Unmanned aerial vehicle high-altitude window breaking dry powder fire extinguishing equipment

Abstract

The invention belongs to the technical field of unmanned aerial vehicle application, and particularly relates to unmanned aerial vehicle high-altitude window breaking dry powder fire extinguishing equipment which comprises an unmanned aerial vehicle assembly, and a window breaking fire extinguishing assembly is carried at the bottom of the unmanned aerial vehicle assembly; the window breaking and fire extinguishing assembly comprises a base fixedly connected with the bottom of the unmanned aerial vehicle assembly; the material storage module is used for storing solid beads for window breaking and dry powder fire extinguishing balls; the transmitting module is used for transmitting solid beads or dry powder fire extinguishing balls for window breaking; and the conveying module is used for conveying the solid beads or the dry powder fire extinguishing balls for window breaking to the transmitting module from the storage module. When a high-rise fire occurs, the unmanned aerial vehicle assembly carries the window breaking and fire extinguishing assembly to fly to a specified height and then get close to an outer window of a high-rise building, solid beads for window breaking are conveyed and loaded to the transmitting module through the material storage module in advance, and the transmitting module transmits the solid beads for window breaking to break the outer window of the high-rise building. And then the dry powder fire extinguishing balls are conveyed to the transmitting module through the material storage module, the transmitting module transmits the dry powder fire extinguishing balls to a fire source, and then high-altitude window breaking and fire extinguishing operation of the unmanned aerial vehicle is achieved.

Description

Technical Field

[0001] The invention belongs to the technical field of unmanned aerial vehicle application, and in particular relates to a high-altitude window-breaking dry powder fire-extinguishing device for unmanned aerial vehicles. Background Art

[0002] In the face of urban development, a large number of high-rise buildings have been built and put into use. High-rise buildings are very high. If a fire occurs, it is very easy to form a chimney effect, and the fire will quickly spread from the lower floors to the higher floors. The use of fire-fighting equipment on the ground is limited: the water pressure is not enough, the fire hose is not easy to pull up to the floor where the fire occurs, and the ladder is slow to set up and it is difficult to reach the top floor. Therefore, it is difficult to extinguish fires in high-rise buildings. Firefighters climb high-rise buildings to extinguish fires on site, which is very likely to cause casualties and is very dangerous. At the same time, the roads along the way for fire trucks are often not smooth, and they are a certain distance apart. It takes a certain amount of time to arrive at the fire scene. Practice has proved that firefighting must race against time. Firefighting can only be effectively extinguished in the early stages of a fire. Once the fire spreads in large quantities and the fire increases sharply, firefighting will be powerless, which will cause immeasurable casualties and property losses.

[0003] With the development of drone technology, the use of drone technology to achieve high-altitude firefighting can not only respond to fires quickly, but also keep firefighters away from the fire source through remote operation to ensure safety. Therefore, there is an urgent need for a drone high-altitude window-breaking dry powder fire-fighting equipment to achieve the above functions. Summary of the invention

[0004] The purpose of the present invention is to provide an unmanned aerial vehicle high-altitude window-breaking dry powder fire-extinguishing device to solve the above-mentioned problems.

[0005] To achieve the above object, the present invention provides the following solutions:

[0006] A drone high-altitude window-breaking dry powder fire-extinguishing device includes a drone component, wherein the drone component is equipped with a window-breaking fire-extinguishing component at the bottom;

[0007] The window breaking fire extinguishing assembly comprises:

[0008] A base, fixedly connected to the bottom of the drone assembly;

[0009] Storage module, used to store solid beads and dry powder fire extinguishing balls for window breaking;

[0010] A launching module, used to launch solid beads or dry powder fire extinguishing balls for breaking windows;

[0011] The conveying module is used to convey the solid beads for window breaking or the dry powder fire extinguishing balls from the storage module to the launching module.

[0012] Optionally, the storage module includes two storage bins opened on the drone fuselage of the drone assembly, one of which is used to store solid beads for window breaking, and the other is used to store dry powder fire extinguishing balls, and the storage bins are connected to the feed end of the conveying module through a feed pipe;

[0013] The base is fixedly connected to the bottom of the UAV fuselage.

[0014] Optionally, the two storage bins are located on both sides of the conveying module respectively.

[0015] Optionally, the conveying module includes:

[0016] An electromagnetic stator ring, wherein the electromagnetic stator ring is fixedly connected to the base, and end covers are fixedly connected to both ends of the electromagnetic stator ring, and a feed port for feeding and a connecting hole for discharging are provided on the end covers, and the feed port is connected to the discharging end of the feed pipe;

[0017] The loading wheel is rotatably arranged in the electromagnetic stator ring, the electromagnetic stator ring is drivingly connected to the loading wheel, and a plurality of material holes circumferentially evenly spaced are opened on the loading wheel. The loading wheel rotates so that the two ends of one of the material holes are respectively connected with the two feed ports, and the two ends of another material hole are respectively connected with the two connecting holes.

