Intrinsically safe gliding fire extinguishing aerial bomb and launching control method thereof
Through photoelectric image guidance and plasma excitation detonation technology, combined with the gliding module, precise fire extinguishing is achieved at long distance release, solving the problems of aircraft control difficulties and detonator safety hazards in the existing technology, and improving the safety of fire-extinguishing bombs Sex and efficiency.
Patent Information
- Application Number
- CN202411264047.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-09-10
- Publication Date
- 2024-12-27
AI Technical Summary
When existing fire-extinguishing bombs are released near the forest fire zone, the aircraft is difficult to control due to strong hot air flow disturbance, which poses a risk of safety explosion, and the detonator fuses used are poor in safety, resulting in great safety hazards during production, transportation and use.
Design an intrinsically safe gliding fire extinguishing bomb, using photoelectric image seeker and plasma excitation tool, detonate violent explosives and fire extinguishing agents through plasma shock wave, combine chemical suppression mechanism to achieve efficient fire extinguishing, and pass the gliding module and tail rudder The machine module provides precise guidance to avoid close-range projection.
It has been implemented to release 1.5km to 3km away from the forest fire area, avoiding the risk of aircraft crashes, improving the production, transportation and use of fire-extinguishing bombs, and no need to use dangerous detonator fuses, ensuring the safety of the entire process.
Smart Images
Figure CN119185830A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the technical field of forest fire extinguishing, and in particular to an intrinsically safe gliding fire-extinguishing bomb and a method for controlling its delivery. Background Art
[0002] Some fire-fighting bombs in the prior art have a short range and need to be mounted on an aircraft and dropped from the air 0.6km to 1.5km away from the forest fire area. Within this distance, due to the violent disturbance of the strong hot air rising, it is easy to cause the aircraft to be unable to control and cause a serious crash. In addition, the central explosive column of some fire-fighting bomb warheads uses a mixture of RDX and TNT explosives. The density of the column ranges from 1.6 to 1.7g / cm 3 The detonation velocity of the charge column is not less than 7000m / s. The detonation of the B explosive requires a detonator fuze. The detonator is a dangerous item strictly controlled by the state. The detonator fuze is filled with explosives with poor safety and high mechanical sensitivity, making these fire-fighting bombs prone to safety explosion accidents during production, transportation, storage, and deployment. Summary of the invention
[0003] In order to overcome the shortcomings of the prior art, the purpose of the present invention is to provide an intrinsically safe gliding fire-extinguishing bomb that can be dropped from the air 1.5km to 3km outside the forest fire area, thereby ensuring that the aircraft does not need to fly over the forest fire site or drop it at close range, and can avoid the risk of crashing due to the inability to effectively control the flight of the aircraft caused by the violent disturbance of the rising strong hot air flow. At the same time, there is no need to install explosive fuses with poor safety and high mechanical sensitivity. Therefore, it is intrinsically safe throughout the entire process of production, transportation, storage, and delivery and use, thereby improving the safety of the fire-extinguishing bomb throughout the entire process of production, transportation, storage, and delivery and use.
[0004] In order to solve the above problems, the technical solution adopted by the present invention is as follows: an intrinsically safe gliding fire-extinguishing bomb, which is mounted in the air by an aircraft and flies to the forest fire site, and is dropped from the air 1.5km to 3km away from the forest fire area, comprising a fire-extinguishing bomb body, an optoelectronic image guidance head, a tail servo module and a first control module; the fire-extinguishing bomb body comprises an outer shell and a plasma excitation device, a high explosive column and a fire extinguishing agent arranged in the outer shell, the high explosive column is inserted in the fire extinguishing agent, the plasma excitation device can generate a plasma shock wave to detonate the high explosive column and the fire extinguishing agent; the optoelectronic image guidance head The head is arranged at the head of the fire-extinguishing bomb body, the tail servo module is arranged at the tail of the fire-extinguishing bomb body, the first control module is arranged in the fire-extinguishing bomb body, and is electrically connected or signal-connected to the photoelectric image seeker, the first control module and the plasma excitation device; the photoelectric image seeker is used to detect the image of the forest fire area and transmit the signal to the first control module, and the first control module can control the tail servo module according to the signal of the photoelectric image seeker to guide the gliding fire-extinguishing bomb to fly to the forest fire area, and control the plasma excitation device to generate plasma shock waves.
