CN110816843A - Fire extinguishing system for high-rise building - Google Patents
Fire extinguishing system for high-rise building Download PDFInfo
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- CN110816843A CN110816843A CN201911095879.1A CN201911095879A CN110816843A CN 110816843 A CN110816843 A CN 110816843A CN 201911095879 A CN201911095879 A CN 201911095879A CN 110816843 A CN110816843 A CN 110816843A
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
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- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62B—DEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
- A62B3/00—Devices or single parts for facilitating escape from buildings or the like, e.g. protection shields, protection screens; Portable devices for preventing smoke penetrating into distinct parts of buildings
- A62B3/005—Rescue tools with forcing action
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- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C19/00—Hand fire-extinguishers in which the extinguishing substance is expelled by an explosion; Exploding containers thrown into the fire
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- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C3/00—Fire prevention, containment or extinguishing specially adapted for particular objects or places
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
- B64D1/06—Bomb releasing; Bombs doors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
- B64D47/04—Arrangements or adaptations of signal or lighting devices the lighting devices being primarily intended to illuminate the way ahead
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
Abstract
A fire extinguishing system for high buildings is provided with a laser ranging sighting device and an infrared camera in the front middle part of an undercarriage; the window breaker launching tube provided with the window breaker is fixed between the front cross beam and the rear cross beam of the undercarriage; the hanging rack is arranged below the front cross beam and the rear cross beam of the undercarriage; 2 or 4 fire extinguishing bomb launching cylinders are fixed on the hanging frame, and the front end of each fire extinguishing bomb launching cylinder is provided with an upper inclination angle of 0-30 degrees. Fire extinguishing bomb and/or rescue bomb are filled in each fire extinguishing bomb launching cylinder respectively. According to the invention, through implementing the glass breaking and the accurate delivery in two steps in sequence, the secondary damage caused by carrying of high-temperature tail flame by the rocket engine or entering of the high-temperature engine into a fire scene is overcome; the cost is reduced and the hit rate is improved by a close-distance delivery mode; the problem of the striking risk that fire extinguishing bomb high speed got into the room and brought is solved, the security and the reliability of fire extinguishing bomb have greatly been improved.
Description
Technical Field
The invention relates to the technical field of fire extinguishing of unmanned aerial vehicles, in particular to a fire extinguishing system for a high-rise building of an unmanned aerial vehicle.
Background
With the rapid increase of high-rise and extra-high-rise buildings, the fire extinguishing and fighting problem of the high-rise buildings is increasingly severe, more than 6000 buildings at 120 meters in China already exist, and more than half of super-high-rise buildings in the world exist in China.
At present, the maximum height that fire control aerial ladder can reach is 110 meters, to the super high-rise building that these fire control aerial ladders can not be considered, the current method of initiatively putting out a fire through the outside mainly has two kinds, firstly utilize the high-accuracy point but putting out a fire of expensive fire-fighting guided missile to put out a fire, this method carries out with ground group vehicle-mounted remote launching's mode, like application number 2012100484453.2, a fire control unit that is applicable to high-rise and super high-rise building fire suppression, secondly along with unmanned aerial vehicle aerial launch remote fire extinguishing rocket that has developed along with unmanned aerial vehicle's technological progress in recent years, like application number 201710604649.8, unmanned fire extinguishing system of high altitude mooring and application number 201710604649.8, unmanned fire extinguishing system of high altitude mooring. Both ground grouped vehicle-mounted launched fire-extinguishing missiles and unmanned aerial vehicle aerial remote launched fire-extinguishing rocket missiles have problems. Firstly, the cost is too high, the fire rescue cost is difficult to bear, and for small products such as fire extinguishing bombs for high buildings, whether laser guidance or infrared guidance, the cost of accurately measuring and controlling each product is only about 3 ten thousand yuan, which can be negligible for the missile for military use, but means an unacceptable luxury price for the product for fire fighting use; secondly, the problems of projectile body strength, flight speed, precision required by hitting, and the like required by glass breaking are integrated, and the manufacturing difficulty and cost of the product are increased; thirdly, the risk of damaging the building body due to inaccurate shooting exists, no matter the fire-extinguishing missile is launched on the ground vehicle at a distance of more than one hundred meters, or the fire-extinguishing rocket missile is launched in the air by the unmanned aerial vehicle at a distance of more than ten meters, the possibility of not entering a window exists, and once the high-speed flying missile body required by 19mm safety glass is deflected, the building wall surface or the building body is damaged; fourthly, in order to meet the requirements of two work tasks of fire extinguishing bomb flight and window breaking, the power source of the fire extinguishing bomb is a small rocket engine, and the fire extinguishing bomb also brings high-temperature tail flame or a high-temperature engine into a fire scene while flying power, so that the possibility of igniting combustible materials in the fire scene is increased; fifthly, the fire extinguishing bomb is in an explosion spraying type, when the fire extinguishing bomb works, the explosive in the fire extinguishing bomb enables the fire extinguishing agent to be thrown to a fire scene, meanwhile, the shell of the fire extinguishing bomb is smashed, fragments of the shell of the fire extinguishing bomb are thrown to the fire scene together, and people waiting for rescue in the fire scene are injured; sixthly, the condition of card bullet appears easily as the guide rail when fire extinguishing bomb launches in the T shape slide rail, makes the fire extinguishing bomb can not break away from unmanned aerial vehicle, draws to turn over unmanned aerial vehicle or explode to turn over unmanned aerial vehicle, causes the unmanned aerial vehicle accident of falling.