[0018] Optionally, a plurality of electromagnetic sheets arranged at equal intervals in the circumferential direction are embedded in the inner wall of the electromagnetic stator ring, and the polarities of two adjacent electromagnetic sheets are opposite;

[0019] The side wall of the loading wheel disc is embedded with a plurality of permanent magnets arranged at equal intervals in the circumferential direction, and the polarities of two adjacent permanent magnets are opposite;

[0020] The electromagnetic sheet generates a magnetic field when energized and is magnetically connected to the permanent magnet sheet.

[0021] Optionally, the transmitting module includes:

[0022] A gun barrel, fixedly connected to one of the end covers, one end of the gun barrel being connected to the connecting hole of the corresponding end cover;

[0023] The air compression part is fixedly connected to the bottom of the drone fuselage, and the air outlet end of the air compression part is connected to the connecting hole of the other end cover.

[0024] Optionally, the air compression unit includes:

[0025] One end of the high-pressure air pipe is fixedly connected to the corresponding end cover, the high-pressure air pipe is connected to the corresponding connecting hole, the other end of the high-pressure air pipe is connected to an air compressor, and the fixed end of the air compressor is fixedly connected to the bottom of the UAV fuselage.

[0026] Optionally, the air compressor includes an air pump housing, the top of the air pump housing is fixedly connected to the bottom of the drone fuselage, and the bottom of the air pump housing is connected to the high-pressure air pipe;

[0027] A piston is vertically slidable in the air pump housing, and the piston divides the inner wall of the air pump housing into an active chamber located at the top and a gas compression chamber located at the bottom. The gas compression chamber is connected to the outside through a one-way valve, and the one-way valve is used to allow external air to enter the gas compression chamber when the piston rises; a second one-way valve is provided at the air inlet end of the high-pressure air pipe, and the second one-way valve is used to prevent the air in the high-pressure air pipe from flowing back to the gas compression chamber when the gas compression chamber is in the suction stage;

[0028] The piston is drivingly connected to a driving part for driving the piston to slide up and down.

[0029] Optionally, the driving part includes a crankshaft, the crankshaft is rotatably arranged in the air pump housing, one end of the crankshaft is axially connected to the output end of the motor, and the fixed end of the motor is fixedly connected to the outer wall of the air pump housing;

[0030] One end of a crankshaft connecting rod is hingedly connected to the middle of the crankshaft, and the other end of the crankshaft connecting rod is hingedly connected to the piston.

[0031] Optionally, a limiting slide is provided at the discharge end of the feed pipe, a slider is slidably connected to the top of the limiting slide, one end of a spring is fixedly connected to the bottom of the slider, the other end of the spring is fixedly connected to an electromagnet, the electromagnet is fixedly connected to the bottom of the limiting slide, the electromagnet is magnetically connected to the slider, when the electromagnet is started, it attracts the slider to compress the spring, the top of the slider is located on the inner side of the top of the limiting slide, when the electromagnet is closed, the spring is released, so that the top of the slider is located on the outer side of the top of the limiting slide, so as to prevent the solid beads or dry powder fire extinguishing balls for breaking windows from rolling.

[0032] Compared with the prior art, the present invention has the following advantages and technical effects:

[0033] During use, a drone component is used to carry a window breaking fire extinguishing component. When a high-rise fire occurs, the drone component carries the window breaking fire extinguishing component to a specified height and approaches the outer windows of the high-rise building. Solid beads for window breaking are first provided through the storage module, and the conveying module is used to convey the solid beads for window breaking and load them into the launching module. The launching module fires the solid beads for window breaking to shatter the outer windows of the high-rise building. Subsequently, the storage module conveys the dry powder fire extinguishing ball to the launching module through the conveying module, and the launching module launches the dry powder fire extinguishing ball to the fire source. After the dry powder fire extinguishing ball is dropped into the fire source, it explodes under the action of high temperature, and the dry powder inside it covers the fire source, thereby realizing the drone's high-altitude window breaking fire extinguishing operation. BRIEF DESCRIPTION OF THE DRAWINGS

[0034] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required for use in the embodiments are briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For those of ordinary skill in the art, other drawings can be obtained based on these drawings without creative labor:

[0035] Figure 1 It is a schematic diagram of the structure of the present invention;

[0036] Figure 2 It is a structural schematic diagram of another angle of the present invention;

[0037] Figure 3 It is a schematic diagram of the bottom structure of the present invention;

[0038] Figure 4 This is an exploded view of the window-breaking fire-extinguishing assembly of the present invention;

[0039] Figure 5 This is a structural diagram of the UAV fuselage of the present invention;

[0040] Figure 6 This is a structural diagram of the feed pipe of the present invention;

[0041] Figure 7 For the present invention Figure 6 A partial enlarged view of the middle part;

[0042] Figure 8 This is a structural diagram of the air compressor of the present invention;

[0043] Among them, 1. UAV component; 2. control module; 3. machine arm; 4. camera; 5. window breaking fire extinguishing component; 101. UAV fuselage; 102. storage bin; 501. gun barrel; 502. feed pipe; 503. base; 504. electromagnetic stator ring; 505. end cover; 506. feed port; 507. shaft connecting hole; 508. connecting hole; 509. loading wheel; 510. material hole; 511. shaft; 512. high-pressure gas pipe; 513. air pump housing; 514. limit slide; 515. slider; 516. spring; 517. electromagnet; 518. piston; 519. motor; 520. crankshaft; 521. crankshaft connecting rod; 522. one-way valve; 523. gas compression chamber; 524. second one-way valve. DETAILED DESCRIPTION