[0005] Compared with the prior art, the beneficial effect of the present invention is that after the gliding fire-extinguishing bomb is dropped, during the landing flight, the photoelectric image seeker can detect the image of the forest fire area, control the tail servo module through the first control module, guide the fire-extinguishing bomb to fly to the forest fire area, and after flying to the target position, the electric energy stored in the high-voltage capacitor is controlled by the first control module to discharge instantly in the central bridge foil of the plasma excitation device, generating a high-temperature, high-pressure, high-speed plasma shock wave, directly detonating the high-explosive column and the fire extinguishing agent, and then forming a large-area explosion ultrafine aerosol shock wave, and cooperating with the chemical inhibition fire extinguishing mechanism to achieve efficient fire extinguishing. The gliding fire-extinguishing bomb can be mounted by manned helicopters, fixed-wing aircraft or large unmanned aerial vehicles, and can be dropped in the air 1.5km to 3km away from the forest fire area through the detection and guidance of the photoelectric image seeker, thereby ensuring that the aircraft does not need to fly over the forest fire site or project at close range, and can avoid the danger of crashing caused by the violent disturbance of the rising strong hot air flow that causes the aircraft to be unable to effectively control flight. At the same time, since the gliding fire-extinguishing bomb can use electric energy to trigger the plasma excitation device to generate a plasma shock wave, and then detonate the high explosive column and the fire extinguishing agent, there is no need to install dangerous goods detonator fuses with poor safety and high mechanical sensitivity. Therefore, it is inherently safe throughout the entire process of production, transportation, storage, and deployment, thereby improving the safety of the fire-extinguishing bomb throughout the entire process of production, transportation, storage, and deployment.
[0006] The above-mentioned intrinsically safe gliding fire-extinguishing bomb has a second control module in the cockpit of the aircraft, and the second control module signal is connected to the photoelectric image seeker and the tail servo module. The second control module can control the tail servo module according to the signal of the photoelectric image seeker to guide the gliding fire-extinguishing bomb to fly to the forest fire area.
[0007] The above-mentioned intrinsically safe gliding fire-extinguishing bomb also includes a glider module, which includes a wing fixing plate, a left wing and a right wing, the wing fixing plate is arranged on the top of the fire-extinguishing bomb body, and the left wing and the right wing are respectively arranged on the left and right sides of the fire-extinguishing bomb body; the tail servo module includes a directional servo, a pitch servo and a servo control unit, and the servo control unit is electrically connected or signal-connected to the directional servo, the pitch servo, the first control module and the second control module.
[0008] The above-mentioned intrinsically safe gliding fire-extinguishing bomb, the first control module includes an intelligent circuit board and a GC-Bus and antenna printed board, the intelligent circuit board is electrically connected or signal-connected to the optoelectronic image seeker, and the intelligent circuit board is connected to the GC-Bus and antenna printed board via a two-wire communication bus GC-Bus and a wireless communication radio frequency line, and the GC-Bus and antenna printed board are connected to the servo control unit via a two-wire communication bus GC-Bus.
[0009] In the above-mentioned intrinsically safe gliding fire-extinguishing bomb, the left wing and the right wing are folding wings.
[0010] The above-mentioned intrinsically safe gliding fire-extinguishing bomb, the second control module includes an image microprocessor controller, a wireless data communication circuit, a display remote control operating system and an electric-controlled mounting locking device; the first interface, the second interface and the third interface of the image microprocessor controller are respectively connected to the wireless data communication circuit, the display remote control operating system and the electric-controlled mounting locking device, and the wireless data communication circuit is signal-connected to the first control module.
[0011] The above-mentioned intrinsically safe gliding fire-extinguishing bomb, the electrically controlled mounting locking device includes a spring, an electromagnetic coil and an electric latch, and a mounting hole is provided on the top of the fire-extinguishing bomb body. When the electromagnetic coil is not energized, the electric latch is inserted into the mounting hole by the action of the spring. When the electromagnetic coil is energized, the electric latch is pulled out of the mounting hole and the gliding fire-extinguishing bomb is released.
