SYSTEM AND PROCESS FOR STARTING THE FLIGHT OF POWER WING AIRFOILS, IN PARTICULAR FOR WIND GENERATOR

Abstract

A system for starting the flight of power wing airfoils, in particular for a wind generator, comprising at least one wing profile, operatively connected through control tie-rods, to winches or other control mechanisms of a flight of such wing profile, and at least one autonomous transporting flying vector adapted to be connected through disengageable connecting means to at least one wing profile and to transport in flight such wing profile. A process is further described, for starting the flight of such power wing airfoils through such system.

Claims

1. A system for starting the flight of power wing airfoils, in particular for a wind generator, comprising: a) at least one wing profile, operatively connected through control tie-rods, to control mechanisms for flight of the at least one wing profile; and b) at least one autonomous transporting flying vector adapted to be connected through a disengageable connecting means to the at least one wing profile and adapted to transport the at least one wing profile in flight.

2. The system of claim 1, wherein the disengageable connecting means comprises: a) at least one dragging cable having a first end connected to the autonomous transporting flying vector; and b) a second opposite end connected to the first end equipped with at least one actuatable engaging/disengaging device adapted to be engaged/disengaged to and from a respective engagement point arranged on the at least one wing profile.

3. The system of claim 2, wherein the actuatable engaging/disengaging device comprises at least one electromagnetic hook and the engagement point arranged on the at least one wing profile is a related element made of metallic material adapted to be magnetically connected to the electromagnetic hook.

4. The system of claim 2, wherein the at least one wing profile further comprises at least one measuring system to triangulate relative positions of the autonomous transporting flying vector and the at least one wing profile.

5. The system of claim 4, wherein the at least one measuring system is preferably an ultrasound type measuring system adapted to high frequency triangulation.

6. The system of claim 3, wherein the engagement point of the actuatable engaging/disengaging device is arranged along an outlet, namely a leading edge of the wing profile.

7. The system of claim 1, wherein starting the flight of the wing profile is assisted by a combined action of two or more of the autonomous transporting flying carriers.

8. The system of claim 1, wherein the autonomous transporting flying carrier is a helicopter with one or more propellers, and preferably a quadcopter, an octocopter or a multicopter.

9. The system of claim 1, wherein the autonomous transporting flying carrier is with electric supply.

10. The system of claim 1, comprising at least one landing, storing and energy recharging station of at least one of the autonomous transporting flying carriers.

12. A process for starting the flight of power wing airfoils, in particular for wind generator, through the system of claim 10, comprising the steps of: a) starting from a stalling position of the power wing profile, taking at least one autonomous transporting flying carrier next to the power wing profile; b) engaging the power wing profile to the autonomous transporting flying carrier through the disengageable connecting means; c) transporting, in flight, the power wing profile through a traction by the autonomous transporting flying carrier, possibly taking care to perform a suitable unwinding of the control tie-rods; and d) disengaging the autonomous transporting flying carrier from the power wing profile, once reaching a height in which there is enough wind for supporting in flight and/or a flight of the profile.

13. The process of claim 12, further comprising the step of taking back the autonomous transporting flying carrier to a landing, storing and energy recharging station.

14. A computer program comprising program code means which, when run on a computer, perform the steps of the process according to claim 13.

15. A computer program comprising program code means which, when run on a computer, perform the steps of the process according to claim 14.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0010] The present invention will be better described by some preferred embodiments thereof, provided as a non-limiting example, with reference to the enclosed drawings, in which:

[0011] FIGS. 1, 2 and 3 show some steps of the process of starting the flight according to the present invention through a system according to the present invention; and

[0012] FIG. 4 shows an alternative embodiment of the system for starting the flight according to the present invention.

DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS

[0013] With reference to the Figures, it is possible to note that the system 1 for starting the flight of power wing airfoils 7, in particular for a wind generator 5, comprises:

[0014] at least one wing profile 7 operatively connected, through respective control tie-rods 9 as known in the art, to suitable winches or other control mechanisms (not shown) of the flight of the related wing profile 7;

[0015] at least one autonomous transporting flying vector 11 adapted to be connected through disengageable connecting means 13 to at least one wing profile 7 and to transport in flight such wing profile 7.