[0044] In the prior art, there is a kind of UAV high-altitude window breaking dry powder fire extinguishing equipment, which includes: a PLC controller, a platform, an air hammer nozzle assembly, a fire extinguishing silo assembly, a positioner, a V-shaped fork slider, a dry powder fire extinguisher, a striker, a thrust fan, a CCD camera, a gas cylinder, and a landing gear; a single device uses 2 to 20 dry powder fire extinguishers, one after another, for controllable chain-type full flooding fire extinguishing, or uses more than 2 devices to extinguish fires in turns. After the dry powder fire extinguisher is used up, the device can fall to the ground to replace the dry powder fire extinguisher and put it into fire extinguishing again, which can make the fire extinguishing chain continue for a long time. The platform is rectangular with a remote control receiver installed on it and a PLC controller installed inside the rectangular body; the platform is equipped with batteries and other components except those installed outside the platform; two gas cylinders filled with compressed air are installed under the platform, and landing gear is installed under the gas cylinders; an air hammer nozzle assembly with a window breaking function is installed on the platform plane, and is fixed in the middle position of the longitudinal plane of the platform, with the axis direction being horizontal; the fire extinguishing bin assembly is installed on the platform, and a dry powder fire extinguisher is placed in the silo on its upper part, and the middle plane of the silo in the length direction coincides with the axis of the air hammer nozzle assembly, and the left and right sliders are installed in its slide box, with the V-shaped fork slider moving in the longitudinal direction; the installation position of the fire extinguishing bin assembly in the width direction must satisfy the requirement that the front end plane of the dry powder fire extinguisher in the fire extinguishing position fits with the powder inlet plane in the air hammer nozzle assembly, and the dry powder fire extinguisher stops here, which means that the fire extinguishing start position of the fire extinguisher is The axis and the hole of the air hammer nozzle assembly are coaxial and connected here, which is a clearance sliding fit, so that after the fire extinguishing is started, the dry powder is pushed by the high-pressure aerosol smoke and ejected from the fire extinguisher through the air hammer nozzle channel at high speed; the striker is used to impact the piezoelectric ceramic at the tail of the dry powder fire extinguisher to achieve ignition, so as to start the dry powder fire extinguisher to extinguish the fire, and the axis of the striker is coaxial with the axis of the dry powder fire extinguisher at the fire extinguishing start position; and a thrust fan is installed on each side of the middle of the platform in the longitudinal direction to generate dynamic thrust in the lateral direction to balance the axial reaction force during the impact window breaking and the dry powder fire extinguisher dry powder spraying fire extinguishing, the two thrust fans are symmetrically installed on both sides of the striker, and their axes are parallel to the axis of the striker; the two blades rotate in opposite directions, turn in opposite directions and have the same speed, and the speed is controlled by the inverter to obtain different dynamic thrusts; the arrangement and installation of these components in the platform are based on the static equilibrium position, and the inverter controls the speed of the thrust fan to achieve dynamic balance.

[0045] The fire extinguishing silo assembly includes: a silo, a slide seat, two left and right V-shaped fork sliders, and two left and right three-position cylinders; the silo is used to store dry powder fire extinguishers; two V-shaped fork sliders are symmetrically assembled on the longitudinal midplane of the slide seat, and the V-shaped fork sliders are pushed forward and extended along the slide in the slide seat under the push of the three-position cylinder to change the distance and positioning between the two V-shaped fork sliders, and the extension and retraction are respectively connected to compressed air pipes, which are connected to two two-position five-way solenoid valves through air pipes, and the P interface of the solenoid valve is connected to the gas cylinder, and the solenoid valve is electrically connected to the PLC controller; the pneumatic position is three positioning, the horizontal distance between the two V-shaped fork sliders A is medium, and the dry powder fire extinguisher can fall freely from top to bottom Entering the fire extinguishing starting position, the horizontal distance between the two V-shaped fork sliders in position B is the smallest, and the dry powder fire extinguisher is clamped and positioned in the slide seat from the outside to the inside. The horizontal distance between the two V-shaped fork sliders in position C is the largest. This position makes the dry powder fire extinguisher in the fire extinguishing position freely fall downward from the V-shaped fork slider after spraying dry powder and fall into the platform warehouse. Then the horizontal distance of the V-shaped fork slider is medium, and another dry powder fire extinguisher freely falls from top to bottom into the fire extinguishing starting position; the spatial depth of the dry powder fire extinguisher loaded in the fire extinguishing silo assembly is stacked vertically in a single row, and the toothed forks of the V-shaped fork slider are staggered on the left and right, which can clamp the dry powder fire extinguisher in the starting position at a small distance without interfering with the left and right V-shaped fork sliders.