[0012] In the intrinsically safe gliding fire-extinguishing bomb mentioned above, the optoelectronic image seeker includes a blister cover connected to the shell, a camera platform arranged in the blister cover and a camera arranged on the camera platform, and the camera is electrically connected or signal-connected to the first control module.
[0013] In the above-mentioned intrinsically safe gliding fire-extinguishing bomb, the high explosive column is RDX, TNT, B high explosive or emulsion explosive, and the fire extinguishing agent is dry powder fire extinguishing agent or liquid fire extinguishing agent.
[0014] The present invention also provides a method for controlling the delivery of an intrinsically safe gliding fire-extinguishing bomb, comprising the following steps:
[0015] Step S100: The gliding fire-extinguishing bomb is mounted on an aircraft and flies to the forest fire site, and is dropped from the air at a distance of 1.5 km to 3 km from the forest fire area;
[0016] Step S200: In the first gliding stage, the second control module controls the tail servo module according to the signal of the photoelectric image seeker, locks the imaging information of the strongest fire source in real time, and guides the gliding fire-extinguishing bomb to fly to the forest fire area;
[0017] Step S300, in the second gliding stage, the first control module controls the tail servo module according to the signal of the optoelectronic image seeker to guide the gliding fire-extinguishing bomb to fly toward the target in the fire area, and controls the plasma excitation device to generate a plasma shock wave to detonate the high explosive column and the fire extinguishing agent.
[0018] The present invention is further described in detail below in conjunction with the accompanying drawings and specific embodiments. BRIEF DESCRIPTION OF THE DRAWINGS
[0019] Figure 1 This is a front view of the gliding fire-extinguishing bomb according to an embodiment of the present invention;
[0020] Figure 2 A top view of a gliding fire-extinguishing bomb according to an embodiment of the present invention;
[0021] Figure 3 This is a front view of the internal structure of the gliding fire-extinguishing bomb according to an embodiment of the present invention;
[0022] Figure 4 is a circuit block diagram of a second control module according to an embodiment of the present invention;
[0023] Figure 5 This is a schematic diagram of an aircraft carrying a gliding fire-extinguishing bomb in an embodiment of the present invention;
[0024] Figure 6 This is a schematic diagram of the guidance system after the aircraft carrying the gliding fire-extinguishing bomb is released according to an embodiment of the present invention.
[0025] Explanation of the accompanying drawings: 100 fire-extinguishing bomb body, 110 shell, 120 plasma excitation device, 130 high explosive column, 140 fire extinguishing agent, 150 electrode plug, 160 mounting hole, 200 optoelectronic image seeker, 210 blister cover, 220 camera pan / tilt, 230 camera, 300 tail servo module, 310 directional servo, 320 pitch servo, 330 servo control unit, 400 first control module, 410 intelligent circuit board, 420 GC-Bus and antenna printed board, 500 second control module, 510 image microprocessor controller, 520 wireless data communication circuit, 530 display remote control operating system, 540 electric control mounting locking device, 600 glider module, 610 wing fixing plate, 620 left wing, 630 right wing. DETAILED DESCRIPTION
[0026] The embodiments of the present invention are described in detail below. Figures 1 to 5 The embodiment of the present invention provides an intrinsically safe gliding fire-extinguishing bomb, including a fire-extinguishing bomb body 100. Figure 3 The fire-extinguishing bomb body 100 includes a shell 110 and a plasma excitation device 120, a high explosive column 130 and a fire extinguishing agent 140 arranged in the shell 110. The high explosive column 130 is inserted into the fire extinguishing agent 140 and is wrapped by the fire extinguishing agent 140. The plasma excitation device 120 can generate a plasma shock wave to instantly detonate the high explosive column 130 and the fire extinguishing agent 140. The fire-extinguishing bomb can use the plasma excitation device 120 to generate a high-temperature, high-pressure, and high-speed plasma shock wave to directly detonate the high explosive column 130 and the fire extinguishing agent 140, thereby forming a large-area explosion ultra-fine aerosol shock wave, and cooperate with the chemical suppression fire extinguishing mechanism to achieve efficient fire extinguishing. Since the fire-extinguishing bomb uses a pure electric energy to trigger the plasma excitation device 120, the intrinsically safe plasma excitation device 120 is a pure electric energy discharge device. The discharge device can generate a plasma shock wave to detonate the high explosive column 130 and the fire extinguishing agent 140, which can replace the existing traditional detonator fuzes with dangerous explosives that are not intrinsically safe. Therefore, the gliding fire-extinguishing bomb does not need to install dangerous goods detonator fuzes with poor safety and high mechanical sensitivity. It has intrinsic safety in the whole process of production, transportation, storage and deployment, which improves the safety of the fire-extinguishing bomb in the whole process of production, transportation, storage and deployment. For the triggering time of the plasma excitation device 120, it can be achieved by temperature sensing, infrared sensing and shooting image information. The high explosive column 130 can be RDX, TNT, B high explosive or emulsion explosive, and the fire extinguishing agent 140 is a dry powder fire extinguishing agent 140 or a liquid fire extinguishing agent 140.
