DRONE AND METHOD FOR CONTROLLING THE ATTITUDE THEREOF

Abstract

Drone (5) which comprises a plurality of propellers (16) driven by motors (17) supported by at least one structure (18), in which a plurality of converters (15) are arranged around the structure (18) to convert electricity to high voltage in low voltage electricity. The present description also relates to a method of controlling the attitude of the drone (5).

Claims

1. A drone which comprises a plurality of propellers driven by motors supported by at least one structure with a plurality of converters arranged around the structure and configured to convert high voltage electrical energy into low voltage electrical energy, wherein at least two converters are arranged in opposite positions with respect to the structure, characterized in that the center of mass of said at least two converters substantially coincides with the center of mass of the drone.

2. The drone according to claim 1, characterized in that the converters are fixed to the motors.

3. The drone according to claim 1, characterized in that the converters are arranged under the propellers in the horizontal flight position of the drone.

4. The drone according to claim 3, characterized in that each converter supplies electrical energy to the motor which drives the propeller under which the converter is arranged.

5. The drone according to claim 1, characterized in that the center of mass of all converters substantially coincides with the center of mass of the drone.

6. The drone according to claim 5, characterized in that the structure comprises a central seat in which a winch is arranged and is provided with a drum which can rotate by means of a motor to unwind or wind a suspended cable, wherein the center of mass of two or more converters falls into the drum of the winch.

7. The drone according to claim 1, characterized by comprising temperature sensors which are arranged at the converters and/or the motors to transmit temperature data to a temperature control unit, which is suitable to calculate variation data of the rotation speed of the motors, which are sent to a flight control unit, according to the temperature data received from the temperature sensors.

8. A method for controlling the attitude of a drone which comprises a plurality of propellers driven by motors supported by at least one structure with a plurality of converters which are suitable to convert high voltage electrical energy into low voltage electrical energy, wherein at least two converters are arranged in opposite positions with respect to the structure and the center of mass of said at least two converters substantially coincides with the center of mass of the drone, characterized in that it comprises the following operating steps: measuring temperatures at the converters and at the motors by means of temperature sensors; calculating variations of the lift forces of the propellers according to said measured temperatures; varying the rotation speed of the motors according to said calculation, so as to vary the lift forces of the respective propellers.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Further advantages and characteristics of the drone and of the method according to the present description will become apparent to those skilled in the art from the following detailed and non-limiting description of an embodiment thereof, referring to the accompanying drawings in which:

[0015] FIG. 1 shows a schematic view of a drone network with a base station on the ground;

[0016] FIG. 2 shows a schematic view of a drone network with a suspended base station;

[0017] FIG. 3 shows a perspective view of the drone;

[0018] FIG. 4 shows a schematic transverse sectional view of the drone of FIG. 3;

[0019] FIG. 5 shows a block diagram of a first control system of the drone of FIG. 3;

[0020] FIG. 6 shows a schematic side view of the drone of FIG. 3;

[0021] FIG. 7 shows a block diagram of a second drone control system of FIG. 3.

EXEMPLARY EMBODIMENTS

[0022] Referring to FIG. 1, it is seen that a drone network, in particular multi-rotor propeller electric drones, may comprise a power cable 1 which is electrically connected to a base winch 2, which can be fixed to the ground. The power cable 1 can supply the base winch 2 with electricity from an electrical network, a generator or an accumulator of electricity. An auxiliary cable 4 is wound on the base winch 2 and is connected, at the opposite end, to a first drone 5. The base winch 2 is equipped with a device, for example by means of sliding contact rings, designed to guarantee continuity of the transmission of energy between the power cable 1 and the auxiliary cable 4 even during the rotation of the drum of the base winch 2. In this way, the auxiliary cable 4 can continuously supply electricity to the first drone 5. A control system 3 comprises a control unit for controlling the operation of an electric motor of the drum of the base winch 2. The first drone 5 can be connected via a suspended cable 6 to a second drone 7. The first drone 5 is equipped with at least one winch 8, on which the suspended cable 6 is wound. The suspended cable 6 can supply electrical energy and/or control signals to the second drone 7, which in turn can be equipped with a winch 10, on which a further suspended cable 11 is wound to supply electrical energy to a third drone 12, which in the present example is the last of the series and thus preferably does not include an on board winch. Drone 5 can also be the only drone in the system and/or have the auxiliary cable 4 wound on the winch 8.

