CN217032193U - Integrated airborne intelligent fire extinguishing system for high-rise building - Google Patents
Integrated airborne intelligent fire extinguishing system for high-rise building Download PDFInfo
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Abstract
The utility model relates to an integrated airborne intelligent fire extinguishing system for a high-rise building, and belongs to the technical field of fire extinguishing devices. The fire extinguishing system comprises a fire extinguishing device, an airborne hanger device, observing and aiming equipment and ground remote control equipment; the fire extinguishing device is mounted on the airborne hanger device, the observing and aiming equipment is mounted on the airborne hanger device, the fire extinguishing device is connected with the observing and aiming equipment through an aviation plug, and the fire extinguishing device is launched through ground remote control equipment; the observing and aiming equipment comprises a laser range finder, a camera device and an information transceiver, and the range information and the image information are transmitted to the ground remote control equipment through the information transceiver; the ground remote control equipment is independent of the fire extinguishing device, the airborne hanging device and the observing and aiming equipment and is operated by ground personnel. The fire extinguishing system can be used as an independent system and is mounted on an unmanned aerial vehicle platform through a mechanical interface and an electrical interface, is not restricted by a carrier platform and other equipment, and is not restricted by a fire scene environment and a launching space.
Description
Technical Field
The utility model relates to an integrated airborne intelligent fire extinguishing system for a high-rise building, and belongs to the technical field of fire extinguishing devices.
Background
With the rapid increase of the number of high-rise buildings in cities, the occurrence probability of high-rise fire risks also increases year by year. The fire extinguishing operation is adversely affected by the high ignition point of the high-rise fire danger, the complex traffic environment below the high-rise building and other conditions.
Aiming at the fire rescue task of high-rise buildings, the existing airborne track launches high-rise building emergency rescue bombs and a bomb-throwing type high-rise building dry powder fire truck. Chinese patent application CN202010138152.3 relates to an airborne track-launched high-rise building emergency rescue bomb, which is composed of a power module, a load module and a blasting dispersion module, and is mainly characterized in that: and aiming at the fire type, rapidly assembling matched emergency rescue bullets for targeted disposal. The operation flow is as follows: and when the fire disaster area arrives at a fire disaster site, analyzing the fire disaster type, quickly assembling emergency rescue bombs, mounting the bombs into an airborne track, and taking off the airborne to execute a launching task. However, the rescue bomb adopts an explosion type scattering mode, although a time delay device is arranged in the rescue bomb, the time sequence of the time delay device cannot be adjusted in real time, so that the shooting distance of the rescue bomb is limited, and the rescue bomb cannot be adjusted according to the distance between buildings. In addition, the rescue bomb adopts airborne launching, but an outer ballistic shooting table is not provided, so that the rescue bomb cannot be compatible with a viewing and aiming device.
The other scheme relates to a projectile type high-rise building dry powder fire truck, the design of the fire truck mainly refers to the mature technology of a vehicle-mounted missile system and integrates the aerospace launching technology, the control technology and the information processing technology, the fire fighting equipment is integrated with all equipment by a single truck, can be independently and flexibly deployed, and adopts a mode of launching fire extinguishing bombs to implement high-precision and high-efficiency fire fighting on high-rise and super high-rise building in urban environment, so that the fire behavior is suppressed in a large area, and the fire behavior is controlled to spread. When the high-rise fire-extinguishing task is executed, the projectile-throwing type high-rise dry powder fire engine runs to a fire scene, a proper ground launching position is selected, and finally, the fire-fighting rescue task is executed according to a field instruction. The projectile type high-rise building dry powder fire truck adopts a ground mode to launch fire extinguishing bombs, so that the fire extinguishing bombs and fire scene targets are not on the same plane, enough space needs to be reserved during launching, the space between high-rise buildings in a city is limited, the surrounding environment of the fire scene is complex, and the sufficient launching space cannot be provided, so that the rescue time can be delayed; in addition, the use cost of the throwing type high-rise building dry powder fire engine is high.
Disclosure of Invention
In view of the above, the present invention provides an integrated intelligent fire extinguishing system on board a high-rise building, which can be mounted on an unmanned aerial vehicle platform as an independent system through a mechanical interface and an electrical interface, and therefore is not restricted by a carrier platform and other devices, and can also be launched in the air at a small range (between buildings), and therefore is not restricted by a fire scene environment and a launching space.