[0027] Further, refer to Figures 1 to 3The gliding fire-extinguishing bomb also includes an optoelectronic image seeker 200, a tail servo module 300 and a first control module 400. The optoelectronic image seeker 200 is arranged at the head of the fire-extinguishing bomb body 100, the tail servo module 300 is arranged at the tail of the fire-extinguishing bomb body 100, and the first control module 400 is arranged in the fire-extinguishing bomb body 100, and is electrically connected or signal-connected to the optoelectronic image seeker 200, the first control module 400 and the plasma excitation device 120; the optoelectronic image seeker 200 is used to detect the image of the forest fire area and transmit the signal to the first control module 400, and the first control module 400 can control the tail servo module 300 according to the signal of the optoelectronic image seeker 200 to guide the gliding fire-extinguishing bomb to fly to the forest fire area, and control the plasma excitation device 120 to generate plasma shock waves. The gliding fire-extinguishing bomb is provided with an optoelectronic image seeker 200. After being dropped, during the landing flight, the optoelectronic image seeker 200 can detect the image of the forest fire area, and control the tail servo module 300 through the first control module 400 to guide the fire-extinguishing bomb to fly to the forest water area. After flying to the target position, the electric energy stored in the high-voltage capacitor of the first control module 400 is instantly discharged in the central bridge foil of the plasma excitation device 120, generating a high-temperature, high-pressure, and high-speed plasma shock wave, directly detonating the high explosive column 130 and the fire extinguishing agent 140, thereby forming a large-area explosion ultrafine aerosol shock wave, and cooperating with the chemical suppression fire extinguishing mechanism to achieve efficient fire extinguishing.
[0028] The gliding fire-extinguishing bomb is mounted on an aircraft such as a manned helicopter, a fixed-wing aircraft or a large unmanned aerial vehicle and flies to the forest fire site. It is dropped from the air 1.5km to 3km away from the forest fire area. A second control module 500 is arranged in the cockpit of the aircraft, and the second control module 500 is connected to the optoelectronic image seeker 200 or the first control module 400 by signal. After the gliding fire-extinguishing bomb is dropped, in the first gliding stage, that is, the initial descent stage, the pilot manually and wirelessly remotely controls the second control module 500 to control the tail servo module 300 according to the signal of the optoelectronic image seeker 200. In the second gliding stage, that is, the final gliding stage, autonomous optoelectronic image navigation is adopted, and the first control module 400 controls the tail servo module 300 according to the signal of the optoelectronic image seeker 200. Among them, the first gliding stage is the initial gliding stage, and the second gliding stage is the final gliding stage. The gliding fire-extinguishing bomb is provided with an optoelectronic image seeker 200, a first control module 400, and a second control module 500. In the first gliding stage, the pilot can remotely control the tail servo module 300 through the second control module 500, and lock the imaging information at the strongest fire source in real time to guide the gliding fire-extinguishing bomb to fly to the target in the fire area. In the second gliding stage, the first control module 400 can autonomously navigate the image to fly to the fire area and detonate the gliding fire-extinguishing bomb to extinguish the fire. Therefore, the gliding fire-extinguishing bomb can be dropped from the air 1.5km to 3km outside the fire area, thereby ensuring that the aircraft does not need to fly over the forest fire site or project at close range, and can avoid the risk of crashing caused by the inability of the aircraft to effectively control flight due to the violent disturbance of the rising strong hot air flow.