[0023] Referring to FIG. 2, it can be seen that in a drone network similar to that of FIG. 1 the base winch 2 can be mounted on a mobile support 13 which can translate and/or rotate with respect to a structure 14 which maintains the mobile support 13 suspended from the ground and for example constituted by one or more suspended cables, as shown in the figure, or by the frame of a structure, by the arm of a crane or by other equipment provided in turn with degrees of freedom of rotation or translation.

[0024] Referring to FIGS. 3 and 4, it can be seen that the drone 5 comprises a plurality of converters 15 capable of converting high voltage electric energy (for example about 1000V DC), received by the auxiliary cable 4, into low voltage electric energy (e.g. 24V DC or 48V DC). The drone 5 further comprises a plurality of propellers 16 driven by motors 17 which are powered by such low voltage electricity and are supported by at least one structure 18, in particular comprising at least one frame formed of a plurality of elements joined together. The converters 15 are arranged around the structure 18, preferably fixed to the motors 17 and/or under the propellers 16, i.e. under the vertical projection of the dimensions of the propellers 16, in the horizontal flight position of the drone 5. Preferably, each converter 15 supplies electrical energy to the motor 17 which drives the propeller 16 under which the converter 15 is arranged, so that the drone 5 comprises the same number of converters 15 and motors 17. Alternative embodiments may include a smaller number of converters 15, each of which feeds multiple motors 17, for example four or two converters 15 for a drone with eight propellers 16. At least two converters 15 can be arranged in opposite positions with respect to the structure 18, preferably at substantially equal distances from the center of mass of the drone 5, so that the center of mass of these at least two converters 15 falls into the drum of the winch 8 and/or substantially coincides with the center of mass of the drone 5.

[0025] Preferably, the converters will be arranged so that the center of mass of the converters coincides to that of the drone and the drone is positioned so that the drone's inertia matrix is diagonal. Thanks to this arrangement, the control logic of the flight attitude is simplified and it is possible to use in an uniform manner the motors and the propellers during the life of the drone.

[0026] The structure 18 can comprise a central seat 19, in particular defined by a portion of the frame having a substantially rectangular shape, in which the winch 8 is arranged which carries the suspended cable 6 and which can rotate around a shaft 20 arranged in the central seat 19. The shaft 20 preferably extends outside the central seat 19 for connecting between their two motors 17 arranged in opposite positions with respect to the structure 18. The center of mass of the drone 5 preferably falls into the drum of the winch 8, in particular in a position substantially coinciding with the center of mass of the winch 8. The winch drum 8 is preferably hollow for housing certain components of the drone 5, in particular a central control unit 21 of the drone 5 and the motor 22 of the winch 8, disposed between the shaft 20 and the drum, so as to optimize the use of space and to balance the drone 5.

[0027] FIG. 5 shows a control system of the drone 5 for reducing the thermal stress of the converters 15 and of the motors 17, maintaining the flight stability of the drone 5, which system comprises temperature sensors 23 arranged in correspondence with the converters 15 and/or of motors 17 to transmit temperature data to a control unit of the temperature 24, which analyzes the distribution of the temperatures measured by the temperature sensors 23 and calculates variation data of the rotation speed of the motors 17, i.e. of their lift forces f1 . . . fn, in order to balance the temperatures, for example by raising the lower ones and lowering the higher ones, without changing the flight attitude of the drone 5. This method can be performed when the drone 5 is equipped with more than four motors 17 and propellers 16, so that there are a plurality of possible speed combinations of each propeller 16 that produce a same combination of lift forces of and of torques applied to the drone 5, preferably including the torque caused by the winch 8. The temperature control unit 24 sends calculated data of speed change to a flight control unit 25, which varies the speed of the motors 17 accordingly.

[0028] FIG. 6 shows the effect on the attitude of the drone 5 of the torque t applied by the motor 22 to operate the winch 8, for example when the suspended cable 6 must be unwound with a certain speed v. To carry out this operation, the motor 22 drives the winch 8 with a torque t which would cause an unwanted pitching of the drone 5. To balance this pitch, the drone 5 varies the speed of the motors 17 to vary the lift forces f1 . . . fn of the propellers 16 and thus generates a pitch torque equal to and opposite to the torque t. In particular, one or more lift forces f1 . . . fn of the propellers 16 are increased or decreased to wind or unwind the suspended cable 6.