Disclosure of Invention
In order to overcome the defects of high cost, high danger and possibility of causing secondary damage of a high-rise fire extinguishing system in the prior art, the invention provides a high-rise fire extinguishing system.
The invention comprises a rotor unmanned aerial vehicle body, a rotor, a laser ranging sighting device, an infrared camera, a window breaker launching tube, a fire extinguishing bomb, a rescue bomb, a fire extinguishing bomb launching tube, an undercarriage and a hanging rack;
a laser ranging sighting device is fixed in the middle of a front cross beam of an undercarriage arranged on the lower surface of the body of the rotor wing unmanned aerial vehicle, and an infrared camera is fixed in the front of the lower end of the body of the rotor wing unmanned aerial vehicle; the window breaker launching tube is fixed between a front cross beam and a rear cross beam of the undercarriage, and a launching port of the window breaker launching tube is positioned at the front cross beam; the window breaker is positioned in the window breaker launching canister and at the rear part of the window breaker launching canister; the hanging rack is arranged below the front cross beam and the rear cross beam of the undercarriage; 2 or 4 fire extinguishing bomb launching cylinders are fixed on the hanging frame, and the cylinder openings of the fire extinguishing bomb launching cylinders are positioned at the front cross beam; the front end of each fire extinguishing bullet launching cylinder has an upper inclination angle of 0-30 degrees.
The fire extinguishing bomb and/or the rescue bomb are/is filled in each fire extinguishing bomb launching cylinder respectively.
The hanging rack comprises a hook, a front elastic rack and a rear elastic rack; the hook is divided into a long hook and a short hook, wherein the long hook is fixed on a rear cross beam of the undercarriage, and the short hook is fixed on a front cross beam of the undercarriage; the lower end of the long hook is fixedly connected with the rear elastic frame, and the lower end of the short hook is fixedly connected with the front elastic frame.
The front bullet rack and the rear bullet rack are both plate-shaped, and two or four fire extinguishing bullet launching tube mounting holes are respectively formed in each bullet rack; the diameter of each fire extinguishing bomb launching tube mounting hole is the same as the outer diameter of the fire extinguishing bomb launching tube, and the fire extinguishing bomb launching tube mounting holes are in close fit.
And three check blocks for positioning the fire extinguishing bomb launching cylinders are uniformly distributed on the inner surface of each launching cylinder mounting hole on the rear bomb frame.
When the cartridge frame is provided with two fire extinguishing bomb launching tube mounting holes, the two fire extinguishing bomb launching tube mounting holes are positioned on the cartridge frame in parallel; when the bullet rack is provided with four fire extinguishing bullet launching tube mounting holes, the four fire extinguishing bullet launching tube mounting holes are uniformly distributed into two groups which are arranged up and down.
The invention fundamentally overcomes the inherent defects of the prior art and products by implementing the problems of glass breaking and accurate delivery in two steps.