In order to achieve the purpose of the utility model, the following technical scheme is provided.
An integrated airborne intelligent fire extinguishing system for high-rise buildings comprises a fire extinguishing device, an airborne hanger device, observing and aiming equipment and ground remote control equipment; the fire extinguishing device is mounted on the airborne hanger device, the observing and aiming equipment is mounted on the airborne hanger device, the fire extinguishing device is connected with the observing and aiming equipment through an aviation plug, and the fire extinguishing device is launched through ground remote control equipment; the observing and aiming equipment comprises a laser range finder, a camera device and an information receiving and transmitting device, wherein the laser range finder is used for measuring the shooting distance information of a target wall body and the fire extinguishing system, the camera device is used for shooting the image information of a fire scene, and the shooting distance information and the image information are transmitted to the ground remote control equipment through the information receiving and transmitting device; the ground remote control equipment is independent of the fire extinguishing device, the airborne hanging device and the observing and aiming equipment and is operated by ground personnel.
Furthermore, the fire extinguishing device comprises more than one uncontrolled rocket projectile powered by a solid rocket engine; fire extinguishing agents and a central blasting and sowing mechanism are loaded in each uncontrolled rocket projectile, and a time sequence device is arranged and connected with the central blasting and sowing mechanism through an electrical interface; the axial direction of the body of the uncontrolled rocket projectile is provided with a front sliding block and a rear sliding block which are used for being connected with the airborne pylon device, and the front sliding block and the rear sliding block are positioned on the same horizontal line.
Further, the airborne hanging device comprises a guide rail and a locking mechanism, wherein the locking mechanism is installed on the guide rail through a mechanical interface I; the locking mechanism is interlocked with an ignition circuit in the aviation plug; the airborne hanging rack device is further provided with a mechanical interface II for carrying observing and aiming equipment.
Furthermore, the guide rail is of a T-U-shaped structure, and the locking mechanism is of a push-pull electromagnetic mechanism and is interlocked with an ignition circuit in the aviation plug.
Furthermore, the observing and aiming device also comprises a single chip microcomputer, and an outer ballistic firing table is stored in the single chip microcomputer; the outer ballistic firing table gives corresponding information of the firing distance and the hitting position of the fire extinguishing device and corresponding information of the firing distance and the time sequence of the fire extinguishing device; the range information measured by the laser range finder and the real-time image shot by the camera device are fed back to the singlechip; the single chip microcomputer obtains a target shooting position according to the shooting distance information and the hit position information of the uncontrolled rocket projectile in the fire extinguishing device, which is given by the built-in external ballistic shooting meter; the singlechip displays the target shooting position information on a real-time image obtained by the camera device and sends the target shooting position information to the ground remote control equipment through the signal receiving and sending device; in addition, the singlechip outputs a control signal to a time sequence device loaded on the uncontrolled rocket projectile according to the time sequence time corresponding to different shooting distances given by the shooting distance information by referring to the built-in outer ballistic shooting table so as to adjust the time sequence time of the time sequence device in real time; the information transceiver is also used for receiving the instruction of the ground remote control equipment, then transmitting the instruction to the singlechip, and the singlechip outputs a signal to unlock the locking mechanism and launch the uncontrolled rocket projectile in the fire extinguishing device.
Furthermore, the ground remote control equipment comprises ground signal transceiving equipment and touch screen type operating equipment, and the touch screen type operating equipment transmits information with the ground signal transceiving equipment in a wireless signal transmission mode; the ground signal transceiver is used for receiving a real-time target picture and a target shooting position sent by an information transceiver in the observing and aiming equipment and transmitting the information to the touch screen type operating equipment, an operator adjusts the position of the carrier according to the target shooting position and sends an instruction through the touch screen type operating equipment, instruction information is transmitted to the information transceiver of the observing and aiming equipment through the ground signal transceiver, the information transceiver of the observing and aiming equipment transmits the information to the single chip microcomputer after receiving the instruction, a transmitting instruction is output through the single chip microcomputer, and the fire extinguishing device shoots a target.
After the fire extinguishing system is integrated, the fire extinguishing system is mounted on a carrier platform, the carrier takes off and flies to a fire scene of a high-rise building, and a camera device of the observing and aiming equipment collects a real-time image and transmits the real-time image to ground remote control equipment; the laser range finder of observation and aiming equipment gathers the range information between target wall body and the fire extinguishing systems to transmit it to ground remote control equipment, ground operating personnel adjust the position of carrier according to the real-time image and the range information of observation and aiming equipment feedback, when ground operating personnel think can launch extinguishing device, send the instruction through ground remote control equipment, make extinguishing device launch to target fire scene department, put out a fire.