[0046] The striker is a pneumatic part, including a striker head and a cylinder, which provides power for starting the piezoelectric ceramics in the dry powder fire extinguisher. Its extension and retraction are respectively connected to compressed air pipes, which are connected to a two-position five-way solenoid valve through an air pipe. The P interface of the solenoid valve is connected to the gas cylinder, and the solenoid valve is electrically connected to the PLC controller; the end face of the striker head is installed close to the piezoelectric ceramic button of the dry powder fire extinguisher in the fire extinguishing position, and is coaxial with the axis of the fire extinguishing nozzle and the air hammer assembly; its power is driven by the cylinder to impact and generate high-voltage electricity to ignite and start the dry powder fire extinguisher.

[0047] The air hammer nozzle assembly is a pneumatic part, including: an air hammer nozzle, a piston, a cylinder body, and a cylinder back barrel; two cylinder seats are installed and fixed on the platform, and the cylinder back barrel is fixed in the hole thereof, the cylinder back barrel is assembled with the cylinder body, and the air hammer nozzle is assembled with the piston; the holes at both ends of the cylinder body are sealed by sealing rings, and the inner hole of the cylinder back barrel and the outer barrel of the air hammer nozzle are slidingly matched; the air hammer nozzle repeatedly changes the axis running direction under the drive of compressed air to perform frequent window breaking operations; the air hammer nozzle and the piston extension and retraction air chambers are respectively connected to compressed air pipes on the cylinder body, and the pipes are connected to the AB ports of the two-position five-way solenoid valve through the air pipe, the P interface of the solenoid valve is connected to the gas cylinder, and the solenoid valve is electrically connected to the PLC controller.

[0048] Pneumatic process: Two gas cylinders are connected in parallel, and the switches of the two gas cylinders are controlled by PLC; the AB air pipes are connected to the air holes of the air hammer nozzle assembly and the three positioning air holes of the two parallel sliders and the cylinder air hole of the striker through the corresponding solenoid valves.

[0049] The power source in the above scheme is a hydrogen battery or a lithium battery, which is connected to a transformer, a rectifier, and a transmitter through a frequency discriminator: one route is connected to a PLC controller; the PLC controller switch is respectively connected to the solenoid valves of the gas cylinder, the fire extinguishing nozzle and the air hammer assembly, the slider, and the striker, and the PLC controller is respectively connected to the DA module to connect the frequency converter, the sensor of the fire extinguishing position of the dry powder fire extinguisher, the remote control, and the frequency converter connected to the thrust fan; the other route is connected to the remote control receiver power line, and the remote control receiver is respectively connected to the PLC controller I port, and controls the opening and speed of the thrust fan by connecting the frequency converter; there is also a PLC communication connection with a CCD camera; the two electrode wires of the piezoelectric ceramic are connected to the two wires of the electric ignition head in the dry powder fire extinguisher.

[0050] The dry powder fire extinguisher is equipped with a powder spray nozzle at the front, dry powder in the middle, an aerosol-generating agent at the bottom, and an electric ignition head at the bottom. It uses piezoelectric ceramics to generate electric sparks to start the aerosol agent to explode and generate 10MP air pressure to push the dry powder out of the nozzle for fire extinguishing. The piezoelectric ceramics are installed at the tail of the cylinder, and the movement direction of the piezoelectric ceramic button is coaxial and in the same direction as the axis of the cylinder, and the button extends out of the cylinder.

[0051] The control process of the above scheme is as follows: 1. Control of flying to the fire point: according to the navigation, the flight path is manually controlled to quickly and directly fly to the fire location, and then the fire extinguishing position is accurately located by video; 2. Window breaking control, the piston in the air hammer nozzle assembly is used to reciprocate in the cylinder body to link the air hammer to break the window; 3. Fire extinguishing control: PLC controller automatic control, according to the instantaneous video image and ranging data of the CCD camera, the automatic control content of the PLC controller includes: the accurate horizontal distance between the fire extinguishing device and the fire extinguishing wall, breaking the window, whether to start the next dry powder fire extinguisher according to the fire extinguishing effect, the piezoelectric ceramic of the striker hitting the dry powder fire extinguisher to start the fire extinguishing, the start and stop of the gas cylinder, and the automatic adjustment of the variable frequency speed to timely start the recoil fan and the variable frequency speed regulation to balance the reaction force; 4. According to the ground monitoring data and images, the remote control is manually adjusted to prioritize the adjustment and control of the window breaking point position, window breaking time, striker impact ignition and fire extinguishing related actions through the PLC; 5. The start and stop of the thrust fan, the balance of speed wind force and horizontal recoil force are automatically controlled by the PLC separate algorithm.

[0052] The robustness of the above scheme lies in that, when the UAV is hovering in the lateral direction, the speed adjustment of the thrust fan can achieve the following: 1. Balance the reaction force of window breaking, so that the air hammer nozzle assembly can be pulled out after the window is broken; 2. Avoid the air hammer nozzle head being stuck by the broken hole, affecting flight safety; 3. Balance the reaction force of dry powder fire extinguishing; this is achieved by the data collected by the CCD camera, which is accurately controlled and adjusted in time by the PLC controller, so that the UAV can be stable without being disturbed by the power of the fire extinguishing step.