[0029] The tail fins of some fire-fighting bombs in the prior art use controlled or uncontrolled "X"-shaped tail fins with small lift. The fire-fighting bombs with controlled "X" tail fins use a high-cost composite guidance system, with SINS+GNSS guidance used for mid-course guidance and semi-strapdown infrared imaging guidance (strapdown inertial navigation+satellite navigation+semi-strapdown infrared imaging navigation) used for terminal guidance, which is relatively expensive. The fire-fighting bombs with uncontrolled "X" tail fins need to be projected at close range, and due to the violent disturbance caused by the rising of strong thermal air currents, the aircraft may be easily uncontrollable, resulting in a serious accident of a crash. The fire-extinguishing bomb of the present invention adopts pure electric energy plasma impact to detonate high explosives and fire extinguishing agents, a glider wing with large lift force and a low-cost guidance system, so that it can be dropped from the air 1.5km to 3km away from the forest fire area. The pilot's manual wireless remote control navigation is adopted for the initial descent stage guidance, and the fire-extinguishing bomb's autonomous photoelectric image navigation is adopted for the terminal stage guidance, thereby ensuring that the aircraft does not need to fly over the forest fire scene or be dropped at close range, and can avoid the risk of crashing caused by the inability to effectively control the flight of the aircraft due to the violent disturbance of the rising strong hot air flow. At the same time, there is no need to install explosive fuses with poor safety and high mechanical sensitivity. Therefore, it is inherently safe in the whole process of production, transportation, storage and delivery and use, thereby improving the safety of the fire-extinguishing bomb in the whole process of production, transportation, storage and delivery and use.
[0030] Furthermore, the gliding fire-extinguishing bomb also includes a glider module 600, which includes a wing fixing plate 610, a left wing 620 and a right wing 630. The wing fixing plate 610 is arranged on the top of the fire-extinguishing bomb body 100, and the left wing 620 and the right wing 630 are respectively arranged on the left and right sides of the fire-extinguishing bomb body 100. The left wing 620 and the right wing 630 can adopt folding wings. The tail servo module 300 includes a directional servo 310, a pitch servo 320 and a servo control unit 330. The left and right swing angle of the directional servo 310 is α, and the pitch swing angle of the pitch servo 320 is β. The servo control unit 330 is electrically connected or signal-connected to the directional servo 310, the pitch servo 320, the first control module 400 and the second control module 500. The outer cover of the fire-extinguishing bomb body 100, the gliding wing module 600, the tail servo module 300 and the photoelectric image seeker 200 are all made of engineering plastics. The gliding fire-extinguishing bomb controls the flight of the gliding fire-extinguishing bomb through the gliding wing module 600 and the tail servo module 300, so that the gliding fire-extinguishing bomb does not rotate during the delivery and descent process, so the low-cost navigation technology can be used to achieve the precise delivery of the gliding fire-extinguishing bomb.
[0031] Further, refer to Figure 3The first control module 400 includes an intelligent circuit board 410 and a GC-Bus and antenna printed board 420. The intelligent circuit board 410 is electrically connected or signal-connected to the optoelectronic image seeker 200, and the intelligent circuit board 410 is connected to the GC-Bus and the antenna printed board 420 via a two-wire communication bus GC-Bus and a wireless communication radio frequency line. The GC-Bus and the antenna printed board 420 are installed in the fire-extinguishing bomb body 100, and the GC-Bus and the antenna printed board 420 are connected to the steering gear control unit 330 via a two-wire communication bus GC-Bus. The steering gear control unit 330 includes a rudder, a pitch rudder electronic control part and a battery power supply part. The GC-Bus in the GC-Bus and antenna printed board 420 is a two-wire GC-Bus (Guidance control Bus) for digital communication and power supply sharing between the steering engine control unit 330 and the intelligent circuit board 410, wherein the GC-Bus and antenna printed board 420 is a long strip printed circuit board, and the printed circuit board is printed with a two-wire GC-Bus bus and a wireless communication antenna. Further, the photoelectric image seeker 200 includes a blister cover 210 connected to the housing 110, a camera platform 220 disposed in the blister cover 210, and a camera 230 disposed on the camera platform 220, and the camera 230 is electrically connected or signal-connected to the first control module 400. The blister cover 210 can be integrally formed with the housing 110 of the optoelectronic image seeker 200 . The camera 230 is electrically connected to the intelligent circuit board 410 . The intelligent circuit board 410 is electrically connected to the electrode plug 150 . The electrode plug 150 is electrically connected to the plasma excitation device 120 .