When the fire extinguishing bomb is used, a fireman puts a window breaker, a fire extinguishing bomb and a rescue bomb into corresponding launching tubes and connects an igniter plug to an unmanned aerial vehicle near a fire scene, the fireman remotely operates the unmanned aerial vehicle to convey the window breaker, the fire extinguishing bomb and the rescue bomb to a distance of 10-15 m from the outer wall of a fire scene building, observes the situation in the fire scene through an infrared camera, warns trapped persons possibly existing in the building through a loudspeaker and a searchlight, confirms that no person appears at the position of the window to be broken through the infrared camera, then breaks a glass wall curtain or window glass of the building in fire through the window breaker, then delivers the fire extinguishing bomb with micro thrust to the fire scene, sprays a fire extinguishing agent after 3 seconds, extinguishes the fire source in the fire scene, can also launch the rescue bomb to provide rescue equipment for the trapped persons according to needs on the scene, enables the trapped persons to save themselves or protects the trapped persons from toxic and harmful gases, the rescue time is prolonged. After the fire extinguishing bomb/rescue bomb carried by the unmanned aerial vehicle is used up, the unmanned aerial vehicle flies back to the ground, and ground fire fighters start a new round of fire extinguishing work after supplementing a window breaker, the fire extinguishing bomb or the rescue bomb according to the requirements.
The invention has the beneficial effects that:
the invention has the advantages that the glass breaking and the accurate delivery are implemented in two steps in sequence, so that the secondary damage caused by carrying of high-temperature tail flame by a rocket engine or entering of the high-temperature engine into a fire scene is overcome; the hitting precision is improved while the cost is reduced by a close-distance delivery mode; the problem of the striking risk that fire extinguishing bomb high speed got into the room and brought is solved, the security and the reliability of fire extinguishing bomb have greatly been improved.
2 because the fire extinguishing bomb need not possess the ability of breaking glass, consequently reducible engine fuel's use amount to greatly reduced fire extinguishing bomb head and shell's intensity uses the material of lightweight, reduces passive quality, improves the carrying capacity of fire extinguishing agent and unmanned aerial vehicle's the year bullet volume.
3 because the fire extinguishing bomb adopts the mode of delivering closely, the fire extinguishing bomb only needs very little thrust, delivers to the scene of a fire at a slower speed, therefore the size, the quality of engine will all reduce by a wide margin, and the quality of the fire extinguishing agent who corresponds with it will increase.
4, the invention arouses the attention of trapped personnel and fire fighters in a fire scene through sound (horn) and light (searchlight) double warning, so that the trapped personnel and the fire fighters can pay attention to avoid the trapped personnel and the fire fighters, and unnecessary injury is avoided; the loudspeaker and the searchlight can also be used for searching and rescuing trapped people and temporarily communicating with the trapped people under the condition of poor illumination.
5 the fire extinguishing bomb and the rescue bomb used by the invention can be matched and used at will according to the fire scene condition, so that the rescue is more targeted, and the rescue quality is improved.
Drawings
Fig. 1 is a schematic structural diagram of a four-launch-tube high-rise fire extinguishing system.
Fig. 2 is a schematic structural diagram of a double-emission-cylinder high-rise fire extinguishing system.
FIG. 3 is a schematic diagram of a relationship between positions of a launch canister and a window breaker.
Fig. 4 is a schematic structural diagram of the onboard part of the dual-shooting pot.
FIG. 5 is a schematic structural diagram of a vehicle-mounted part of four launch cans.
Fig. 6 is a schematic view of a tail hook.
Fig. 7 is a schematic view of a head hook.
Fig. 8 is a schematic view of a dual-tail cartridge carrier.
Fig. 9 is a schematic view of a dual head cartridge holder.
Fig. 10 is a schematic view of a four-issue tail cartridge holder.
Fig. 11 is a schematic view of a four-hair nose cartridge holder.
In the figure: 1. a rotor unmanned aerial vehicle fuselage; 2. a rotor; 3. a laser ranging sight; 4. an infrared camera; 5. a window breaker; 6. a window breaker launch canister; 7. fire extinguishing bombs; 8. a rescue bomb; 9. a fire extinguishing bomb launching tube; 10. a horn; 11. a searchlight; 12. a landing gear; 13. a hanger; 14. a safety mechanism.
Detailed Description
The embodiment is a high building fire extinguishing system, including rotor unmanned aerial vehicle fuselage 1, rotor 2, laser rangefinder sight 3, infrared camera 4, broken window ware 5, broken window ware launching tube 6, fire extinguishing bomb 7, rescue bullet 8, fire extinguishing bomb launching tube 9, loudspeaker 10, searchlight 11, undercarriage 12, stores pylon 13 and safety gear 14.
