Wire cutting-putting-taking integrated system and method based on high-altitude lightning attraction

Abstract

The application provides a wire cutting-putting-taking integrated system based on high-altitude lightning attraction, and belongs to the technical field of high-altitude lightning attraction. The application comprises a lightning attraction launching system, a ground remote sensing control center for controlling the lightning attraction launching system to launch a lightning attraction rocket to a strong thunderstorm cloud group and for monitoring the flight trajectory of the lightning attraction rocket in real time, when the lightning attraction rocket reaches a strong charge center area of the strong thunderstorm cloud group, the ground remote sensing control center controls a wire cutting system in the lightning attraction launching system to cut the wire and a wire putting system to put the wire respectively, when lightning is successfully induced and the wire is completely melted, the ground remote sensing control center stops sending a wire taking instruction to a wire taking system in the lightning attraction launching system, and when lightning is not successfully induced, the ground remote sensing control center controls the wire taking system to continue wire taking operation.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of high-altitude lightning attraction, and particularly relates to a wire cutting-putting-retrieving integrated system and a lightning attraction method based on high-altitude lightning attraction. BACKGROUND

[0002] The artificial triggered lightning produced by launching small rockets with thin metal wires into thunderstorm clouds can be used to conveniently measure the lightning electromagnetic field and the current at the bottom of the channel, and greatly promotes the research on the lightning physical process. Moreover, through the artificial triggered lightning experiment, the lightning electromagnetic effect evaluation and lightning protection detection can be performed on the ground lightning protection facilities and power lines.

[0003] The traditional artificial triggered lightning can be divided into ground triggered lightning and air triggered lightning according to the triggering mode. The lightning guide wires of the two are connected to the ground in a certain way, and the difference lies in that the lightning guide wire of the ground triggered lightning is directly connected to the ground, while the lightning guide wire of the air triggered lightning is connected to a section of insulating nylon line, and then the nylon line is connected to the ground. When operating, the lightning guide wire is stretched and unfolded with the rocket rising. The ground triggered lightning is caused by the breakdown discharge of the top end of the wire, while the air triggered lightning is caused by the bidirectional breakdown discharge of the top end and the bottom end of the wire. The traditional artificial triggered lightning has high space-time controllability, which provides excellent conditions for related quantitative measurement. For example, the ground triggered lightning can be used to carry out direct current measurement, and the air triggered lightning can be used to carry out targeted detection on the leader transmission and grounding process. Therefore, the traditional artificial triggered lightning plays an important role in the research on lightning discharge mechanism and lightning electromagnetic radiation characteristics.

[0004] Whether ground triggered or air triggered, the traditional artificial triggered lightning conductor needs to be connected to the ground in some form, and the length of the conductor less than 1 km determines that the upper limit of the triggered lightning height must be lower than 1 km, which belongs to low-altitude lightning triggering. Since the key to whether lightning can be successfully triggered lies in whether the tip of the conductor meets the condition of breakdown discharge, high-altitude lightning triggering operation through certain technical means will achieve more efficient artificial lightning triggering. This is because: high-altitude lightning triggering operation drags the conductor from the ground to gradually approach or even enter the charge region of the thunderstorm cloud (usually above 5 km, up to tens of kilometers), and the electric field strength can be 1 to 2 orders of magnitude larger than that near the ground. The larger electric field makes the breakdown discharge of the conductor tip more likely to occur; at the same time, the flight time of the high-altitude lightning triggering operation drag conductor is greatly increased, which further increases the possibility of successful lightning triggering. Therefore, high-altitude lightning triggering has higher application value in artificially influencing and changing the charge structure of thunderstorm clouds, and is more conducive to the study of the interaction between lightning activity and thunderstorm cloud environment. Of course, the uncertainty of whether high-altitude lightning triggering strikes the ground and the randomness of the strike position are greater than those of low-altitude lightning triggering. Therefore, the conditions for conducting quantitative measurement research on current, near-field electromagnetic field, etc. are not as good as those of low-altitude lightning triggering. Compared with low-altitude lightning triggering, high-altitude lightning triggering sacrifices certain spatiotemporal controllability and quantitative measurement conditions, but greatly improves the probability and efficiency of lightning triggering, and has higher application value in artificially influencing lightning activity and thunderstorm cloud charge structure.