[0032] Further, refer to Figure 4 The second control module 500 includes an image microprocessor controller 510, a wireless data communication circuit 520, a display remote control operating system 530 and an electric mounted locking device 540; the first interface, the second interface and the third interface of the image microprocessor controller 510 are respectively connected to the wireless data communication circuit 520, the display remote control operating system 530 and the electric mounted locking device 540, and the wireless data communication circuit 520 is connected to the first control module 400 by signal. Further, the first interface of the image microprocessor controller 510 is connected to the wireless data communication circuit 520, the antenna in the wireless data communication line and the GC-Bus in the gliding fire-extinguishing bomb and the antenna printed board 420 perform wireless data communication, and transmit the image information of the optoelectronic image seeker 200 in the gliding fire-extinguishing bomb and the flight control information of the steering engine control unit 330. The second interface of the image microprocessor controller 510 is connected to the display remote control operating system 530, which is the interface for the driver to control the release of the gliding fire-extinguishing bomb, and the driver to observe the fire image and manually remotely control the flight of the gliding fire-extinguishing bomb.
[0033] Further, refer to Figure 1 and Figure 5 The electric-controlled mounting lock device 540 includes a spring, an electromagnetic coil and an electric latch. A mounting hole 160 is provided on the top of the fire-extinguishing bomb body 100. When the electromagnetic coil is not energized, the electric latch is inserted into the mounting hole 160 by the action of the spring. When the electromagnetic coil is energized, the electric latch is pulled out of the mounting hole 160, and the gliding fire-extinguishing bomb is launched. There are two electric latches and two mounting holes 160. When launching the gliding fire-extinguishing bomb, the two electric latches are pulled out of the mounting hole 160 at the same time to launch the gliding fire-extinguishing bomb.
[0034] The embodiment of the present invention also provides a method for controlling the delivery of an intrinsically safe gliding fire-extinguishing bomb, comprising the following steps:
[0035] Step S100: The gliding fire-extinguishing bomb is mounted on an aircraft and flies to the forest fire site, and is dropped from the air at a distance of 1.5 km to 3 km from the forest fire area;
[0036] Step S200: In the first gliding stage (initial descent stage), the pilot manually and wirelessly remotely controls the second control module 500 to control the tail servo module 300 according to the signal of the optoelectronic image seeker 200, and locks the imaging information of the strongest fire source in real time, guiding the gliding fire-extinguishing bomb to fly to the forest fire area;
[0037] Step S300, in the second gliding stage (the final gliding stage), autonomous optoelectronic image navigation is adopted, and the first control module 400 autonomously controls the tail servo module 300 according to the signal of the optoelectronic image seeker 200 to guide the gliding fire-extinguishing bomb to fly toward the target in the fire area, and controls the plasma excitation device 120 to generate a plasma shock wave to detonate the high explosive column 130 and the fire extinguishing agent 140.
[0038] Therefore, the gliding fire-extinguishing bomb adopts a pure electric energy-triggered plasma excitation device 120, and does not need to install a dangerous detonator fuse with poor safety and high mechanical sensitivity. Therefore, it is inherently safe in the entire process of production, transportation, storage, and delivery, which improves the safety of the fire-extinguishing bomb in the entire process of production, transportation, storage, and delivery. It can be dropped from the air 1.5km to 3km outside the fire area, thereby ensuring that the aircraft does not need to fly over the forest fire site or project at close range, and can avoid the risk of crashing caused by the violent disturbance of the rising strong hot air flow that causes the aircraft to be unable to effectively control the flight. The gliding fire-extinguishing bomb controls the flight of the gliding fire-extinguishing bomb through the gliding wing module 600 and the tail wing servo module 300, so that the gliding fire-extinguishing bomb does not rotate during the delivery and descent process, so low-cost navigation technology can be used to achieve accurate delivery of the gliding fire-extinguishing bomb.