Further, when the sighting device further comprises a single chip microcomputer, an outer ballistic firing table is stored in the single chip microcomputer; the outer ballistic firing table gives corresponding information of the firing distance and the hitting position of the fire extinguishing device and corresponding information of the firing distance and the firing time of the fire extinguishing device; after the fire extinguishing system is integrated, the fire extinguishing system is mounted on a carrier platform, a carrier takes off and flies to a fire scene of a high-rise building, a camera device of a sighting device collects a real-time image, a laser range finder collects the range information between a target wall and the fire extinguishing system, the real-time image and the range information are transmitted to a single chip microcomputer, the range information is analyzed by the single chip microcomputer, and the target shooting position is obtained according to the hitting position information of a non-controlled rocket projectile in the fire extinguishing device, which is given by a built-in external ballistic firing watch; the singlechip processes the target shooting position and the real-time image obtained by the camera device, so that the target position information is displayed on the real-time image in the form of an indication cursor and is sent to the ground remote control equipment through the signal transceiver; the ground operator adjusts the position of the carrier according to a real-time image fed back by a camera device of the sighting device and the sighting information of the target shooting position, so that a sighting indication cursor is positioned at the center of the target; after the adjustment is finished, when the fire extinguishing device can be launched, a ground operator sends an instruction through touch screen type operating equipment of ground remote control equipment, the observing and aiming equipment outputs ignition current to an uncontrolled rocket projectile in the fire extinguishing device after receiving the instruction, the uncontrolled rocket projectile accelerates after being ignited, hits a target shooting position and penetrates through a glass curtain wall to enter a fire scene, and the uncontrolled rocket projectile is provided with a time sequence device, so that the spreading time of a central blasting spreading mechanism can be controlled, the fire extinguishing agent can be spread when the uncontrolled rocket projectile is in the middle of the fire scene, and the fire extinguishing agent is dispersed to the periphery for fire extinguishing; after one uncontrolled rocket projectile is launched, the carrier stays in situ to observe the fire scene, if open fire or reburning condition still exists, the uncontrolled rocket projectile in the fire extinguishing device can be continuously launched into the fire scene according to the operation until the fire is controlled.
Advantageous effects
1. The utility model provides an integrated airborne intelligent fire extinguishing system for a high-rise building, which integrates a fire extinguishing device, an airborne hanger device, observing and aiming equipment and ground remote control equipment, can be used as an independent system and is hung on an unmanned aerial vehicle platform through a mechanical interface and an electrical interface, and is not constrained by an airborne platform and other equipment. When the fire extinguishing system is used for launching, the fire extinguishing device in the fire extinguishing system and a fire scene are positioned on the same plane, and the fire extinguishing system can launch in the air at a small distance (between buildings), so that the fire extinguishing system is not limited by the fire scene environment and launching space, and quick rescue can be realized. In addition, the airborne hanging rack device, the observing and aiming equipment and the ground remote control equipment can be repeatedly used, the consumption of each task or training is only the fire extinguishing device, and the fire extinguishing device can greatly reduce the production cost by means of the existing batch cost control measures, so that the use cost is reduced.
2. The fire extinguishing device is provided with a time sequence device, and the time sequence device is connected with the central blasting sowing mechanism through an electrical interface and used for controlling the sowing time of the central blasting sowing mechanism.
3. The locking mechanism in the airborne hanger device is interlocked with the ignition circuit in the aviation plug, so that the situation that the fire extinguishing device is ignited by mistake when unlocking fails is avoided.
4. The guide rail in the airborne hanging device adopts a T-U type structure so as to realize that the front and rear sliders on the uncontrolled rocket projectile are simultaneously off-orbit, thereby improving the hit precision;
5. the single chip microcomputer in the observing and aiming equipment is provided with the parameters of the outer trajectory firing chart of the uncontrolled rocket projectile in the built-in fire extinguishing device, and can be matched with corresponding time sequence time according to different firing distance information, so that the fire extinguishing system has a time sequence intelligent binding function, the launch of the uncontrolled rocket projectile in the fire extinguishing device is not limited by the firing distance of a fire scene, and the uncontrolled rocket projectile can be launched at any time in an effective firing range.
