TREE TRIMMING WITH DRONE

Abstract

The present invention relates to a cutting device (1) for fitting on an unmanned aerial vehicle (10) for the high-level pruning of vegetation in areas close to power distribution lines, which comprises at least one system for attachment (200) to the aerial vehicle (10) having a central beam (230), at least four arms (210) having connection points (12) to rods of the unmanned aerial vehicle, oriented toward motors of the aerial vehicle (10) for attachment to the aerial vehicle and a system for releasing (220) at least one cutting tool (300) whilst in use, and at least one cutting tool (300), made up of a plurality of saws each driven by a motor (310), a cutting rod (330) for attaching the plurality of saws and an automatic leveling system (320) for the cutting rod (330), which maintains said rod (330) in a horizontal position during the cutting process.

Claims

1. Cutting device to be fitted to an unmanned aerial vehicle for the high-level pruning of vegetation in areas close to power distribution lines, wherein it comprises at least one system for attachment to the unmanned aerial vehicle having a central beam, at least four arms having connection points to rods of the unmanned aerial vehicle, oriented toward motors of the unmanned aerial vehicle for attachment to the aerial vehicle and a release system for at least one cutting tool whilst in use, wherein said cutting tool in use comprises a plurality of saws each driven by a motor, a cutting rod for attaching the plurality of saws and an automatic leveling system for the cutting rod, which maintains said rod in a horizontal position during the cutting process.

2. Cutting device according to claim 1, wherein at each end of the central beam of the attachment system two opposite arms extend outwards.

3. Cutting device according to claim 2, wherein each arm is formed by an outward horizontal extension an upward vertical extension and a second outward horizontal extension, which comprises at least one opening.

4. Cutting device according to claim 2, wherein it comprises a connection component which comprises a connection point, which is connected to the second extension of the arm, and a clamping portion, connected to the connection point at one end and which in turn is secured to the arm of the drone by the clamping portion at the other end.

5. Cutting device according to claim 1, wherein on the lower central portion of the beam a connection point is arranged on the base of the system for attachment to the cutting rod, which in turn has a rail for the release system.

6. Cutting device according to claim 5, wherein the release system is configured with two portions, wherein a first portion of the release system is fixed to the unmanned aerial vehicle, and consists of a system of three rails where a second portion, which is rigidly connected to a cutting tool (300) is fastened from below, and which has on its upper portion a metal platen which rotates by 90 on a vertical axis.

7. Cutting device according to claim 6, wherein the first portion, the rail on the central connection point, just below the center of the unmanned aerial vehicle has a square profile with no lower face, wherein on its side faces it has opposite slots; on the left side the slot is arranged from the center toward the rear and on the right side the slot is arranged from the center toward the front, and on the upper face of the profile of the central connection point is a hole that allows both portions of the release system to be aligned.

8. Cutting device according to claim 7, wherein the second portion has on its upper portion a metal platen which rotates by 90 on a vertical axis.

9. Cutting device according to claim 8, wherein in the open (or disengaged) position, the platen is collinear with the cutting tool and with the side faces of the first portion of the release system, the axis of rotation has an upward extension which is inserted in the hole in the upper face of the first portion.

10. Cutting device according to claim 9, wherein when the second portion is fastened to the first portion, the platen rotates by 90 in a clockwise direction, actuated by a high-torque servomotor, actuated in turn by radio by the copilot.

11. Cutting device according to claim 10, wherein to unfasten both portions and release the cutting tool, the metal platen rotates by 90 in an anti-clockwise direction, actuated by the high-torque servomotor, actuated in turn by radio by the copilot of the unmanned aerial vehicle, wherein the platen comes out of both slots of the first portion and allows the cutting tool to be released by the effect of gravity.

12. Cutting device according to claim 1, wherein the plurality of saws comprises from one to three saws, where each is driven by a three-phase electric motor.

13. Cutting device according to claim 12, wherein the motors are controlled by electronic drivers controlled from a multichannel radio frequency receiver.

14. Cutting device according to claim 13, wherein the radio receiver also controls the movement of a servomotor which drives the system for releasing/separating the cutting tool from the drone.

15. Cutting device according to claim 1, wherein it comprises a plurality of batteries which supply electric power for the cutting tool and the mechanical release system.

16. Cutting device according to claim 1, wherein the automatic leveling system comprises low-friction bearings mounted on the load center of the cutting rod.

17. Cutting device according to claim 16, wherein it comprises drive modules to correct movements that take the cutting rod out of its horizontal position, where said drive modules comprise three-phase electric motors, which in turn actuate variable-pitch propellers.