[0005] To achieve high-altitude lightning triggering, a steel ring can be installed at the tail of the lightning triggering rocket, a traction weight is fixed on it, and about 200 m of conductor is wound on the steel ring. After the lightning triggering rocket is launched to a certain height (such as ~5 km), the traction line is cut off inside to make the traction weight release quickly, draw out the conductor wound in the steel ring, and drag out a longer conductor to complete the air artificial lightning triggering. According to research, the 200 m long conductor can trigger lightning in the background electric field of different regions of a thunderstorm process with high sensitivity. Generally speaking, the longer the conductor, the better the lightning triggering performance, but when the conductor reaches a certain length, further increasing the length of the conductor will no longer significantly improve the lightning triggering performance. Considering the actual application scenarios such as specific storage and unwinding, it is not appropriate to set too long a conductor.

[0006] In actual operation, there are still many technical difficulties to be broken through in the mode of high-altitude triggered lightning. For example, first, the consideration of the tension of the wire, the influence of the excessive tension of the wire in the stretching and unfolding process, etc. may cause the wire to fail to be smoothly unfolded with the rocket; second, the problem of the wire unfolding time, if the wire is immediately unfolded after the rocket is launched, there is a risk of being melted by the engine flame, and the function of releasing the wire after the ignition is completed must be realized; third, the safety problem in actual operation: if the rocket lightning triggering part is successful or unsuccessful, the nearly hundred-meter wire is maintained in the unfolded state, and finally falls with the rocket parachute, because the wire has large tensile strength and conductivity, it has high risk when falling into high-voltage lines, highways, farmland, etc.

[0007] Therefore, based on the above characteristics of high-altitude artificial triggered lightning, it is urgent to develop a stable and reliable high-altitude lightning triggering wire releasing and collecting system and method. SUMMARY

[0008] Therefore, in order to solve the problems in the background art, the present application provides a wire cutting-releasing-collecting integrated system and method based on high-altitude lightning triggering. By controlling the wire cutting system, the wire releasing system and the wire collecting system through the ground remote sensing control center, the safety of air lightning triggering is ensured, and solid technical support is provided for continuous and efficient completion of air artificial lightning triggering operation.

[0009] To achieve the above purpose, the present application provides the following technical scheme:

[0010] A wire cutting-releasing-collecting integrated system based on high-altitude lightning triggering, comprising:

[0011] A lightning launching system;

[0012] A ground remote sensing control center for controlling the lightning launching system to launch a lightning rocket to a strong thunderstorm cloud group, and for monitoring the flight trajectory of the lightning rocket in real time. When the lightning rocket reaches the strong charge center area of the strong thunderstorm cloud group, the ground remote sensing control center controls the wire cutting system in the lightning launching system to cut the wire and controls the wire releasing system to release the wire, respectively, wherein the wire cutting of the wire cutting system refers to cutting the locking wire of the locking traction plummet in the wire cutting system;

[0013] When the lightning is successfully triggered and the wire is completely melted, the ground remote sensing control center stops sending the wire collecting instruction to the wire collecting system in the lightning launching system;

[0014] When the lightning is not successfully triggered, the ground remote sensing control center controls the wire collecting system to continue the wire collecting operation.

[0015] Preferably, the wire cutting system comprises:

[0016] a tangent table arranged on one side of the lightning attracting rocket;

[0017] a tangent fixing frame arranged on the tangent table;

[0018] a tangent driving system arranged on the tangent fixing frame, for driving the tangent cutter to cut the locking line.

[0019] Preferably, it further comprises:

[0020] a locking line device arranged on both sides of the tangent fixing frame, for keeping the locking line in a tight state during the tangent cutting operation, facilitating the quick cutting of the locking line.

[0021] Preferably, it further comprises:

[0022] a wire pulley arranged on the edge of the tangent table on both sides, facilitating the feeding and discharging of the locking line.

[0023] Preferably, the tangent cutter comprises:

[0024] an upper tangent cutter connected with the tangent driving system, vertically moving under the driving of the tangent driving system;

[0025] a lower tangent cutter arranged on the tangent table, with the blade upward.

[0026] Preferably, the upper tangent cutter is connected with the tangent driving system through a vertical guide rail.

[0027] Preferably, the tangent driving system is a tangent motor.

[0028] Preferably, the wire feeding system comprises:

[0029] a traction weight fixed on a steel ring, with the wire wound thereon;

[0030] a locking ring fixed on the steel ring;

[0031] a locking line connected to the locking ring and the tangent system, for fixing the traction weight to prevent it from falling before cutting.