[0016] Preferably, such disengageable connecting means 13 are composed of at least one dragging cable 15 having a first end connected to such autonomous transporting flying vector 11 and a second opposite end to such first end equipped with at least one actuatable engaging/disengaging device 17 adapted to be engaged/disengaged to and from a respective engagement point arranged on the wing profile 7 and, for example, arranged along the attachment edge of the wing profile 7 itself. In a preferred alternative, as it is possible to note in particular in FIG. 4, it is possible to provide that the engagement point of the actuatable engaging/disengaging device 17 is arranged along the outlet edge 18 of the wing profile 7 in order to enable the starting of flight of the wing profile 7, so that this latter one, once having reached the desired flight height and having been disengaged from the autonomous transporting flying vector 11, can take the falling speed along the correct direction, exploiting the force of gravity and easily exit from a possible stalling situation.

[0017] Preferably, such actuatable engaging/disengaging device 17 is at least one electromagnetic hook and such engagement point arranged on the wing profile 7 is a related element made of metallic material, adapted to be magnetically connected to such electromagnetic hook. Obviously, the length, for example included between 4 m and 6 m, of the dragging cable 15 is the most suitable one to ensure the freedom of manoeuvre in flight of the autonomous transporting flying vector 11 without the flow produced by its own propellers necessarily impacts onto the wing profile 7.

[0018] As it is possible to note in particular always in FIG. 4, it is also possible to provide that, in case of wing profiles 7 whose sizes and weights are relatively high, the starting of flight of the wing profile 7 can be assisted by the combined action of two or more of such autonomous transporting flying vectors 11: in such case, in order to keep the geometry of the wing profile 7 unchanged, which could be subjected to distortions due to the combined traction exerted on different points of its own attachment or outlet edge 18 by two or more autonomous transporting flying vectors 11, such wing profile 7 of the system 1 according to the present invention can further comprise at least one measuring system 19, for example of the ultrasound type 21, which high frequency triangulates the relative positions of the autonomous transporting flying vectors 11 and of the wing profile 7.

[0019] In a preferred embodiment of the system 1 according to the present invention, such autonomous transporting flying vector 11 is a helicopter with one or more propellers, such as, for example, a quadcopter, an octocopter, a multicopter, etc., and, still more preferably, with electric supply. In fact, the electric supply of the autonomous transporting flying vector 11 is particularly suitable, since the manoeuvre for starting the flight of the wing profile 7 can be completed in few minutes and, therefore, compatibly with the energetic autonomy of such vector 11, possibly allowing the vector 11 itself to autonomously go back to a suitable recharging station, once having taken in flight and disengaged the wing profile 7 itself. For such purpose, the system 1 according to the present invention can therefore further comprise at least one landing, storing and energy recharging station (not shown) of at least one of such autonomous transporting flying vectors 11.

[0020] The present invention further refers to a process for starting the flight of power wing airfoils 7, in particular for wind generator 5, preferably through a system 1 according to the present invention as previously described, such system 1 in particular comprising at least one wing profile 7 operatively connected, through respective control tie-rods 9 as known in the art, to suitable winches or other control mechanisms (not shown) of the flight of the related wing profile 7, and at least one autonomous transporting flying vector 11 adapted to be connected through disengageable connecting means 13 to at least one wing profile 7 and a transport in flight such wing profile 7. In particular, the process according to the present invention comprises the steps of:

[0021] starting from a stalling position of the power wing profile 7 (like the one, for example, shown in FIG. 1), taking at least one autonomous transporting flying vector 11 next to such power wing profile 7;

[0022] engaging such power wing profile 7 to such autonomous transporting flying vector 11 through such disengageable connecting means 13 (as shown, for example, in FIG. 2);

[0023] transporting in flight such power wing profile 7 through traction by such autonomous transporting flying vector 11, possibly taking care of suitably unwinding the related control tie-rods 9 (as shown, for example, in FIG. 3);

[0024] once having reached, by such power wing profile 7, a height in which there is enough wind for supporting in flight and/or the flight of the profile 7, disengaging such autonomous transporting flying vector 11 from such power wing profile 7.

[0025] Possibly, the process according to the present invention can comprise the step of taking back such autonomous transporting flying vector 11 to a landing, storing and energy recharging station.

[0026] It is wholly clear that the present invention further refers to at least one computer program comprising program code means which, when run on a computer, autonomously and automatically perform all or part of the steps of the above mentioned process.