[0029] FIG. 7 shows a control system of the attitude of the drone 5 to balance the rotation of the winch 8, which system comprises a control unit of the attitude 26 which receives information as input data of the torque t transmitted by a control unit of the winch 27 and data of the speeds of the motors 17 transmitted by the flight control unit 25. In the method according to the present embodiment, the control unit of the attitude 26 calculates a speed variation of the propellers 16 concerned, for example the two propellers 16 of FIG. 6 placed along a the direction perpendicular to the axis of rotation of the winch 8, so that the relative lift forces f1 and f2 balance the torque t, as described above, and sends the resulting varied speed data to the motors 17 of the two propellers 16. If the direction perpendicular to the axis of rotation of the winch 8 does not coincide with the position of two propellers 16, the control unit of the attitude 26 acts on a number superior of propellers 16, so as to have anyway a torque at the center of mass of the drone 5 which balances the torque t.

[0030] The temperature control unit 24 and/or the control unit of the flight 25 and/or the control unit of the attitude 26 and/or the control unit of the winch 27 can be implemented in a known manner in at least a single electronic control unit, preferably arranged in the central control unit 21 of the drone 5.

[0031] Any variants or additions may be made by skilled persons to the embodiment described and illustrated herein remaining within the scope of the following claims. In particular, further embodiments may include the technical characteristics of one of the following examples with the addition of one or more technical characteristics described in the text or illustrated in the drawings, taken individually or in any mutual combination.

EXAMPLES

[0032] 1. Drone (5) which comprises a plurality of propellers (16) driven by motors (17) supported by at least one structure (18), characterized in that a plurality of converters (15) are arranged around the structure (18) to convert high voltage electrical energy into low voltage electrical energy.

[0033] 2. Drone (5) according to the previous example, characterized in that the converters (15) are fixed to the motors (17).

[0034] 3. Drone (5) according to one of the preceding examples, characterized in that the converters (15) are arranged under the propellers (16) in the horizontal flight position of the drone (5).

[0035] 4. Drone (5) according to the previous example, characterized in that each converter (15) supplies electrical energy to the motor (17) which drives the propeller (16) under which the converter (15) is arranged.

[0036] 5. Drone (5) according to one of the preceding examples, characterized in that at least two converters (15) are arranged in opposite positions with respect to the structure (18).

[0037] 6. Drone (5) according to the previous example, characterized in that the center of mass of said at least two converters (15) substantially coincides with the center of mass of the drone (5).

[0038] 7. Drone (5) according to one of the preceding examples, characterized in that the center of mass of all converters (15) substantially coincides with the center of mass of the drone (5).

[0039] 8. Drone (5) according to the previous example, characterized in that the structure (18) comprises a central seat (19) in which a winch (8) is arranged and is provided with a drum which can rotate by means of a motor (22) to unwind or wind a suspended cable (6), wherein the center of mass of two or more converters (15) falls into the drum of the winch (8).

[0040] 9. Drone (5) according to one of the preceding examples, characterized by comprising temperature sensors (23) which are arranged at the converters (15) and/or the motors (17) to transmit temperature data to a temperature control unit (24), which is suitable to calculate variation data of the rotation speed of the motors (17), which are sent to a flight control unit (25), according to the temperature data received from the temperature sensors (23).

[0041] 10. Method for controlling the attitude of a drone (5) which comprises a plurality of propellers (16) driven by motors (17) supported by at least one structure (18), characterized in that it comprises the following operating steps: [0042] measuring temperatures at the motors (17) by means of temperature sensors (23); [0043] calculating variations of the lift forces (f1 . . . fn) of the propellers (16) according to said measured temperatures; [0044] varying the rotation speed of the motors (17) according to said calculation, so as to vary the lift forces (f1 . . . fn) of the respective propellers (16).

[0045] 11. Method according to the previous example, wherein the drone (5) also comprises a plurality of converters (15) which are suitable to convert high voltage electrical energy into low voltage electrical energy, characterized in that it comprises the following further operating steps: [0046] measuring temperatures at the converters (15) using temperature sensors (23); [0047] calculating variations of the lift forces (f1 . . . fn) of the propellers (16) according to said measured temperatures; [0048] varying the rotation speed of the motors (17) according to said calculation, so as to vary the lift forces (f1 . . . fn) of the respective propellers (16).