[0032] Preferably, it further comprises a wire tube;

[0033] the locking line is connected to the locking ring through the wire tube, for preventing the locking line from being fused.

[0034] Preferably, the traction weight is fixed through a buckle and the ring surface of the steel ring.

[0035] Preferably, the wire feeding system comprises:

[0036] A take-up drive system for driving a take-up post to rotate to wind the wire onto the take-up post.

[0037] Preferably, a power-assisted pulley is further included.

[0038] The wire is wound onto the take-up post around the power-assisted pulley.

[0039] Preferably, a traction rail is further included.

[0040] Preferably, a traction rail is further included.

[0041] A anti-winding plate is slidingly connected to the traction rail.

[0042] A force-releasing sword-shaped rod is rotationally connected at one end to the anti-winding plate and provided with a circular ring at the other end.

[0043] A force-releasing spring is connected at one end to the force-releasing sword-shaped rod and at the other end to a bracket of the traction rail.

[0044] The wire is wound onto the take-up post through the circular ring.

[0045] Preferably, the take-up drive system is a take-up motor.

[0046] Preferably, the ground remote sensing control center controls the wire cutting system, the wire releasing system and the wire take-up system through a micro control system.

[0047] Preferably, the micro control system includes:

[0048] A main control sensor is provided with a wire cutting module circuit, a wire releasing module circuit and a wire take-up module circuit for controlling the wire cutting system, the wire releasing system and the wire take-up system, respectively.

[0049] A transceiving sensor is used for receiving and sending information.

[0050] A power supply module is used for supplying power to the wire cutting system, the wire releasing system, the wire take-up system, the wire cutting module circuit, the wire releasing module circuit, the wire take-up module circuit and the transceiving sensor.

[0051] Preferably, a micro mushroom antenna is connected to the transceiving sensor.

[0052] Preferably, the power supply module is a lithium battery.

[0053] Preferably, a debris safety landing system is further included.

[0054] The debris safety landing system includes a parachute arranged in the head of the lightning attracting rocket.

[0055] In another aspect, the application further provides a lightning attracting method of the above-mentioned wire cutting-releasing-take-up integrated system based on high-altitude lightning attraction, including the following steps:

[0056] Step (1): The ground remote sensing control center controls the lightning launch system to complete the launch of the lightning rocket;

[0057] Step (2): The ground remote sensing control center receives the flight trajectory information sent by the lightning-inducing rocket in real time. When the lightning-inducing rocket reaches the central area of ​​the strong thunderstorm cloud, the ground remote control system sends tangent and release commands to the lightning-inducing rocket respectively.

[0058] If lightning is successfully triggered and the wire melts completely, the wire reeling operation is stopped.

[0059] If lightning is not successfully triggered, the wire-receiving operation will continue.

[0060] Compared with the prior art, the present invention has the following beneficial effects:

[0061] This invention utilizes a ground-based remote sensing control center to intelligently control the tangent system for tangenting, the wire-laying system for wire-laying, and the wire-retrieval system for wire-retrieval, achieving time accuracy down to the microsecond level. This not only ensures the safety of aerial mine-initiating but also provides solid technical support for the continuous and efficient completion of aerial artificial mine-initiating operations.

[0062] To ensure the smooth execution of the integrated tangent-layout-retrieval operation of the lightning-inducing rocket at high altitudes and the safe recovery of incompletely melted wires, the retrieval system in this invention has a linear speed of no less than 100 meters per minute, and the weight and volume of the layout and retrieval system meet the payload requirements of the lightning-inducing rocket.

[0063] This invention features a separate control system and operating compartment for tangenting, wire deployment, and wire retraction at the front of the lightning-inducing rocket's power chamber. A steel ring and a traction weight are installed on the tail fin of the lightning-inducing rocket or other high-range lightning-inducing rockets, and a parachute is installed inside the top compartment. This not only ensures the smooth completion of the tangent-wire deployment process during high-altitude lightning induction but also allows for wire retraction under specific conditions, even if the wire does not completely melt or trigger lightning. This not only guarantees the safety of aerial lightning induction but also provides solid technical support for the continuous and efficient completion of aerial artificial lightning induction operations. A specially designed wire conduit is used for protection to prevent the wire from melting due to high-temperature propellant. A traction weight that combines wire storage and release functions ensures smooth wire deployment. To prevent the wire from falling during low-altitude flight, a locking ring securely fixes the wire to the steel ring.

