CN214216144U - High altitude conflagration rescue unmanned aerial vehicle - Google Patents
High altitude conflagration rescue unmanned aerial vehicle Download PDFInfo
- Publication number
- CN214216144U CN214216144U CN202120118494.9U CN202120118494U CN214216144U CN 214216144 U CN214216144 U CN 214216144U CN 202120118494 U CN202120118494 U CN 202120118494U CN 214216144 U CN214216144 U CN 214216144U
- Authority
- CN
- China
- Prior art keywords
- rescue
- aerial vehicle
- unmanned aerial
- fire
- carbon dioxide
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Abstract
The utility model provides a high altitude conflagration rescue unmanned aerial vehicle, this application is an unmanned aerial vehicle who possesses high altitude conflagration rescue and put out a fire, equipment essential parts includes the UWB radar, carbon dioxide extinguishing device, the bullet of putting out a fire, the rescue device, infrared camera, rotor and unmanned aerial vehicle system, provide power to equipment through the installation rotor, unmanned aerial vehicle system carries out long-range high altitude wireless control to it, the analysis is shot to the high altitude scene to installation infrared camera, whether stranded personnel have in the UWB radar of installation can monitor the conflagration scene, the carbon dioxide extinguishing device that equipment carried and the bullet of putting out a fire can put out a fire to the small area and handle, it is very important to build temporary passage when the rescue, the rescue device can carry the manned rescue in the air to stranded personnel, through reasonable mechanical design, solve the key difficult point of high altitude conflagration rescue, guarantee people's life and property safety.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially involves a high altitude conflagration rescue unmanned aerial vehicle.
Background
Today of the rapid development of technology, the unmanned aerial vehicle technology has gradually merged into our life, unmanned aerial vehicle shooting, unmanned aerial vehicle reconnaissance, unmanned aerial vehicle rescue and the like are closely related to our life, the unmanned aerial vehicle has the advantages of small volume, low manufacturing cost, convenience in use, low requirement on working environment, strong adaptability and the like, and countries in the world are all tightening to carry out unmanned technology development work, and the unmanned aerial vehicle is applied to a plurality of fields such as military, civil and business. At present, urban buildings are erected in high buildings in rapid urbanization, high-rise fire fighting is always the focus of attention, once a fire disaster occurs in the high buildings, the safety of lives and properties of people is seriously threatened, and in some places with incomplete fire fighting facilities, fire fighters need to burst life risks or even make great sacrifice to provide rescue and fire fighting when the fire disaster occurs. Therefore, the high-altitude fire rescue unmanned aerial vehicle is designed according to the difficult and painful points of the high-altitude fire, the fire can be extinguished on the high-altitude fire scene through the unmanned aerial vehicle, the trapped personnel in the high-altitude fire area can be detected, the high-altitude trapped personnel can be provided with air rescue service, the fire fighters can be prevented from directly conducting high-altitude fire extinguishing rescue, and the safety of lives and properties of people can be guaranteed.
SUMMERY OF THE UTILITY MODEL
In order to solve the existing problem, the utility model provides a high altitude conflagration rescue unmanned aerial vehicle, through install the UWB radar on unmanned aerial vehicle, carbon dioxide extinguishing device, the bullet of putting out a fire, the rescue device, infrared camera, rotor and unmanned aerial vehicle system, provide power to equipment through the installation rotor, unmanned aerial vehicle system carries out long-range high altitude wireless control to it, the analysis is shot to the high altitude scene to installation infrared camera, whether stranded personnel have in the UWB radar of installation can monitor the scene of fire, the carbon dioxide extinguishing device that equipment carried and the bullet of putting out a fire can put out a fire to the subregion and handle, it is very important to build interim passageway when the rescue, rescue device can carry the people and carry out aerial rescue to stranded personnel, through reasonable mechanical design, solve the key difficult point of high altitude conflagration rescue of putting out a fire, guarantee people's lives and property safety.
The utility model provides a high altitude fire rescue unmanned aerial vehicle, including carbon dioxide storage device, carbon dioxide injection apparatus, fire extinguishing bomb, handrail pull ring, backrest plate, pedal board, rotor system, power, controller and mounting panel, high altitude fire rescue unmanned aerial vehicle main part is installed on the mounting panel, corresponding rotor system support is installed to mounting panel upside position department, the support end-mounting corresponds rotor system, rotor system control circuit line is connected to the controller on the mounting panel through the support is internal, install carbon dioxide storage device on the mounting panel inside rotor system support mounting position, two sets of carbon dioxide injection apparatus are installed to the upper portion symmetry design of carbon dioxide storage device; a power supply is arranged at the rear part of a support plate on which the carbon dioxide storage device is arranged, and a controller is arranged at the front end of the power supply; two groups of fire extinguishing bombs are arranged on the lower side of the support plate, the fire extinguishing bombs are arranged in the launching device, rescue devices are arranged on the lower sides of the periphery of the support plate, the rescue devices are of a frame structure, the bottom of the frame of the rescue devices is closed, a pedal plate is arranged at the front end of the frame, a back plate is arranged on the rear side, protection plates are arranged on the left side and the right side, and a handrail pull ring hung down from the middle of the support plate is arranged in the middle of the rescue devices; the supporting rods on the periphery of the rescue device are fixed to the lower sides of the four corners of the support plate.