18. Cutting device according to claim 17, wherein the pitch of the propellers is controlled by servomotors which are in turn actuated by an electronic control system, which operates based on electronic gyroscopes and accelerometers, capable of detecting tilts and angular accelerations of the cutting tool.

19. Cutting device according to claim 1, wherein the release system of the cutting tool is controlled by radio control actuated by a ground operator (copilot); when the release system is actuated, the radio control sends an order over the servomotor of the release system, resulting in the mechanical disconnection of the cutting tool, and releasing said cutting tool by the effect of gravity from the attachment system.

20. Cutting device according to claim 19, wherein the radio control controls the switching on and speed control of the cutting saws, allowing the cutting saws to be switched on, their speed to be controlled and a stop request to be issued to an electric deceleration system.

21. Cutting system for the high-level pruning of vegetation in areas close to power distribution lines, wherein it comprises an unmanned aerial vehicle, preferably an industrial drone, in order to approach highly complex access points, which comprises a plurality of drive motors, and a cutting device which comprises at least one attachment system to the unmanned aerial vehicle (10) having a central beam, at least four arms having connection points to rods of the unmanned aerial vehicle, oriented toward motors of the unmanned aerial vehicle for attachment to the unmanned aerial vehicle and a release system for at least one cutting tool whilst in use, where said cutting tool is made up of a plurality of saws each driven by a motor, a cutting rod for attaching the plurality of saws and an automatic leveling system for the cutting rod, which maintains said rod in a horizontal position during the cutting process.

22. Cutting system according to claim 21, wherein at each end of the central beam of the attachment system two opposite arms extend outwards.

23. Cutting system according to claim 22, wherein each arm is formed by an outward horizontal extension, an upward vertical extension and a second outward horizontal extension, which comprises at least one opening.

24. Cutting system according to claim 22, wherein it comprises a connection component which comprises a connection point, which is connected to the second extension of the arm, and a clamping portion connected to the connection point at one end and which in turn is secured to the arm of the drone by the clamping portion at the other end.

25. Cutting system according to claim 21, wherein on the lower central portion of the beam is arranged a connection point of the base of the attachment system to the cutting rod, which in turn has a rail for the release system.

26. Cutting system according to claim 25, wherein the release system is configured in two portions, where a first portion of the release system is fixed to the unmanned aerial vehicle, and consists of a system of three rails where a second portion, which is rigidly connected to a cutting tool is fastened from below, and which has a metal platen on its upper portion which rotates by 90 on a vertical axis.

27. Cutting system according to claim 26, wherein the first portion, the rail on the central connection point, just below the center of the unmanned aerial vehicle has a square profile, with no lower face, wherein it has opposite slots on its side faces; on the left side the slot is arranged from the center toward the rear and on the right side, the slot is arranged from the center toward the front, and on the upper face of the profile of the central connection point is a hole which allows both portions of the release system to be aligned.

28. Cutting system according to claim 27, wherein the second portion has, on its upper portion, a metal platen which rotates by 90 on a vertical axis.

29. Cutting system according to claim 28, wherein in the open (or disengaged) position, the platen is collinear with the cutting tool and with the side faces of the first portion of the release system, the axis of rotation has an upward extension which is inserted in the hole in the upper face of the first portion.

30. Cutting system according to claim 29, wherein when the second portion is fastened to the first portion, the platen rotates by 90 in a clockwise direction, actuated by a high-torque servomotor, actuated in turn by radio by the copilot.

31. Cutting system according to claim 30, wherein to unfasten both portions and release the cutting tool, the metal platen rotates by 90 in an anti-clockwise direction, actuated by the high-torque servomotor, actuated in turn by radio by the copilot of the unmanned aerial vehicle, wherein the platen comes out of both slots of the first portion and allows the cutting tool to be released by the effect of gravity.

32. Cutting system according to claim 21, wherein the attachment system comprises a release system for at least one cutting tool whilst in use, to separate the cutting tool from the unmanned aircraft.

33. Cutting system according to claim 21, wherein the plurality of saws comprises from one to three saws, where each is driven by a three-phase electric motor.

34. Cutting system according to claim 33, wherein the motors are controlled by electronic drivers controlled from a multichannel radio frequency receiver.

35. Cutting system according to claim 34, wherein the radio receiver also controls the movement of a servomotor which drives the system for releasing/separating the cutting tool from the drone.

36. Cutting system according to claim 21, wherein it comprises a plurality of batteries that supply electric power for the cutting tool and the mechanical release system.