Drawings
Fig. 1 is a schematic structural diagram of a fire extinguishing system integrated with a fire extinguishing device, an onboard hanging rack device and a viewing and aiming device.
FIG. 2 is a schematic view of the structure of the uncontrolled rocket projectile of the present invention.
The system comprises a fire extinguishing device 1, an onboard hanger device 2, a viewing and aiming device 3, a time sequence device 4, a central blasting and spreading mechanism 5, an ultrafine dry powder extinguishing agent 6, a solid rocket engine 7, a front sliding block 8 and a rear sliding block 9.
Detailed Description
The utility model is further illustrated but not limited by the following description of embodiments in connection with the accompanying drawings.
As shown in fig. 1-2, an integrated airborne intelligent fire extinguishing system for high-rise buildings comprises a fire extinguishing device 1, an airborne hanger device 2, a sighting device 3 and a ground remote control device; the fire extinguishing device 1 is mounted on a guide rail of the airborne hanger device 2, the observing and aiming equipment 3 is mounted on the airborne hanger device 2, the fire extinguishing device 1 is connected with the observing and aiming equipment 3 through an aviation plug, and the fire extinguishing device 1 is launched through ground remote control equipment; the observing and aiming equipment 3 comprises a laser range finder, a camera device and an information transmitting and receiving device, wherein the laser range finder is used for measuring the range information of a target wall body and a fire extinguishing system, the camera device is used for shooting image information of a fire scene, and the range information and the image information are transmitted to ground remote control equipment through the information transmitting and receiving device; the ground remote control equipment is independent of the fire extinguishing device 1, the airborne hanging device 2 and the observing and aiming equipment 3 and is operated by ground personnel.
The fire extinguishing device 1 is an execution unit for high-rise building fire rescue, and comprises four uncontrolled rocket projectiles taking a solid rocket engine 7 as power; each uncontrolled rocket projectile is internally loaded with superfine dry powder extinguishing agents 6 and a central blasting and scattering mechanism 5, the central blasting and scattering mechanism 5 is arranged at the center of the uncontrolled rocket projectile, and the superfine dry powder extinguishing agents 6 are arranged around the central blasting and scattering mechanism 5; a time sequence device 4 is also arranged in each uncontrolled rocket projectile, and the time sequence device 4 is connected with a central blasting and sowing mechanism 5 through an electrical interface; the front sliding block 8 and the rear sliding block 9 are arranged along the axial direction of the projectile body of the uncontrolled rocket projectile and are used for being connected with a guide rail in the airborne pylon device 2, and the front sliding block 8 and the rear sliding block 9 are positioned on the same horizontal line.
The airborne hanging rack device 2 comprises a guide rail and a locking mechanism, and the locking mechanism is arranged on the guide rail through a mechanical interface I; the guide rail adopts a T-U type structure to realize that the front slide block 8 and the rear slide block 9 on the uncontrolled rocket projectile simultaneously leave the orbit, thereby improving the hit precision; the locking mechanism adopts a push-pull electromagnetic mechanism and is interlocked with an ignition circuit in the aviation plug, so that the condition that the fire extinguishing device 1 is ignited by mistake when the unlocking fails is avoided; in addition, the airborne hanger device 2 is further provided with a mechanical interface II for carrying the observing and aiming equipment 3.
The sighting device 3 also comprises a singlechip, and an outer ballistic firing table is stored in the singlechip; the functions of the sighting device 3 are mainly as follows: firstly, ranging, namely measuring the distance between a target wall and a fire extinguishing system in real time through a laser range finder, and feeding the measured range information back to a single chip microcomputer in real time; secondly, time sequence binding, namely, the singlechip outputs a control signal to a time sequence device 4 loaded on the uncontrolled rocket projectile according to time sequence time corresponding to different shooting distances given by the built-in outer ballistic shooting table according to the shooting distance information so as to adjust the time sequence time of the time sequence device 4 in real time; thirdly, shooting, wherein the shooting device shoots a target and feeds real-time image information back to the singlechip; fourthly, image processing, namely analyzing the shooting distance information by a single chip microcomputer, then obtaining a target shooting position according to the hitting position information of the uncontrolled rocket projectile in the fire extinguishing device 1 given by a built-in external ballistic shooting meter, processing the target shooting position and a real-time image obtained by a camera device by the single chip microcomputer, displaying the target position information on the real-time image, and sending the target position information to ground remote control equipment through a signal transceiving device; fifthly, an information receiving and sending device receives an instruction of the ground remote control equipment, then the instruction is transmitted to the single chip microcomputer, and the single chip microcomputer outputs a signal to unlock the locking mechanism and launch the uncontrolled rocket projectile in the fire extinguishing device 1.