[0039] After the gliding fire-extinguishing bomb is released, the pilot can remotely control the tail servo module 300 through the second control module 500 in the first gliding stage, and lock the imaging information of the strongest fire source in real time to guide the gliding fire-extinguishing bomb to fly to the target in the fire area. In the second gliding stage, the first control module 400 can autonomously navigate the image to fly to the fire area and detonate the gliding fire-extinguishing bomb to extinguish the fire. Therefore, the gliding fire-extinguishing bomb is an intrinsically safe, low-cost, easy-to-control gliding fire-extinguishing bomb that can be released over a long range and can accurately and quickly extinguish fires in forest areas.
[0040] Further, refer to Figure 6 , the schematic diagram of the guidance system of the aircraft after the gliding fire-extinguishing bomb is dropped, wherein ① the altitude H=0.5Km-2Km where the aircraft drops the gliding fire-extinguishing bomb in the air; ② the gliding guidance system for the descent of the gliding fire-extinguishing bomb in the IS stage, which is the wireless remote control navigation of the pilot; ③ the guidance system for the gliding fire-extinguishing bomb in the terminal stage of the FP, which is the autonomous navigation of the photoelectric image of the fire source area; ④ is the fire source area; the horizontal distance L=1.5Km-3Km from the fire source area to the place where the aircraft drops the gliding fire-extinguishing bomb in the air.
[0041] It should be noted that in the description of the present invention, if there are any orientation descriptions, such as up, down, front, back, left, right, etc., the orientations or positional relationships indicated are all based on the orientations or positional relationships shown in the drawings. They are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed or operated in a specific orientation, and cannot be understood as a limitation on the present invention.
[0042] In the description of the present invention, "several" means one or more, "more" means two or more, "greater than", "less than", "exceed" etc. are understood to exclude the number itself, and "above", "below", "within" etc. are understood to include the number itself. If there is a description of "first" or "second", it is only used to distinguish the technical features, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features or implicitly indicating the order of the indicated technical features.
[0043] In the description of the present invention, unless otherwise clearly defined, terms such as setting, installing, connecting, etc. should be understood in a broad sense, and technicians in the relevant technical field can reasonably determine the specific meanings of the above terms in the present invention based on the specific content of the technical solution.
[0044] The above-mentioned embodiments are only preferred embodiments of the present invention and cannot be used to limit the scope of protection of the present invention. Any non-substantial changes and substitutions made by technicians in this field on the basis of the present invention shall fall within the scope of protection required by the present invention.
Claims
1. An intrinsically safe gliding fire-fighting bomb, which is mounted on an aircraft and flies to the forest fire site, and is dropped from the air 1.5km to 3km away from the forest fire area, characterized in that: It comprises a fire-extinguishing bomb body (100), an optoelectronic image seeker (200), a tail servo module (300) and a first control module (400); The fire-extinguishing bomb body (100) comprises an outer shell (110), and a plasma excitation device (120), a high explosive column (130) and a fire extinguishing agent (140) arranged in the outer shell (110); the high explosive column (130) is inserted in the fire extinguishing agent (140); the plasma excitation device (120) can generate a plasma shock wave to detonate the high explosive column (130) and the fire extinguishing agent (140); The photoelectric image seeker (200) is arranged at the head of the fire-extinguishing bomb body (100), the tail servo module (300) is arranged at the tail of the fire-extinguishing bomb body (100), and the first control module (400) is arranged in the fire-extinguishing bomb body (100) and is electrically connected or signal-connected to the photoelectric image seeker (200), the first control module (400) and the plasma excitation device (120); The photoelectric image seeker (200) is used to detect an image of a forest fire area and transmit a signal to the first control module (400). The first control module (400) can control the tail servo module (300) according to the signal of the photoelectric image seeker (200) to guide the gliding fire-extinguishing bomb to fly toward the forest fire area, and control the plasma excitation device (120) to generate a plasma shock wave.
2. The intrinsically safe gliding fire-extinguishing bomb according to claim 1 is characterized in that: A second control module (500) is provided in the cockpit of the aircraft. The second control module (500) is connected to the photoelectric image seeker (200) and the tail servo module (300) by signal. The second control module (500) can control the tail servo module (300) according to the signal of the photoelectric image seeker (200) to guide the gliding fire-extinguishing bomb to fly to the forest fire area.