37. Cutting system according to claim 21, wherein the automatic leveling system comprises low-friction bearings mounted on the load center of the cutting rod.

38. Cutting system according to claim 37, wherein it comprises drive modules for correcting movements that take the cutting rod out of its horizontal position, where said drive modules comprise three-phase electric motors, which in turn actuate variable-pitch propellers.

39. Cutting system according to claim 38, wherein the pitch of the propellers is controlled by servomotors which in turn are actuated by an electronic control system, which operates based on electronic gyroscopes and accelerometers, capable of detecting tilts and angular accelerations of the cutting tool.

40. Cutting system according to claim 21, wherein the system for releasing the cutting tool is controlled by a radio control actuated by a ground operator (copilot); when the release system is actuated, the radio control sends an order over the servomotor of the release system resulting in the mechanical disconnection of the cutting tool, releasing said cutting tool by the effect of gravity from the attachment system.

41. Cutting system according to claim 40, wherein the radio control controls the switching on and speed control of the cutting saws, allowing the cutting saws to be switched on, their speed to be controlled, and a stop request to be issued to an electric deceleration system.

Description

DESCRIPTION OF THE DRAWINGS

[0019] FIG. 1 is a view of the attachment system according to a preferred embodiment of the invention.

[0020] FIG. 2 is a view of a connection component for an arm of the drone according to a preferred embodiment of the invention.

[0021] FIG. 3 is a view of the cutting tool and the associated components according to a preferred embodiment of the invention.

[0022] FIG. 4 is a view of the cutting system and device according to a preferred embodiment of the invention.

DETAILED DESCRIPTION OF THE INVENTION

[0023] The cutting system (100) and device (1) according to the present invention are designed to be fitted to an unmanned aerial vehicle (10), where said unmanned aerial vehicle may be an industrial drone, in order to approach highly complex access points.

[0024] The cutting device (1) comprises at least one variable-geometry attachment system (200) for attachment to the unmanned aerial vehicle (10) (UAV), configured as a mechanical system for anchoring at least four arms (210) to the drive motors (11) of the aerial vehicle (10), with connection points to the variable-geometry rods of the drone (10), as shown in FIGS. 1 and 2. As can be seen in FIG. 1, the attachment system (200) comprises a central beam (230), wherein at each end of said central beam (230) two arms (210), opposite one another, extend outwards, each arm (210) being formed by an outward horizontal extension (210a), an upward vertical extension (210b) and a second outward horizontal extension (210c), which comprises at least one opening for connection by attachment means with a connection component (240) to an arm of the drone (10), which in turn comprises a connection point (240a) with a second extension of the arm (210c) and a clamping portion (240b), connected to the connection point (240) which is secured to the arm of the drone by a clamping portion at the other end (FIG. 2.)

[0025] On the lower central portion of the beam (230) a connection point (250) is arranged for connecting the base of the attachment system (200) to a cutting rod (330), which in turn has a rail for the release system (220) (FIG. 2.)

[0026] The function of the attachment system (200) is to act as a mechanical base for connecting at least one cutting tool (300) to the unmanned aerial vehicle (10). A portion of the attachment system (200) is removable, in which portion a release system (220) for at least one cutting tool (300) whilst in use is located. Said release system (220) is designed mainly to separate the cutting tool (300) from the unmanned aerial vehicle (10) in situations such as the cutting tool (300) becoming entangled in the vegetation that is being cut, or instability produced by the cutting tool (300) such as to prevent the unmanned aerial vehicle (10) from flying. Moreover, said release system (220) of the two portions which comprise the attachment system (200) facilitates access to the cutting tool (300) for transport, maintenance, exchange with other cutting tools, battery changes, etc.

[0027] The release system (220) is configured in two portions. The first portion of the release system (220) is fixed to the unmanned aerial vehicle (10) and consists of a system with three rails (250, 250a, 250b) where the second portion (220a), which is rigidly connected to a cutting tool (300), is fastened from below.

[0028] The first portion, the rail on the central connection point (250), just below the center of the unmanned aerial vehicle (10) has a square profile, with no lower face. On the side faces are opposed slots, where, on the left side, the slot is arranged from the center toward the rear and on the right side, the slot is arranged from the center toward the front. On the upper face of the profile of the central connection point (250) is a hole which allows both portions of the release system (220) to be aligned.