The lower surface of rotor unmanned aerial vehicle fuselage 1 is fixed with undercarriage 12. The laser ranging sighting device 3 is fixed in the middle of the nose beam of the undercarriage through an adapter and used for measuring the distance from the outer wall of a building and playing a role in auxiliary aiming. Infrared camera 4 fixes at rotor unmanned aerial vehicle fuselage lower extreme front portion for survey scene of a fire temperature distribution and provide the scene picture for ground. The window breaker launching tube 6 is fixed between a front cross beam and a rear cross beam of the landing gear 12 through a connecting piece, and a launching port of the window breaker launching tube is located at the front cross beam. The window breaker 5 is positioned in the window breaker launching canister and at the rear part of the window breaker launching canister. The hanger 13 is mounted below the front and rear cross members of the landing gear. Four fire extinguishing bomb launching cylinders 9 are fixed on the hanging frame, and the cylinder openings of the fire extinguishing bomb launching cylinders are positioned at the front cross beam. The fire extinguishing bomb 7 and/or the rescue bomb 8 are/is filled in each fire extinguishing bomb launching cylinder respectively.
A searchlight 11 and a horn 10 are fixed to the landing gear 12 for lighting the fire and transmitting information to the persons trapped in the fire and the fire fighters. The loudspeaker and the searchlight both adopt the existing products.
Rotor unmanned aerial vehicle adopts prior art.
The hanging frame 13 comprises four hooks, two elastic frames and four reinforcing ribs; the two bullet racks are divided into a front bullet rack and a rear bullet rack. The hooks are J-shaped hollow thin metal plates and are fixed on a front cross beam and a rear cross beam of the undercarriage 12, wherein two shorter hooks are positioned at the front cross beam of the undercarriage, one end of each of the two shorter hooks is hooked on the cross beam and fixed through a screw, and the other end of each of the two shorter hooks is fixedly connected with the front elastic frame; two longer J-shaped hollow thin metal plates are positioned at the rear cross beam of the undercarriage, one end of each thin metal plate is hooked on the cross beam and fixed through screws, and the other end of each thin metal plate is fixedly connected with the rear elastic frame. Due to the fact that the length of the hook is different, the launching tube has an upper inclination angle of 0-30 degrees. The front elastic frame and the rear elastic frame are supported through reinforcing ribs to ensure the rigidity of the front elastic frame and the rear elastic frame.
The bomb rack is plate-shaped, and two or four fire extinguishing bomb launching tube mounting holes are formed in each bomb rack. The diameter of each launching tube mounting hole on the front bullet rack is the same as the outer diameter of the fire extinguishing bullet launching tube 9, and the fire extinguishing bullet launching tubes and the fire extinguishing bullet launching tube are in close fit. The diameter of each launching tube mounting hole on the rear bullet rack is also the same as the outer diameter of the fire extinguishing bullet launching tube 9, and the fire extinguishing bullet launching tubes and the fire extinguishing bullet launching tube are in close fit; three radially protruding stop blocks are uniformly distributed on the inner surface of each launching tube mounting hole on the rear bullet rack; after the rear end of the fire extinguishing bomb launching tube is installed in the launching tube installing hole in the rear bomb rack, the position of the fire extinguishing bomb launching tube is limited through the matching between the stop block and the boss on the outer circumferential surface of the fire extinguishing bomb launching tube. Screw holes connected with the hooks are arranged on the edges of the elastic frames.
When the cartridge frame is provided with two fire extinguishing bomb launching tube mounting holes, the two fire extinguishing bomb launching tube mounting holes are positioned on the cartridge frame in parallel; when the bullet rack is provided with four fire extinguishing bullet launching tube mounting holes, the four fire extinguishing bullet launching tube mounting holes are uniformly distributed into two groups which are arranged up and down.
The fire extinguishing bomb launching tube is a hollow cylinder with a protrusion at the front part, and the protrusion at the front part is used for fixing the launching tube on the bomb rack.
The fire extinguishing bomb adopts a powder-spraying high-rise fire extinguishing bomb disclosed in the invention creation with the application number of 201911063627.0, and is a powder-pushing and throwing type fire extinguishing bomb using a low-temperature gas agent as a power source.