The ground remote control equipment consists of ground signal transceiving equipment and touch screen type operating equipment, and the touch screen type operating equipment transmits information with the ground signal transceiving equipment in a wireless signal transmission mode; the ground signal transceiver is used for receiving a real-time target picture and a target shooting position sent by an information transceiver in the observing and aiming device 3 and transmitting the information to the touch screen type operating device, an operator adjusts the position of the carrier according to the target shooting position, after the adjustment is finished, the operator can send an instruction through the touch screen type operating device, instruction information is transmitted to the information transceiver of the observing and aiming device 3 through the ground signal transceiver, after the information transceiver of the observing and aiming device 3 receives the instruction, the information is transmitted to the single chip microcomputer, a launching instruction is output through the single chip microcomputer, and uncontrolled rocket projectiles in the fire extinguishing device 1 are launched off-track to hit a target.
After the fire extinguishing system is integrated, the fire extinguishing system is mounted on a carrier platform, the carrier takes off and flies to a fire scene of a high-rise building, and a camera device of the observing and aiming equipment 3 collects a real-time image and transmits the real-time image to a single chip microcomputer; the laser range finder of the sighting device 3 collects the shooting distance information between a target wall and the fire extinguishing system and then transmits the shooting distance information to the single chip microcomputer, on one hand, the single chip microcomputer outputs a control signal to a time sequence device 4 loaded on the uncontrolled rocket projectile according to the shooting distance information and time sequence time corresponding to different shooting distances given by a built-in outer ballistic firing schedule, so that the time sequence time of the time sequence device 4 is adjusted in real time; on the other hand, the singlechip analyzes the shooting distance information, then obtains a target shooting position according to the hitting position information of the uncontrolled rocket projectile in the fire extinguishing device 1 given by the built-in external ballistic shooting meter, processes the target shooting position and the real-time image obtained by the camera device, displays the target position information on the real-time image in the form of an indication cursor, and sends the target position information to the ground remote control equipment through the signal transceiver; the ground operator adjusts the position of the carrier according to the real-time image fed back by the camera device of the sighting device 3 and the sighting information of the target shooting position, so that the sighting indication cursor is positioned at the center of the target; the touch screen type operating equipment of the ground remote control equipment sends out an instruction, the observing and aiming equipment 3 outputs ignition current to the uncontrolled rocket projectile in the fire extinguishing device 1 after receiving the instruction, the uncontrolled rocket projectile accelerates and flies after igniting, hits a target shooting position and enters a fire scene through a glass curtain wall, and the uncontrolled rocket projectile is provided with a time sequence device 4, so that the spreading time of a central blasting spreading mechanism 5 can be controlled, the uncontrolled rocket projectile can spread the superfine dry powder fire extinguishing agent 6 when being in the middle of the fire scene, and the superfine dry powder fire extinguishing agent 6 can disperse and extinguish fire all around; after the uncontrolled rocket projectile is launched, the carrier stays in situ to observe the fire scene condition, if open fire or re-combustion condition still exists, the uncontrolled rocket projectile in the fire extinguishing device 1 can be continuously launched into the fire scene according to the operation until the fire behavior is controlled.
The present invention includes, but is not limited to, the above embodiments, and any equivalent substitutions or partial modifications made under the principle of the present invention should be considered within the scope of the present invention.
Claims (6)
1. The utility model provides an intelligent fire extinguishing systems of integrated form high-rise building machine carrier which characterized in that: the fire extinguishing system comprises a fire extinguishing device (1), an airborne hanging rack device (2), observing and aiming equipment (3) and ground remote control equipment; the fire extinguishing device (1) is mounted on the airborne hanger device (2), the observing and aiming equipment (3) is mounted on the airborne hanger device (2), the fire extinguishing device (1) is connected with the observing and aiming equipment (3) through an aviation plug, and the fire extinguishing device (1) is launched through ground remote control equipment; the observation and aiming equipment (3) comprises a laser range finder, a camera device and an information transceiving device, wherein the laser range finder is used for measuring the shooting distance information of a target wall body and the fire extinguishing system, the camera device is used for shooting the image information of a fire scene, and the shooting distance information and the image information are transmitted to the ground remote control equipment through the information transceiving device; the ground remote control equipment is independent of the fire extinguishing device (1), the airborne hanging rack device (2) and the observing and aiming equipment (3) and is operated by ground personnel.