[0064] The present invention effectively solves the technical problems of the conductor breaking due to excessive tension during the stretching and unfolding process, which may prevent the conductor from being successfully unfolded with the rocket, as well as the issues of conductor initiation and unfolding time and operational safety. Attached Figure Description

[0065] Figure 1 It is the whole structure schematic diagram of the application;

[0066] Figure 2 It is the tangent system structure schematic diagram;

[0067] Figure 3 It is the pay-off system structure schematic diagram;

[0068] Figure 4 It is the take-up system structure schematic diagram;

[0069] Figure 5 It is the micro-control system structure schematic diagram;

[0070] Figure 6 It is the principle schematic diagram of the application;

[0071] In the figure, 1, tangent system; 2, pay-off system; 3, take-up system; 4, micro-control system; 5, operation implementation master control system; 11, tangent motor; 12, vertical guide rail; 13, upper tangent cutter; 14, lower tangent cutter; 15, wire locker; 16, tangent table; 17, tangent fixing frame; 21, wire guide tube; 22, locking wire; 23, locking ring; 24, traction plummet; 31, take-up motor; 32, wire; 33, take-up column; 34, anti-winding plate; 35, unloading spring; 36, traction track; 37, unloading cutter-shaped rod; 38, power-assisted pulley; 41, master control sensor; 42, lithium battery; 43, transceiver sensor; 44, micro mushroom antenna; 51, lightning attracting launching system; 52, strong thunderstorm cloud cluster; 53, debris safe landing system; 54, ground remote sensing control center; 411, tangent module circuit; 412, pay-off module circuit; 413, take-up module circuit. DETAILED DESCRIPTION

[0072] The technical solutions in the embodiments of the application will be clearly and completely described below with reference to the drawings in the embodiments of the application. Obviously, the described embodiments are only part of the embodiments of the application, and all other embodiments obtained by a person of ordinary skill in the art without creative effort on the basis of the embodiments of the application shall fall within the protection scope of the application.

[0073] In the description of the application, it should be noted that the terms "upper", "lower", "inner", "outer", "top / bottom end" and the like indicate the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the application and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as a limitation on the application.

[0074] In the description of the present application, it should be noted that unless otherwise explicitly specified and limited, the terms "mounting", "provided with", "sleeved / connected", "connected" and the like should be understood broadly, for example, "connected" can be fixedly connected, or detachably connected, or integrally connected; can be mechanically connected, or electrically connected; can be directly connected, or indirectly connected through an intermediate medium, or can be internal communication of two elements. For those skilled in the art, the specific meanings of the above terms in the present application can be understood according to the specific circumstances.

[0075] As shown in Figure 1 The present application provides a wire cutting-putting-up-wire integrated system based on high-altitude lightning attraction, comprising:

[0076] a lightning attraction launching system;

[0077] a ground remote sensing control center 54 for controlling the lightning attraction launching system to launch a lightning attraction rocket to a strong thunderstorm cloud 52, preferably by means of remote wireless remote control to complete the launching of the lightning attraction rocket, and for real-time monitoring of the flight trajectory of the lightning attraction rocket, when the lightning attraction rocket reaches the strong charge center area of the strong thunderstorm cloud 52, the ground remote sensing control center 54 controls the cutting system 1 cutting and the putting-up-wire system 2 putting-up-wire in the lightning attraction launching system respectively, wherein the cutting system 1 cutting refers to cutting off the locking line 22 of the locking traction plummet 24 in the cutting system 1;

[0078] When the lightning is successfully induced, and the wire is completely melted, the ground remote sensing control center 54 stops sending the wire collecting instruction to the wire collecting system 3 in the lightning attraction launching system;

[0079] When the lightning is not successfully induced (when the lightning does not hit the wire or the wire is not completely melted by the lightning), the ground remote sensing control center 54 controls the wire collecting system 3 to continue the wire collecting operation.

[0080] As shown in Figure 2 In the present application, a specific embodiment of the cutting system 3 is provided, comprising:

[0081] a cutting table 16 provided on one side of the lightning attraction rocket;

[0082] a cutting fixed frame 17 provided on the cutting table 16;

[0083] a cutting driving system provided on the cutting fixed frame 17 for driving the cutting knife to cut off the wire.