[0053] Stop firefighting at any time without using other dry powder fire extinguishers that are not involved, so as to save firefighting costs; two or more devices are used, which are suitable for larger fires. If one dry powder fire extinguisher has used up all the dry powder during firefighting, it can immediately leave the fire scene, descend to the ground, unload the dry powder fire extinguisher that has used up all the dry powder, load a new dry powder fire extinguisher, and then another device will take over to continue firefighting. Subsequent equipment can continue to take over the rotation of firefighting, and the equipment that has completed the replacement and filling of dry powder fire extinguishers can join the rotation of firefighting again.

[0054] However, after analyzing the above scheme, its window breaking function needs to be close to high-rise buildings. The rising hot air flow generated during a fire and the strong lateral wind force of the high-rise building itself can easily interfere with the flight of the drone.

[0055] Another prior art provides a window-breaking fire-fighting drone, which includes a drone body connected to four rotating shafts, with rotatable propellers fixed above the rotating shafts to provide lift during flight. The drone body includes a retractable window-breaking device, and the bottom of the drone body is provided with a connecting shaft, which is used to connect the fuselage with a dry powder containing device.

[0056] The dry powder containing device includes a dry powder storage bottle and a dry powder spraying port. The thrust generated by the motor can realize the spraying of the dry powder in the dry powder bottle, so as to be used for fire extinguishing. The retractable window breaking device includes a telescopic rod and a window breaking head. The thrust and suction generated by the motor can control the extension and retraction of the telescopic rod, so as to be better used for fire extinguishing. The above-mentioned window-breaking drone fire extinguishing device can realize rapid fire extinguishing on high floors. The device has a simple structure and is easy to operate. Compared with traditional fire extinguishing devices, it not only has more functions, but also has a faster fire extinguishing effect, which greatly reduces the losses of high-rise fires. However, the above-mentioned device carries a limited amount of dry powder. When launching dry powder, the dry powder is easily affected by the airflow of the drone blades and cannot be accurately applied to the fire source, resulting in poor fire extinguishing effect.

[0057] Through the analysis of the above technology, an improved solution of the present invention is proposed.

[0058] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0059] In order to make the above-mentioned objects, features and advantages of the present invention more obvious and easy to understand, the present invention is further described in detail below with reference to the accompanying drawings and specific embodiments.

[0060] Reference Figures 1 to 8, the present invention discloses a UAV high-altitude window-breaking dry powder fire-extinguishing device, comprising a UAV component 1, and a window-breaking fire-extinguishing component 5 is mounted on the bottom of the UAV component 1;

[0061] The window breaking fire extinguishing assembly 5 comprises:

[0062] The base 503 is fixedly connected to the bottom of the drone component 1;

[0063] Storage module, used to store solid beads and dry powder fire extinguishing balls for window breaking;

[0064] A launching module, used to launch solid beads or dry powder fire extinguishing balls for breaking windows;

[0065] The conveying module is used to convey the solid beads or dry powder fire extinguishing balls for window breaking from the storage module to the launching module.

[0066] During use, the drone component 1 is equipped with the window breaking fire extinguishing component 5. When a high-rise fire occurs, the drone component 1 carries the window breaking fire extinguishing component 5 to a specified height and approaches the outer window of the high-rise building. The solid beads for window breaking are first provided through the storage module, and the conveying module is used to convey the solid beads for window breaking and load them into the launching module. The launching module fires the solid beads for window breaking to shatter the outer window of the high-rise building. Subsequently, the storage module conveys the dry powder fire extinguishing ball to the launching module through the conveying module, and the launching module launches the dry powder fire extinguishing ball to the fire source. After the dry powder fire extinguishing ball is thrown into the fire source, it explodes under the action of high temperature, and the dry powder inside it covers the fire source, thereby realizing the drone's high-altitude window breaking fire extinguishing operation.

[0067] As an optional embodiment of the present application, the storage module includes two storage bins 102 opened on the drone fuselage 101 of the drone assembly 1, one of which is used to store solid beads for window breaking, and the other is used to store dry powder fire extinguishing balls. The storage bin 102 is connected to the feed end of the conveying module through a feed pipe 502;

[0068] The base 503 is fixedly connected to the bottom of the drone body 101 .

[0069] The drone assembly 1 includes a drone body 101, a battery is installed inside the drone body 101, and a control module 2 is mounted on the top of the drone body 101. The control module 2 is used to control the flight of the drone and data transmission. The control module 2 is also used to control the operation of the launch module and the conveying module.

[0070] A plurality of arms 3 are arranged around the drone body 101. The far ends of the arms 3 are equipped with motors for the drone to fly. The number of the arms 3 is set according to the required take-off weight.

[0071] The machine arm 3 and the drone body 101 can be folded or telescopic to achieve the ability of convenient transportation.

[0072] The detailed structure and settings of the machine arm 3 and the control module 2 can be obtained through the existing technology, so they are not described in detail.

[0073] The bottom of the drone body 101 is equipped with a camera 4 through a gimbal. The camera 4 can be a binocular camera. The camera 4 can be a camera with thermal sensing shooting and ordinary shooting functions, which is convenient for finding the fire source and determining whether the fire source is covered. The camera 4 is an existing technology, so it is not described in detail.