2. The integrated airborne intelligent fire extinguishing system for high-rise buildings according to claim 1, characterized in that: the fire extinguishing device (1) comprises more than one uncontrolled rocket projectile which takes a solid rocket engine (7) as power; the fire extinguishing agent (6) and the central blasting scattering mechanism (5) are loaded in each uncontrolled rocket projectile, the time sequence device (4) is arranged, and the time sequence device (4) is connected with the central blasting scattering mechanism (5) through an electrical interface; a front sliding block (8) and a rear sliding block (9) are arranged in the axial direction of a projectile body of the uncontrolled rocket projectile and are used for being connected with an airborne pylon device (2), and the front sliding block (8) and the rear sliding block (9) are located on the same horizontal line.
3. The integrated airborne intelligent fire extinguishing system for high-rise buildings according to claim 1 or 2, characterized in that: the airborne hanging rack device (2) comprises a guide rail and a locking mechanism, wherein the locking mechanism is arranged on the guide rail through a mechanical interface I; the locking mechanism is interlocked with an ignition circuit in the aviation plug; the airborne hanging rack device (2) is further provided with a mechanical interface II for carrying the observing and aiming equipment (3).
4. The integrated airborne intelligent fire extinguishing system for high-rise buildings according to claim 3, characterized in that: the guide rail is of a T-U-shaped structure, and the locking mechanism is of a push-pull electromagnetic mechanism and is interlocked with an ignition circuit in the aviation plug.
5. The integrated airborne intelligent fire extinguishing system for high-rise buildings according to claim 3, characterized in that: the observing and aiming device (3) also comprises a singlechip, and an outer trajectory shooting meter is stored in the singlechip; the outer ballistic firing table gives corresponding information of the firing distance and the hitting position of the fire extinguishing device and corresponding information of the firing distance and the time sequence of the fire extinguishing device; the shooting range information measured by the laser range finder and the real-time image shot by the camera device are fed back to the single chip microcomputer; the single chip microcomputer obtains a target shooting position according to the shooting distance information and the hit position information of the uncontrolled rocket projectile in the fire extinguishing device (1) given by the built-in external ballistic shooting meter; the singlechip displays the target shooting position information on a real-time image obtained by the camera device and sends the target shooting position information to the ground remote control equipment through the signal receiving and sending device; in addition, the singlechip outputs a control signal to a time sequence device (4) loaded on the uncontrolled rocket projectile according to the time sequence time corresponding to different shooting distances given by the shooting distance information by referring to the built-in outer ballistic shooting table so as to adjust the time sequence time of the time sequence device (4) in real time; the information transceiver is also used for receiving the instruction of the ground remote control equipment, then transmitting the instruction to the single chip microcomputer, and the single chip microcomputer outputs signals to unlock the locking mechanism and launch the uncontrolled rocket projectile in the fire extinguishing device (1).
6. The integrated airborne intelligent fire extinguishing system for high-rise buildings according to claim 5, characterized in that: the ground remote control equipment comprises ground signal transceiving equipment and touch screen type operating equipment, and the touch screen type operating equipment transmits information with the ground signal transceiving equipment in a wireless signal transmission mode; the ground signal transceiver is used for receiving a real-time target picture and a target shooting position sent by an information transceiver in the sighting device (3) and transmitting the information to the touch screen type operating device, an operator adjusts the position of a carrier according to the target shooting position and sends an instruction through the touch screen type operating device, instruction information is transmitted to the information transceiver of the sighting device (3) through the ground signal transceiver, after the information transceiver of the sighting device (3) receives the instruction, the information is transmitted to the single chip microcomputer, the single chip microcomputer outputs a transmitting instruction, and the fire extinguishing device (1) shoots a target.
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| US20230308042A1 (en) * | 2022-01-27 | 2023-09-28 | Ameristar Solar, LLC | SOLAR eVTOL DRONE TOWER |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20230308042A1 (en) * | 2022-01-27 | 2023-09-28 | Ameristar Solar, LLC | SOLAR eVTOL DRONE TOWER |
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