[0084] The tangent platform 16 is preferably fixed to one side of the lightning-inducing rocket, perpendicular to the rocket body, and a tangent fixing bracket 17 is fixed on it. The tangent fixing bracket 17 is preferably installed in the middle area of ​​the tangent platform 16. A tangent drive system is installed on the tangent fixing bracket 17.

[0085] The tangent system provided by the present invention further includes:

[0086] The locking device 15 is disposed on both sides of the wire cutting fixing frame 17 and is used to keep the locking wire 22 in a taut state when the wire cutting operation is performed, which is conducive to the rapid cutting of the locking wire 22. It is preferably installed at the center position on both sides of the wire cutting fixing frame 17.

[0087] The tangent system 1 provided by the present invention further includes:

[0088] The wire pulleys are located on the edges of both sides of the tangent table 16 to facilitate the locking of the wire 22's entry and exit.

[0089] like Figure 2 As shown, the locking line 22 passes over the wire pulley and the locking device 15, and the locking line 22 is in a taut state.

[0090] In the tangent system 1 provided by the present invention, the cutter includes:

[0091] The upper cutter 13 is connected to the tangent drive system, and the upper cutter 13 moves vertically under the drive of the tangent drive system.

[0092] The lower cutter 14 is disposed on the tangent table 16 with the blade facing upward. Preferably, the lower cutter 14 is installed in the center of the tangent table 16 with the blade facing upward, and the two are welded together and do not need to be moved.

[0093] In the tangent system provided by the present invention, the upper cutter 13 is preferably connected to the tangent drive system (preferably welded together) via a vertical guide rail 12 and is installed together with the tangent drive system. Under the drive of the tangent drive system, the vertical guide rail 12 enables the upper cutter 13 to move up and down, completing the tangent operation or stopping the tangent operation.

[0094] In the tangential system provided by the present invention, the tangential drive system is a tangential motor 11.

[0095] like Figure 3 As shown, the present invention provides a specific embodiment of a wire-laying system 2, the wire-laying system 2 comprising:

[0096] The traction weight 24 is fixed on the steel ring and has a wire 32 wound around it. It is used to pull the wire 32 and is one of the key components for the wire 32 to be fully deployed.

[0097] Locking ring 23, which is fixed to the steel ring;

[0098] Locking line 22, connected to the locking ring 23 and the tangent system, is used to secure the traction weight and prevent it from falling before it is cut.

[0099] The above-mentioned wire-laying system provided by the present invention also includes a conductor tube 21, which is used to protect the locking wire 22 from being melted by high-temperature gunpowder.

[0100] The locking line 22 is connected to the locking ring 23 through the conduit 21. In order to ensure that it does not fall off during low-altitude flight, it is firmly fixed to the steel ring by the locking line 22 and the locking ring 23.

[0101] In the above-described line-laying system provided by the present invention, the traction weight 24 is fixed by a buckle and the annular surface of the steel ring.

[0102] like Figure 4 As shown, the present invention also provides a specific embodiment of the wire retraction system 3, wherein the wire retraction system 3 is an emergency plan activated when the wire is not fully fused or has not been struck by lightning, ensuring that the wire 32 does not float in the air for an extended period of time or dangle from high-voltage lines, highways, etc., causing danger. The wire retraction system 3 includes:

[0103] A take-up drive system is used to drive the take-up post 33 to rotate so that the wire 32 is wound onto the take-up post 33. Preferably, the head of the take-up drive system pulls the take-up post 33 to rotate clockwise so that the wire 32 can be wound onto the take-up post 33.

[0104] The above-described take-up system provided by the present invention also includes a booster pulley 38;

[0105] The wire 32 passes around the assist pulley 38 and is wound around the take-up post 33.

[0106] The above-described take-up system 3 provided by the present invention further includes:

[0107] Traction track 36;

[0108] Anti-winding plate 34, which is slidably connected to the traction rail 36;

[0109] The unloading knife-shaped rod 37 has one end rotatably connected to the anti-winding plate 34, and the other end is provided with a ring;

[0110] The unloading spring 35 has one end connected to the unloading knife-shaped rod 37 and the other end connected to the bracket of the traction rail 36;

[0111] The conductor 32 passes through the ring and is wound around the take-up post 33.

[0112] In the above-mentioned take-up system 3 provided by the present application, the take-up driving system is a take-up motor 31.