[0074] At least two storage bins 102 are provided inside the drone body 101, wherein one storage bin 102 is used to store solid beads for window breaking, and the other storage bin 102 is used to store dry powder fire extinguishing balls. The size of the solid beads for window breaking is comparable to that of the dry powder fire extinguishing balls.

[0075] As an optional implementation of the present application, two storage bins 102 are respectively located on both sides of the conveying module.

[0076] The size of the solid beads for breaking windows is comparable to that of the dry powder fire extinguishing balls, and the balance of the drone body 101 can be ensured by adjusting the number of solid beads for breaking windows and the number of dry powder fire extinguishing balls.

[0077] As an optional embodiment of the present application, the conveying module includes:

[0078] The electromagnetic stator ring 504 is fixedly connected to the base 503. The two ends of the electromagnetic stator ring 504 are respectively fixedly connected with end covers 505. The end covers 505 are provided with a feed port 506 for feeding and a connecting hole 508 for discharging. The feed port 506 is connected with the discharging end of the feed pipe 502.

[0079] The loading wheel 509 is rotatably arranged in the electromagnetic stator ring 504, and the electromagnetic stator ring 504 is transmission-connected to the loading wheel 509. A plurality of material holes 510 circumferentially evenly spaced are provided on the loading wheel 509. The loading wheel 509 rotates so that the two ends of one of the material holes 510 are respectively connected to the two feed ports 506, and the two ends of another material hole 510 are respectively connected to the two connecting holes 508.

[0080] During operation, the electromagnetic stator ring 504 drives the loading wheel 509 to rotate, so that the material hole 510 opened on the loading wheel 509 switches between the connecting hole 508 and the feed port 506, and the solid beads for breaking windows or the dry powder fire extinguishing balls roll from the feed pipe 502 into one of the material holes 510. The loading wheel 509 rotates to move the material hole 510 between the two connecting holes 508 and connect them, so that the solid beads for breaking windows or the dry powder fire extinguishing balls are filled into the launching module.

[0081] As an optional implementation of the present application, the inner wall of the electromagnetic stator ring 504 is embedded with a plurality of electromagnetic sheets arranged at equal intervals in the circumferential direction, and the polarities of two adjacent electromagnetic sheets are opposite;

[0082] The side wall of the loading wheel 509 is embedded with a plurality of permanent magnets arranged at equal intervals in the circumferential direction, and the polarities of two adjacent permanent magnets are opposite;

[0083] When the electromagnetic sheet is energized, a magnetic field is generated and magnetically connected to the permanent magnet sheet.

[0084] By energizing the electromagnetic sheet to generate a magnetic field, the magnetic fields generated by two adjacent electromagnetic sheets have opposite polarities. When the magnetic field is generated, the electromagnetic sheet is magnetically connected to the permanent magnet sheet, and the loading wheel 509 can be driven to rotate under the magnetic effect. By switching the polarity of the electromagnetic sheet, the loading wheel 509 can be driven to rotate and its rotation angle and speed can be controlled.

[0085] A rotating shaft 511 is axially connected to the middle of the loading wheel disc 509 , and an end of the rotating shaft 511 is rotatably connected to the end cover 505 through a rotating shaft connecting hole 507 opened in the middle of the end cover 505 .

[0086] As an optional implementation mode of the present application, the transmitting module includes:

[0087] The gun barrel 501 is fixedly connected to one of the end covers 505, and one end of the gun barrel 501 is connected to the communication hole 508 of the corresponding end cover 505;

[0088] The air compression unit is fixedly connected to the bottom of the drone body 101 , and the air outlet of the air compression unit is connected to the connecting hole 508 of another end cover 505 .

[0089] During use, the loading wheel 509 rotates to connect one of the material holes 510 between the barrel 501 and the high-pressure air pipe 512. At this time, the high-pressure air stored in the high-pressure air pipe 512 will push the solid beads for breaking windows or the dry powder fire extinguishing balls to be ejected. When the loading wheel 509 rotates, its side wall is blocked at the air outlet end of the high-pressure air pipe 512. This is the inflation stage, and the internal air pressure is increased through the air compression part. As the barrel 501 is connected to one of the material holes 510, the air in the high-pressure air pipe 512 is gradually released and pushes the corresponding solid beads for breaking windows or the dry powder fire extinguishing balls to move, until the loading wheel 509 rotates to the material hole 510 and the barrel 501 are coaxial. The solid beads for breaking windows or the dry powder fire extinguishing balls are no longer limited by the side wall of the end cover 505, and the solid beads for breaking windows or the dry powder fire extinguishing balls are ejected through the barrel 501 at high speed under the action of air pressure.

[0090] As an optional embodiment of the present application, the air compression unit includes:

[0091] One end of the high-pressure air pipe 512 is fixedly connected to the corresponding end cover 505 , and the high-pressure air pipe 512 is connected to the corresponding connecting hole 508 . The other end of the high-pressure air pipe 512 is connected to an air compressor, and the fixed end of the air compressor is fixedly connected to the bottom of the UAV fuselage 101 .