The fire extinguishing bomb comprises a powder spraying cover, a sealing piece, a launching tube, a powder tube, a guide tube, a dry powder extinguishing agent, a powder pushing plate, a hot aerosol, a connecting piece, a delay agent, a delay igniter, a combustion chamber shell, a low-temperature gas generating agent, a pressing piece, a rear cover and an igniter; wherein: the powder cylinder is positioned in the launching cylinder, and the dry powder extinguishing agent is arranged in the powder cylinder; the powder spraying cover is fixed at the upper end of the powder cylinder, and a sealing piece is arranged on the upper end face of the powder cylinder; the powder pushing plate is positioned at the lower end in the powder cylinder; the connecting piece is positioned in the launching tube and sleeved on the outer circumferential surface of the lower end of the powder tube; the outer circumferential surface of the connecting piece is in clearance fit with the inner circumferential surface of the launching barrel; the hot aerosol filling cavity is positioned between the lower end surface of the powder pushing plate and the inner end surface of the connecting piece; the center of the lower end face of the connecting piece is provided with a delay igniter sleeve which axially protrudes, and one end of the delay igniter is arranged in the delay igniter sleeve; one end of the linear delay medicament passes through the inner hole of the delay igniter, enters the guide tube and penetrates out of the air hole on the guide tube; the guide tube is positioned in the powder cylinder, the upper end of the guide tube is arranged in the center of the membrane supporting ring in the connecting piece, and the lower end of the guide tube is arranged in the center of the connecting piece; the powder cylinder, the launching cylinder and the guide pipe are coaxial; the upper end of the combustion chamber shell is fixedly connected with the connecting sleeve on the lower end surface of the connecting piece, and the lower end of the combustion chamber shell is fixedly connected with the rear cover; a pressing sheet is arranged on the lower end surface of the combustion chamber shell; the igniter penetrates through the through holes in the center of the pressing sheet and the center of the rear cover, one end of the igniter is positioned in the combustion chamber shell, and the other end of the igniter is positioned outside the combustion chamber shell; the low-temperature gas generating agent is arranged in the combustion chamber shell; and an air hole with the aperture of 2-5 mm is formed in the tube body at the lower end of the guide tube.
The rescue bomb adopts the prior art, uses low-temperature gas agent as a power source, and is a fire-fighting device capable of carrying rescue devices such as gas masks, ropes and the like to enter a fire scene.
The undercarriage is light metal pipe, is "A" font and arranges, and anterior and rear portion all have a crossbeam, for symmetrical structure for erect stores pylon, broken window ware launching tube and laser range finder sight, have the twice crossbeam to connect between anterior and the rear portion respectively, wherein the lower part crossbeam plays the effect that supports unmanned aerial vehicle, and the entablature plays the reinforcement effect.
The safety mechanism is an electronic lock fixed at the front end of the fire extinguishing bomb launching tube and is in linkage relation with an ignition system, the fire extinguishing bomb can be ignited and launched after the electronic lock is unlocked, and the safety mechanism is used for fixing the fire extinguishing bomb and providing double insurance for launching the fire extinguishing bomb.
The invention relates to a fire extinguishing system for a high building. The glass breaking and the accurate delivery are implemented in two steps, so that the inherent defects of the prior art and products are fundamentally overcome.
The invention achieves the aim through the following scheme that near a fire scene, a fireman puts a window breaker, a fire extinguishing bomb and a rescue bomb into corresponding launching cylinders, an igniter plug is connected to an unmanned aerial vehicle, the fireman remotely operates the unmanned aerial vehicle to convey the window breaker, the fire extinguishing bomb and the rescue bomb to a distance of 10-15 m away from the outer wall of a fire scene building, the condition in the fire scene is observed through an infrared camera, trapped persons possibly existing in the building are warned through a loudspeaker and a highlight flashlight, the glass wall curtain or window glass of the fire scene building is broken through the window breaker after the infrared camera confirms that no person appears at the position of a window to be broken, then the fire extinguishing bomb with micro-thrust is delivered to the fire scene, the fire extinguishing bomb starts to spray dry powder fire extinguishing agent after 3 seconds, a fire source of the fire scene is extinguished, and the rescue bomb can be launched to provide rescue equipment for the trapped persons as required on the scene, the trapped person can save himself or protect the trapped person from harmful gas and prolong the rescue time. After the fire extinguishing bomb/rescue bomb carried by the unmanned aerial vehicle is used up, the unmanned aerial vehicle flies back to the ground, and ground fire fighters start a new round of fire extinguishing work after supplementing a window breaker, the fire extinguishing bomb or the rescue bomb according to the requirements.
