 5 , further comprising a winch mounted to the chassis, the winch comprising:
a reel having the line wound on the reel; and
a motor operable to rotate the reel under control of the control system to cause the line to wind onto and off of the reel, and as a result causing the free end of the line to raise and lower.
11. The unmanned aerial vehicle of claim 10 , further comprising a current sensor operable to sense current drawn by the motor;
wherein the control system is configured to determine a fault condition based upon information received from the current sensor, and to activate the heating tube to sever the line in response to the fault condition.
12. The unmanned aerial vehicle of claim 5 , wherein the portion of the line extends through the heating tube extends through the heating tube horizontally.
13. 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, the control system comprising an inertial sensor;
at least one rotor operable to generate lift under control of the control system;
a line having one end coupled to the chassis and an opposite free end, wherein the free end is positioned below the chassis; and
a severing device operable to sever the line under control of the control system;
wherein the control system is configured to cause the severing device to sever the line based upon information generated by the inertial sensor.
14. The unmanned aerial vehicle of claim 13 , wherein the severing device comprises a heating tube through which a portion of the line extends; and
wherein the heating tube is configured to sever the line by causing the line to burn and/or melt.
15. The unmanned aerial vehicle of claim 14 , wherein the heating tube extends horizontally.
16. The unmanned aerial vehicle of claim 13 , wherein the control system is configured to determine a fault condition based upon the information generated by the inertial sensor, and to cause the severing device to sever the line in response to the fault condition.
17. The unmanned aerial vehicle of claim 13 , wherein the severing device comprises a heating tube configured to sever the line by causing the line to melt and/or burn.
18. The unmanned aerial vehicle of claim 17 , wherein the at least one rotor is configured to generate lift along a vertical direction; and
wherein a central axis of the heating tube extends transverse to the vertical direction.
19. The unmanned aerial vehicle of claim 13 , wherein the control system is configured to determine a fault condition based upon the information generated by the inertial sensor, and to activate the severing device in response to the fault condition.