[0113] The guide wire 32 is pulled into the rocket chamber from outside the arrow body, passes through the power-assisted pulley 38 and the ring on the top of the force-releasing knife-shaped rod 37, and is then wound on the take-up column 33; the force-releasing knife-shaped rod 37 is fixed on the anti-winding plate 34 through a movable ring and connected with the force-releasing spring 35 at the other end; the anti-winding plate 34 is fixed on the pulling track 36 at the upper part and moves forward and backward.

[0114] As shown in the figure, in the present application, the ground remote sensing control center 54 controls the take-up system 3, the pay-off system 2 and the wire-cutting system 1 through the micro control system 4. Figure 5

[0115] The present application provides a specific embodiment of the above-mentioned micro control system, and the micro control system 4 serves as the brain of the take-up system 3, the pay-off system 2 and the wire-cutting system 1.

[0116] The main control sensor 41 is provided with wire-cutting module circuit 411, pay-off module circuit 412 and take-up module circuit 413 for controlling the take-up system 3, the pay-off system 2 and the wire-cutting system 1 respectively; the wire-cutting module circuit 411, the pay-off module circuit 412 and the take-up module circuit 413 are connected with the main control sensor 41 in the form of connectors;

[0117] The transceiving sensor 43 is used for receiving and sending information;

[0118] The power supply module is used for supplying power to the take-up system 3, the pay-off system 2, the wire-cutting system 1, the wire-cutting module circuit 411, the pay-off module circuit 412, the take-up module circuit 413 and the transceiving sensor 43, and for supplying power to the components that need power in the above-mentioned modules and sensors.

[0119] In the present application, the transceiving sensor is connected with a micro mushroom antenna 44, and the transceiving sensor 43 and the micro mushroom antenna 44 together constitute a signal receiving and sending system.

[0120] In the above-mentioned micro control system 4 provided by the present application, the power supply module is a lithium battery 42.

[0121] As shown in the figure, in the present application, it further includes: Figure 6

[0122] The debris safe landing system 53 includes a landing parachute arranged in the head of the lightning-attracting rocket.

[0123] ​​The lightning attracting launching system 51, the strong thunderstorm cloud group 52, the debris safe landing system 53 and the ground remote sensing control center 54 jointly constitute an operation implementation master control system 5. After the lightning attracting rocket of the lightning attracting launching system 51 is launched, the ground remote sensing control center 54 sends a lightning attracting rocket head parachute opening instruction to complete the safe landing of the debris.

[0124] In another aspect, the application also provides a lightning attracting method of the above-mentioned wire cutting, laying and collecting integrated system based on high-altitude lightning attraction, which comprises the following steps, and can be specifically as follows:

[0125] Step (1), the ground remote sensing control center 54 controls the lightning attracting launching system 51 to complete the launching of the lightning attracting rocket; preferably, the instruction is launched to the lightning attracting launching system 51 through a wireless mode, and the launching of the lightning attracting rocket is completed through a remote wireless remote control mode;

[0126] Step (2), the ground remote sensing control center 54 receives the flight trajectory information sent by the lightning attracting rocket in real time, and when the lightning attracting rocket reaches the central area of the strong thunderstorm cloud group 52, the ground remote control control system sends a wire cutting and laying instruction to the lightning attracting rocket, respectively;

[0127] If the lightning is successfully attracted, and the wire is completely melted, the wire collecting operation is stopped, and the parachute ejection instruction is immediately started.

[0128] When the lightning is not successfully attracted (when the lightning does not hit the wire or the wire is not completely melted by the lightning), the wire collecting operation is continued, when the lightning does not hit the wire or the wire is not completely melted by the lightning.

[0129] The above is only a preferred specific embodiment of the application; however, the protection scope of the application is not limited thereto. Any person skilled in the art can make equivalent replacements or changes to the technical scheme of the application and the improvement concept thereof within the technical scope disclosed by the application, which should be covered in the protection scope of the application.