Claims (6)
1. A high-rise fire extinguishing system is characterized by comprising a rotor unmanned aerial vehicle body, a rotor, a laser ranging sighting device, an infrared camera, a window breaker launching tube, a fire extinguishing bomb, a rescue bomb, a fire extinguishing bomb launching tube, an undercarriage and a hanger;
a laser ranging sighting device is fixed in the middle of a front cross beam of an undercarriage arranged on the lower surface of the body of the rotor wing unmanned aerial vehicle, and an infrared camera is fixed in the front of the lower end of the body of the rotor wing unmanned aerial vehicle; the window breaker launching tube is fixed between a front cross beam and a rear cross beam of the undercarriage, and a launching port of the window breaker launching tube is positioned at the front cross beam; the window breaker is positioned in the window breaker launching canister and at the rear part of the window breaker launching canister; the hanging rack is arranged below the front cross beam and the rear cross beam of the undercarriage; 2 or 4 fire extinguishing bomb launching cylinders are fixed on the hanging frame, and the cylinder openings of the fire extinguishing bomb launching cylinders are positioned at the front cross beam; the front end of each fire extinguishing bullet launching cylinder has an upper inclination angle of 0-30 degrees.
2. A fire extinguishing system for high buildings according to claim 1, wherein the fire extinguishing bomb and/or the rescue bomb is loaded in each of the fire extinguishing bomb launching cylinders.
3. A fire suppression system for high buildings according to claim 1 wherein the hanger comprises a hook, a front cartridge rack and a rear cartridge rack; the hook is divided into a long hook and a short hook, wherein the long hook is fixed on a rear cross beam of the undercarriage, and the short hook is fixed on a front cross beam of the undercarriage; the lower end of the long hook is fixedly connected with the rear elastic frame, and the lower end of the short hook is fixedly connected with the front elastic frame.
4. A fire extinguishing system for high buildings according to claim 1, wherein the front cartridge carrier and the rear cartridge carrier are each plate-shaped, and two or four fire extinguishing bomb launcher mounting holes are formed in each cartridge carrier; the diameter of each fire extinguishing bomb launching tube mounting hole is the same as the outer diameter of the fire extinguishing bomb launching tube, and the fire extinguishing bomb launching tube mounting holes are in close fit.
5. A fire extinguishing system for high buildings according to claim 1, wherein three stoppers for positioning the fire extinguishing bomb-launching cylinders are uniformly distributed on the inner surface of each of the cartridge-mounting holes of the rear cartridge frame.
6. A fire extinguishing system for high buildings according to claim 4, wherein when the cartridge frame is opened with two fire extinguishing bomb launching tube mounting holes, the two fire extinguishing bomb launching tube mounting holes are located in parallel on the cartridge frame; when the bullet rack is provided with four fire extinguishing bullet launching tube mounting holes, the four fire extinguishing bullet launching tube mounting holes are uniformly distributed into two groups which are arranged up and down.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911095879.1A CN110816843A (en) | 2019-11-11 | 2019-11-11 | Fire extinguishing system for high-rise building |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911095879.1A CN110816843A (en) | 2019-11-11 | 2019-11-11 | Fire extinguishing system for high-rise building |
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| Publication Number | Publication Date |
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| CN110816843A true CN110816843A (en) | 2020-02-21 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201911095879.1A Pending CN110816843A (en) | 2019-11-11 | 2019-11-11 | Fire extinguishing system for high-rise building |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111450443A (en) * | 2020-03-17 | 2020-07-28 | 猫头鹰安防科技有限公司 | High-altitude fire extinguishing unmanned aerial vehicle |
| CN113908469A (en) * | 2021-10-29 | 2022-01-11 | 亿航智能设备（广州）有限公司 | High-rise fire extinguishing fire engine and fire extinguishing method |
| CN114295001A (en) * | 2021-12-30 | 2022-04-08 | 平裕（成都）科技有限公司 | Aiming method of glass breaking equipment |
| CN115970184A (en) * | 2022-12-07 | 2023-04-18 | 深圳天益建设工程有限公司 | Multifunctional building fire-fighting device with broken window structure |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN111450443A (en) * | 2020-03-17 | 2020-07-28 | 猫头鹰安防科技有限公司 | High-altitude fire extinguishing unmanned aerial vehicle |
| CN113908469A (en) * | 2021-10-29 | 2022-01-11 | 亿航智能设备（广州）有限公司 | High-rise fire extinguishing fire engine and fire extinguishing method |
| CN114295001A (en) * | 2021-12-30 | 2022-04-08 | 平裕（成都）科技有限公司 | Aiming method of glass breaking equipment |
| CN115970184A (en) * | 2022-12-07 | 2023-04-18 | 深圳天益建设工程有限公司 | Multifunctional building fire-fighting device with broken window structure |
| CN115970184B (en) * | 2022-12-07 | 2023-10-27 | 深圳天益建设工程有限公司 | Multifunctional building fire-fighting device with window breaking structure |
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