[0029] The second portion, which is rigidly connected to the cutting tool (300), has on its upper portion a metal platen (220a) which rotates by 90 on a vertical axis. In the open (or disengaged) position, the platen (220a) is collinear with the cutting tool (300) and with the side faces of the first portion of the release system (220), the axis of rotation has a downward extension which is inserted in the hole in the upper face of the first portion. When the second portion is fastened to the first portion, the platen (220a) rotates by 90 in a clockwise direction, actuated by a high-torque servomotor (220b), actuated in turn by radio by the copilot. The metal platen (220a) then fits into the slots in the side faces of the first portion (250). As long as both portions are fastened, the complete cutting tool assembly (300) is suspended from the metal platen. To unfasten both portions and release the cutting tool (300), the metal platen (220b) rotates by 90 in an anti-clockwise direction, actuated by the high-torque servomotor (220a), actuated in turn by radio by the copilot of the unmanned aerial vehicle (10). The platen (220a) comes out of both slots in the first portion (250) and allows the cutting tool to be released by the effect of gravity.

[0030] The system (100) also comprises at least one cutting tool (300), which in a preferred embodiment is made up of one to three (depending on the task conditions) 7-inch saws, each driven by a three-phase brushless electric motor (310). Said motors (310) are controlled by electronic drivers (Electronic Speed Controller, ESC). The drivers of the motors are in turn controlled from a multichannel radio frequency receiver. The radio receiver also controls the movement of a servomotor (320) which drives the system (220) for releasing/separating the cutting tool from the drone (10), allowing said cutting tool (300), should it unexpectedly become trapped in the vegetation, to be released/separated by the release system (220), leaving the drone (10) free of the cutting tool (300). The electric power for the cutting tool (300) and the mechanical release system (220) is supplied by lithium-ion polymer (LiPo) batteries, independent of the batteries that drive the unmanned aircraft (10).

[0031] The cutting tool (300) has an automatic leveling system (320) for a cutting rod (330), which maintains the horizontal position thereof. This is achieved by means of pivots with low friction bearings mounted on the load center of the cutting rod. The cutting rod (330) has a normal state of equilibrium, and corrections to movements that take said cutting rod out of its horizontal position are produced by drive modules (340) which may adjust or reverse the vertical and horizontal thrust at the end of the cutting rod (330) opposite the cutting disks. The drive module (340) is made up of three-phase brushless electric motors (341), which in turn actuate variable-pitch propellers (342). The pitch of the propellers (342) is controlled by servomotors which in turn are actuated by an electronic control system, which operates based on electronic gyroscopes and accelerometers, capable of detecting tilts and angular accelerations of the cutting tool. The fact that the cutting tool (300) can pivot at its center prevents said cutting tool from transferring too much rotational inertia to the drone (10).

[0032] The cutting tool (300) may also produce limited rotations on a vertical axis to facilitate the pruning action when the aircraft (10) is static (in hover mode) close to the point where pruning is to take place, and the cutting rod (330) can rotate in a horizontal plane (left-right) and cut vegetation without the need to move the drone (10). The tool (300) pivots on a horizontal rotation mechanism mounted on a low-friction bearing. The impulse for the rotary movement comes from another drive module controlled by the same electronic control system that keeps the cutting rod horizontal (but performing functions on a vertical axis).

[0033] The system (220) for releasing the cutting tool (300) is controlled by radio control actuated by a ground operator (copilot). When the release system (220) is actuated, the radio control sends an order over the servomotor of the release system (220), resulting in the mechanical disconnection of the cutting tool (330), and releasing said cutting tool by the effect of gravity from the attachment system (200). The same radio control signal in turn generates an order for the motors (310) that actuate the cutting saws to decelerate, in order to reduce risk. The electronic drivers, the radio frequency receiver and the batteries are arranged in an electric control unit (350) positioned close to one end of the cutting rod (330).

[0034] The cutting saws are switched on and their speed controlled by multichannel radio control actuated by a ground operator (copilot). This allows the cutting saws to be switched on, their speed to be controlled, and a stop request to be issued to an electric deceleration system. The horizontal movement (left-right) actuation order is issued by radio control actuated by a ground operator (copilot), which acts on the electronic stabilization system for the cutting rod, which in turn acts on the servomotors of the drive modules. Finally, this makes possible the angular changes required to perform the cutting work.

[0035] Owing to the extra weight and rotational inertia added to the unmanned aircraft (10) as a result of the attachment (200) and the cutting tool (300) systems, the gains characteristic of the aircraft flight control system must be modified to greatly improve the dampening of the oscillations produced during any translation movement. The cameras and their stabilization systems (gimbals) must also be repositioned owing to the installation of the base of the attachment system.