Patent Application
20230415916
The present invention relates to a lightning stroke resistant structure of a flying object.
An unmanned aerial vehicle such as a drone has been conventionally known. Since the unmanned aerial vehicle flies outdoors, there is a high risk of encountering a lightning strike. Therefore, in Non-Patent Literature 1, a direct lightning stroke test is carried out in which a high voltage current directly strikes an unmanned aerial vehicle during flight. Then, it is reported that the current passes through an airframe of the unmanned aerial vehicle and reaches the ground, rendering the unmanned aerial vehicle inoperable.
In a case where a lightning strike occurs on an unmanned aerial vehicle, the unmanned aerial vehicle will break down and become inoperable, and thus there is a possibility that human and material losses occur due to a crash of the unmanned aerial vehicle.
The present invention has been made in view of the above circumstances, and an object of the present invention is to provide a technology capable of preventing deterioration of a flight function and a crash due to a lightning stroke on a flying object.
A lightning stroke resistant structure of a flying object according to an aspect of the present invention includes a lattice-shaped conductor surrounding a flying object with a distance not hindering flight, an attachment part for the conductor connected between the lattice-shaped conductor and a part of the flying object, and a conducting wire connected between the lattice-shaped conductor and a ground point on a ground.
According to the present invention, it is possible to prevent deterioration of a flight function and crash due to a lightning stroke on a flying object.
Hereinafter, an embodiment of the present invention will be described with reference to the drawings. In the drawings, the same parts are denoted by the same reference signs, and description thereof is omitted.
The conductor 11 is a conductor that receives a lightning stroke current from the sky instead of the unmanned aerial vehicle 100. The conductor 11 is arranged outside the periphery of the unmanned aerial vehicle 100 so as to surround the unmanned aerial vehicle 100 at a distance that does not hinder the flight of the unmanned aerial vehicle 100 located inside. The conductor 11 has a lattice shape as illustrated in
The attachment part 12 is an attachment part for the conductor 11 for attaching and fixing the lattice-shaped conductor 11 to the unmanned aerial vehicle 100. The attachment part 12 is, for example, an insulating rod member. The rod member is connected between one point (part) of the lattice-shaped conductor 11 and one point (part) of the unmanned aerial vehicle 100. Although a plurality of rod members may be connected to a plurality of points of the unmanned aerial vehicle 100, it is preferable to connect one rod member to only one point of the unmanned aerial vehicle 100 in order to eliminate the possibility of the lightning stroke current to flow into the unmanned aerial vehicle 100.
The conducting wire 13 is a conducting wire for causing a lightning stroke current received by the lattice-shaped conductor 11 to flow to the ground. The conducting wire 13 is, for example, a conducting wire cable. The conducting wire cable is connected between a lower part of the lattice-shaped conductor 11 and an input end of the control facility 14 on the ground.
The control facility 14 is a control facility for controlling the lightning stroke current passing through the conducting wire 13. The control facility 14 is installed on the ground. The control facility 14 is, for example, a lightning stroke current cutoff device, a lightning rod, a structure on the ground, or a ground. Any ground point on the ground may be used.
That is, the lightning stroke resistant structure of the unmanned aerial vehicle has a configuration in which the unmanned aerial vehicle 100 is surrounded by the lattice-shaped conductor 11 at a distance to such an extent that flight is not hindered on the outside of the unmanned aerial vehicle 100, the lattice-shaped conductor 11 is connected to a main body of the unmanned aerial vehicle 100 at one point, the conducting wire 13 is connected to the lower part of the lattice-shaped conductor 11, and the conducting wire 13 is connected to the control facility 14 on the ground.
With this configuration, even if a lightning strike occurs on the unmanned aerial vehicle 100, a lightning stroke current due to the lightning strike is received by the lattice-shaped conductor 11 and flows to the ground via the lower conducting wire 13. The lightning stroke current is shunted by the lattice-shaped conductor 11, and electric fields due to the currents cancel each other inside the lattice-shaped conductor 11, so that the influence of the lightning stroke current on the unmanned aerial vehicle 100 can be extremely reduced.
That is, a lightning stroke does not enter the vicinity of the unmanned aerial vehicle 100 due to the Faraday gauge effect caused by the lattice-shaped conductor 11 surrounding the outside of the unmanned aerial vehicle 100. The Faraday gauge effect is an effect in which an electric line of force cannot enter the inside surrounded by the conductor, so that an external electric field is blocked and potentials inside are all equal. Furthermore, since the lightning stroke current flows in a grid shape, the electric fields inside the grid cancel each other from four directions, and thus the lightning stroke current can be extremely reduced.
As described above, according to the present embodiment, since the lightning stroke resistant structure of the unmanned aerial vehicle includes the lattice-shaped conductor 11 surrounding the unmanned aerial vehicle 100 with a distance not hindering the flight, the attachment part 12 for the conductor 11 connected between the lattice-shaped conductor 11 and a part of the unmanned aerial vehicle 100, and the conducting wire 13 connected between the lattice-shaped conductor 11 and the control facility 14 on the ground, it is possible to prevent deterioration of the flight function and crash due to the lightning stroke to the unmanned aerial vehicle 100.
Finally, in the present embodiment, although an unmanned aerial vehicle such as a drone has been described as an example, the present invention can be applied to a flying object to which the above-described lightning stroke resistant structure can be added. The flying object is, for example, a balloon, a small manned aircraft, a flying object or aircraft flying in a high altitude, or the like.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/JP2020/042476 | 11/13/2020 | WO |