[0092] As an optional embodiment of the present application, the air compressor includes an air pump housing 513, the top of the air pump housing 513 is fixedly connected to the bottom of the drone fuselage 101, and the bottom of the air pump housing 513 is connected to the high-pressure air pipe 512;

[0093] A piston 518 slides vertically in the air pump housing 513. The piston 518 divides the inner wall of the air pump housing 513 into an active chamber located at the top and a gas compression chamber 523 located at the bottom. The gas compression chamber 523 is connected to the outside through a one-way valve 522. The one-way valve 522 is used to allow external air to enter the gas compression chamber 523 when the piston 518 rises. A second one-way valve 524 is provided at the air inlet end of the high-pressure air pipe 512. The second one-way valve 524 is used to prevent the air in the high-pressure air pipe 512 from flowing back to the gas compression chamber 523 when the gas compression chamber 523 is in the inhalation stage.

[0094] The piston 518 is drivingly connected to a driving part for driving it to slide up and down.

[0095] As an optional embodiment of the present application, the driving unit includes a crankshaft 520, which is rotatably disposed in the air pump housing 513, one end of the crankshaft 520 is axially connected to the output end of the motor 519, and the fixed end of the motor 519 is fixedly connected to the outer wall of the air pump housing 513;

[0096] One end of a crankshaft connecting rod 521 is hingedly connected to the middle of the crankshaft 520 , and the other end of the crankshaft connecting rod 521 is hingedly connected to the piston 518 .

[0097] The crankshaft 520 is driven to rotate by the motor 519, and the piston 518 slides up and down under the cooperation of the crankshaft 520 and the crankshaft connecting rod 521. When the piston 518 rises, the one-way valve 522 serves as the air inlet end to supply air to the gas compression chamber 523. When the piston 518 descends, the second one-way valve 524 serves as the air outlet end to supply air to the high-pressure air pipe 512. Since the gas flow direction is restricted by the one-way valve 522 and the second one-way valve 524, the air pressure in the high-pressure air pipe 512 will continue to increase with the reciprocating motion of the piston 518.

[0098] As an optional embodiment of the present application, a limiting slide 514 is provided at the discharge end of the feed pipe 502, and a slider 515 is slidably connected to the top of the limiting slide 514, and one end of a spring 516 is fixedly connected to the bottom of the slider 515, and the other end of the spring 516 is fixedly connected to an electromagnet 517, and the electromagnet 517 is fixedly connected to the bottom of the limiting slide 514. The electromagnet 517 is magnetically connected to the slider 515, and when the electromagnet 517 is started, it attracts the slider 515 to compress the spring 516, and the top of the slider 515 is located on the inner side of the top of the limiting slide 514. When the electromagnet 517 is closed, the spring 516 is released, so that the top of the slider 515 is located on the outer side of the top of the limiting slide 514, so as to prevent the solid beads or dry powder fire extinguishing balls for breaking windows from rolling.

[0099] By making the top of the slider 515 located outside the top of the limiting slide 514, the rolling of the solid beads for window breaking or the dry powder fire extinguishing ball can be hindered. When the solid beads for window breaking are needed to be launched, the electromagnet 517 in the feeding pipe 502 on the side for conveying the solid beads for window breaking is started, and the spring 516 is compressed when the slider 515 is attracted, while the electromagnet 517 in the feeding pipe 502 for conveying the dry powder fire extinguishing ball is in a closed state, thereby preventing the dry powder fire extinguishing ball from entering the material hole 510. Conversely, when the window breaking is completed, the state of the total electromagnet 517 of the two feeding pipes 502 is switched to stop conveying the solid beads for window breaking and start conveying the dry powder fire extinguishing ball.

[0100] In the description of the present invention, it should be understood that the terms "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside" and "outside" etc., indicating orientations or positional relationships, are based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation on the present invention.

[0101] The embodiments described above are only descriptions of the preferred modes of the present invention, and are not intended to limit the scope of the present invention. Without departing from the design spirit of the present invention, various modifications and improvements made to the technical solutions of the present invention by ordinary technicians in this field should all fall within the protection scope determined by the claims of the present invention.

Claims

1. A drone high-altitude window-breaking dry powder fire extinguishing device, comprising a drone component (1), characterized in that: The bottom of the drone component (1) is equipped with a window-breaking fire-extinguishing component (5); The window breaking fire extinguishing assembly (5) comprises: A base (503) is fixedly connected to the bottom of the drone component (1); Storage module, used to store solid beads and dry powder fire extinguishing balls for window breaking; A launching module, used to launch solid beads or dry powder fire extinguishing balls for breaking windows; The conveying module is used to convey the solid beads for window breaking or the dry powder fire extinguishing balls from the storage module to the launching module.

2. The UAV high-altitude window-breaking dry powder fire extinguishing equipment according to claim 1 is characterized by: The material storage module comprises two material storage bins (102) provided on the drone fuselage (101) of the drone assembly (1), wherein one of the material storage bins (102) is used to store solid beads for window breaking, and the other material storage bin (102) is used to store dry powder fire extinguishing balls, and the material storage bin (102) is connected to the feed end of the conveying module via a feed pipe (502); The base (503) is fixedly connected to the bottom of the drone body (101).