Claims

1. A wire cutting-laying-retrieving integrated system based on high-altitude lightning induction, characterized in that, include: Lightning-launching system; The ground-based remote sensing control center is used to control the lightning launch system to launch lightning rockets towards the strong thunderstorm cloud and to monitor the flight trajectory of the lightning rockets in real time. When the lightning rockets reach the strong charge center area of ​​the strong thunderstorm cloud, the ground-based remote sensing control center controls the tangential system and the wire-laying system within the lightning launch system to cut the wire and lay the wire, respectively. The tangential system cutting refers to cutting the locking wire of the locking traction weight in the tangential system. When lightning is successfully triggered and the wire is completely melted, the ground remote sensing control center stops sending wire receiving commands to the receiving system within the lightning triggering system. If lightning is not successfully triggered, the ground remote sensing control center controls the receiving system to continue the receiving operation. The tangent system includes: A tangential platform is located on one side of the lightning-inducing rocket; A tangent fixing bracket is disposed on the tangent table; A tangent drive system, which is mounted on the tangent fixing frame, is used to drive the cutter to cut the locking wire; The locking device is located on both sides of the wire cutting fixing frame and is used to keep the locking wire taut during the wire cutting operation, which is conducive to the rapid cutting of the locking wire. The wire pulleys are located on the edges of both sides of the tangent table to facilitate locking the wire inlet and outlet. The cutter includes: The upper cutter is connected to the tangent drive system and moves vertically under the drive of the tangent drive system; The lower cutter is mounted on the tangent table with its blade facing upwards; The upper cutter is connected to the tangent drive system via a vertical guide rail; The tangential drive system is a tangential motor; The wire-laying system includes: A traction weight, which is fixed to a steel ring, around which the aforementioned wire is wound; A locking ring, which is fixed to the steel ring; A locking line, connected to the locking ring and the tangent system, is used to secure the traction weight and prevent it from falling before it is cut. It also includes conduit; The locking wire is connected to the locking ring through the conduit to prevent the locking wire from melting. The traction weight is fixed by a buckle and the annular surface of the steel ring; The receiving system includes: A take-up drive system for driving the take-up post to rotate so that the wire is wound onto the take-up post; It also includes power-assisted pulleys; The conductor passes around the assist pulley and is wound around the take-up post; Also includes: Traction track; An anti-winding plate, which is slidably connected to the traction rail; The unloading knife-shaped rod has one end rotatably connected to the anti-winding plate, and the other end is provided with a ring; A relief spring, one end of which is connected to the relief blade rod, and the other end of which is connected to the bracket of the traction rail; The conductor passes through the loop and is wound around the take-up post.

2. The integrated wire cutting-laying-retrieving system based on high-altitude lightning as described in claim 1, characterized in that, The take-up drive system is a take-up motor.

3. The integrated wire cutting-laying-retrieving system based on high-altitude lightning as described in claim 1, characterized in that, The ground-based remote sensing control center controls the tangent system, the wire laying system, and the wire take-up system through a micro-control system.

4. The integrated wire cutting-laying-retrieving system based on high-altitude lightning as described in claim 3, characterized in that, The microcontroller system includes: The main control sensor is equipped with tangent module circuits, pay-off module circuits, and take-up module circuits respectively used to control the tangent system, pay-off system, and take-up system. Transceiver sensors are used to receive and send information; The power supply module is used to supply power to the tangent system, the pay-off system, the take-up system, the tangent module circuit, the pay-off module circuit, the take-up module circuit, and the transceiver sensor.

5. The integrated wire cutting-laying-retrieving system based on high-altitude lightning as described in claim 4, characterized in that, The transceiver sensor is equipped with a miniature mushroom antenna.

6. The integrated wire cutting-laying-retrieving system based on high-altitude lightning as described in claim 4, characterized in that, The power supply module is a lithium battery.

7. A wire cutting-laying-retrieving integrated system based on high-altitude lightning strikes according to any one of claims 1-6, characterized in that, Also includes: The debris landing system includes a parachute disposed within the head of the lightning-inducing rocket.

8. A lightning-attracting method for a high-altitude lightning-attracting integrated wire cutting-laying-retrieving system according to any one of claims 1-7, characterized in that, Includes the following steps: Step (1): The ground remote sensing control center controls the lightning launch system to complete the launch of the lightning rocket; Step (2): The ground remote sensing control center receives the flight trajectory information sent by the lightning-inducing rocket in real time. When the lightning-inducing rocket reaches the central area of ​​the strong thunderstorm cloud, the ground remote control system sends tangent and release commands to the lightning-inducing rocket respectively. If lightning is successfully triggered and the wire is completely melted, the wire reeling operation is stopped. If lightning is not successfully triggered, the wire-receiving operation will continue.

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