3. The intrinsically safe gliding fire-extinguishing bomb according to claim 2 is characterized in that: It also includes a glider module (600), the glider module (600) includes a wing fixing plate (610), a left wing (620) and a right wing (630), the wing fixing plate (610) is arranged on the top of the fire extinguishing bomb body (100), and the left wing (620) and the right wing (630) are respectively arranged on the left and right sides of the fire extinguishing bomb body (100); The tail servo module (300) comprises a directional servo (310), a pitch servo (320) and a servo control unit (330); the servo control unit (330) is electrically connected or signal-connected to the directional servo (310), the pitch servo (320), the first control module (400) and the second control module (500).
4. The intrinsically safe gliding fire-extinguishing bomb according to claim 3 is characterized in that: The first control module (400) comprises an intelligent circuit board (410) and a GC-Bus and antenna printed board (420), wherein the intelligent circuit board (410) is electrically connected or signal-connected to the optoelectronic image seeker (200), and the intelligent circuit board (410) is connected to the GC-Bus and antenna printed board (420) via a two-wire communication bus GC-Bus and a wireless communication radio frequency line, and the GC-Bus and antenna printed board (420) are connected to the steering gear control unit (330) via the two-wire communication bus GC-Bus.
5. The intrinsically safe gliding fire-extinguishing bomb according to claim 3 is characterized in that: The left wing (620) and the right wing (630) are foldable wings.
6. The intrinsically safe gliding fire-extinguishing bomb according to claim 2 is characterized in that: The second control module (500) comprises an image microprocessor controller (510), a wireless data communication circuit (520), a display remote control operating system (530) and an electrically controlled mounting locking device (540); The first interface, the second interface and the third interface of the image microprocessor controller (510) are respectively connected to the wireless data communication circuit (520), the display remote control operating system (530) and the electric-controlled mounting locking device (540), and the wireless data communication circuit (520) is signal-connected to the first control module (400).
7. The intrinsically safe gliding fire-extinguishing bomb according to claim 6 is characterized in that: The electrically controlled mounting locking device (540) comprises a spring, an electromagnetic coil and an electric latch. A mounting hole (160) is provided on the top of the fire-extinguishing bomb body (100). When the electromagnetic coil is not energized, the electric latch is inserted into the mounting hole (160) by the action of the spring. When the electromagnetic coil is energized, the electric latch is pulled out of the mounting hole (160) and the gliding fire-extinguishing bomb is released.
8. The intrinsically safe gliding fire-extinguishing bomb according to any one of claims 1 to 7, characterized in that: The photoelectric image seeker (200) comprises a blister outer cover (210) connected to the housing (110), a camera platform (220) disposed in the blister outer cover (210), and a camera (230) disposed on the camera platform (220), wherein the camera (230) is electrically connected or signal-connected to the first control module (400).
9. The intrinsically safe gliding fire-extinguishing bomb according to any one of claims 1 to 7, characterized in that: The high explosive column (130) is RDX, TNT, B high explosive or emulsion explosive, and the fire extinguishing agent (140) is dry powder fire extinguishing agent (140) or liquid fire extinguishing agent (140).
10. A method for controlling the delivery of an intrinsically safe gliding fire-extinguishing bomb, comprising the following steps: Step S100: The gliding fire-extinguishing bomb is mounted on an aircraft and flies to the forest fire site, and is dropped from the air at a distance of 1.5 km to 3 km from the forest fire area; Step S200: In the first gliding stage, the second control module (500) controls the tail servo module (300) according to the signal of the photoelectric image seeker (200), locks the imaging information of the strongest fire source in real time, and wirelessly remotely guides the gliding fire-extinguishing bomb to fly to the forest fire area; Step S300: In the second gliding stage, the first control module (400) controls the tail servo module (300) according to the signal of the photoelectric image seeker (200), guides the gliding fire-extinguishing bomb to fly toward the target in the fire area, and controls the plasma excitation device (120) to generate a plasma shock wave to detonate the high explosive column (130) and the fire extinguishing agent (140).