3. The UAV high-altitude window-breaking dry powder fire extinguishing equipment according to claim 2 is characterized by: The two material storage bins (102) are respectively located on two sides of the conveying module.

4. The UAV high-altitude window-breaking dry powder fire extinguishing equipment according to claim 2 is characterized in that: The conveying module comprises: An electromagnetic stator ring (504), wherein the electromagnetic stator ring (504) is fixedly connected to the base (503), and end covers (505) are respectively fixedly connected to both ends of the electromagnetic stator ring (504), and a feed port (506) for feeding and a connecting hole (508) for discharging are provided on the end cover (505), and the feed port (506) is connected to the discharging end of the feed pipe (502); A loading wheel disc (509) is rotatably disposed in the electromagnetic stator ring (504); the electromagnetic stator ring (504) is transmission-connected to the loading wheel disc (509); a plurality of material holes (510) are provided on the loading wheel disc (509) at equal intervals in the circumferential direction; the loading wheel disc (509) rotates so that the two ends of one of the material holes (510) are respectively connected to the two feed ports (506); and the two ends of another material hole (510) are respectively connected to the two connecting holes (508).

5. The UAV high-altitude window-breaking dry powder fire extinguishing equipment according to claim 4 is characterized by: The inner wall of the electromagnetic stator ring (504) is embedded with a plurality of electromagnetic sheets arranged at equal intervals in the circumferential direction, and the polarities of two adjacent electromagnetic sheets are opposite; A plurality of permanent magnets arranged at equal intervals in the circumferential direction are embedded in the side wall of the loading wheel disc (509), and the polarities of two adjacent permanent magnets are opposite; The electromagnetic sheet generates a magnetic field when energized and is magnetically connected to the permanent magnet sheet.

6. The UAV high-altitude window-breaking dry powder fire extinguishing equipment according to claim 4 is characterized in that: The transmitting module comprises: A gun barrel (501) is fixedly connected to one of the end covers (505), and one end of the gun barrel (501) is connected to the communication hole (508) of the corresponding end cover (505); The air compression unit is fixedly connected to the bottom of the drone fuselage (101), and the air outlet end of the air compression unit is connected to the connecting hole (508) of the other end cover (505).

7. The UAV high-altitude window-breaking dry powder fire extinguishing equipment according to claim 6 is characterized in that: The air compression unit comprises: One end of the high-pressure air pipe (512) is fixedly connected to the corresponding end cover (505), the high-pressure air pipe (512) is connected to the corresponding connecting hole (508), and the other end of the high-pressure air pipe (512) is connected to an air compressor, and the fixed end of the air compressor is fixedly connected to the bottom of the UAV fuselage (101).

8. The UAV high-altitude window-breaking dry powder fire extinguishing equipment according to claim 7 is characterized by: The air compressor comprises an air pump housing (513), the top of the air pump housing (513) is fixedly connected to the bottom of the drone fuselage (101), and the bottom of the air pump housing (513) is connected to the high-pressure air pipe (512); A piston (518) is vertically slidable in the air pump housing (513), and the piston (518) divides the inner wall of the air pump housing (513) into an active chamber located at the top and a gas compression chamber (523) located at the bottom. The gas compression chamber (523) is connected to the outside through a one-way valve (522), and the one-way valve (522) is used to allow external air to enter the gas compression chamber (523) when the piston (518) rises; a second one-way valve (524) is provided at the air inlet end of the high-pressure air pipe (512), and the second one-way valve (524) is used to prevent the air in the high-pressure air pipe (512) from flowing back to the gas compression chamber (523) when the gas compression chamber (523) is in the inhalation stage; The piston (518) is drivingly connected to a driving part for driving it to slide up and down.

9. The UAV high-altitude window-breaking dry powder fire extinguishing equipment according to claim 8 is characterized by: The driving part comprises a crankshaft (520), the crankshaft (520) is rotatably arranged in the air pump housing (513), one end of the crankshaft (520) is axially connected to the output end of the motor (519), and the fixed end of the motor (519) is fixedly connected to the outer wall of the air pump housing (513); One end of a crankshaft connecting rod (521) is hingedly connected to the middle of the crankshaft (520), and the other end of the crankshaft connecting rod (521) is hingedly connected to the piston (518).

10. The UAV high-altitude window-breaking dry powder fire extinguishing equipment according to claim 2 is characterized by: The discharge end of the feed pipe (502) is provided with a limit slideway (514), the top of the limit slideway (514) is slidably connected with a slider (515), the bottom of the slider (515) is fixedly connected with one end of a spring (516), the other end of the spring (516) is fixedly connected with an electromagnet (517), the electromagnet (517) is fixedly connected to the bottom of the limit slideway (514), the electromagnet (517) is magnetically connected to the slider (515), when the electromagnet (517) is started, it attracts the slider (515) to compress the spring (516), the top of the slider (515) is located inside the top of the limit slideway (514), when the electromagnet (517) is closed, the spring (516) is released, so that the top of the slider (515) is located outside the top of the limit slideway (514), so as to prevent the solid beads or dry powder fire extinguishing balls for breaking windows from rolling.

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