As a further improvement of the utility model, the device is provided with a carbon dioxide storage device and a carbon dioxide injection device, and the injection of the carbon dioxide is controlled by a controller to extinguish the fire in the combustion area; two groups of fire extinguishing bombs are arranged on the support plate, and fire extinguishing can be carried out on a fire area through the reflection fire extinguishing bombs; unmanned aerial vehicle possesses two kinds of modes of putting out a fire.
As the utility model discloses further improve, unmanned aerial vehicle installs the rescue device, and the rescue device is frame rack structure, and the preparation material adopts and hinders the hot material preparation, can provide aerial rescue to high altitude conflagration stranded personnel.
As the utility model discloses further improve, unmanned up-mounting UWB radar can be stranded to the regional detection of high altitude conflagration whether personnel.
As the utility model discloses further improve, unmanned aerial vehicle installs infrared camera, through to conflagration site data acquisition, for control manager provides the visual angle, provides the accurate position of putting out a fire for extinguishing device simultaneously.
As the utility model discloses further improve, six corresponding rotor system support of group of mounting panel upside position department installation consider that the capacity needs generally to use six rotor unmanned aerial vehicle.
The utility model provides a high altitude conflagration rescue unmanned aerial vehicle, the concrete design as follows:
1) the high-altitude fire rescue unmanned aerial vehicle is characterized in that a support plate is designed, rotor system supports are installed at four corners of the support plate, a rotor system is installed at the tail end of each rotor system support, and a rescue device is installed at the lower end of the support plate;
2) according to the high-altitude fire rescue unmanned aerial vehicle, a carbon dioxide storage device and a carbon dioxide injection device are arranged on the upper side of a support plate, a UWB radar is arranged at the upper end of the middle of the carbon dioxide injection device, and a power supply and a controller are arranged on the support plate at the rear end of the carbon dioxide storage device; two groups of fire extinguishing bombs are arranged at the lower end of the support plate, the fire extinguishing bombs are arranged in the launching device, and an infrared camera is arranged on the support plate in the middle of the fire extinguishing bombs to provide a visual angle for a site and carry out data acquisition and analysis on a site fire;
3) this application high altitude conflagration rescue unmanned aerial vehicle design's mounting plate lower extreme installation rescue device, rescue device design are frame construction, and the bottom is closed, both sides installation guard plate, and the rear side sets up back board, front side and sets up the step board, can let by the device that rescue personnel squat, and the rescue device adopts the heat-insulating material preparation, can effectively protect inside personnel.
Drawings
FIG. 1 is a schematic view of the overall structure of the device of the present invention;
FIG. 2 is a schematic view of a partial structure of the device of the present invention;
fig. 3 is a schematic view of a local structure of the device of the present invention.
Illustration of the drawings:
1. a UWB radar; 2. a carbon dioxide storage device; 3. a carbon dioxide injection device; 4. fire extinguishing bombs; 5. an armrest pull ring; 6. a backrest plate; 7. a pedal plate; 8. an infrared camera; 9. a rotor system; 10. a power source; 11. a controller; 12. a support plate.
Detailed Description
The invention will be described in further detail with reference to the following detailed description and accompanying drawings:
the utility model provides a high altitude conflagration rescue unmanned aerial vehicle, through install the UWB radar on unmanned aerial vehicle, carbon dioxide extinguishing device, the bullet of putting out a fire, rescue device, infrared camera, rotor and unmanned aerial vehicle system, provide power to equipment through the installation rotor, unmanned aerial vehicle system carries out long-range high altitude wireless control to it, the analysis is shot to the high altitude scene to installation infrared camera, whether the UWB radar of installation can monitor the scene of fire has the personnel of being stranded, the carbon dioxide extinguishing device that equipment carried and the bullet of putting out a fire can put out a fire to the subregion and handle, it is very important to build temporary passage when the rescue, rescue device can carry the people and carry out aerial rescue to the personnel of being stranded, through reasonable mechanical design, solve the key difficult point of high altitude conflagration fire-fighting rescue, guarantee people's life and property safety.
As an embodiment of the utility model, the utility model provides a high altitude fire rescue unmanned aerial vehicle, including UWB radar 1, carbon dioxide storage device 2, carbon dioxide injection apparatus 3, fire extinguishing bomb 4, handrail pull ring 5, backrest plate 6, pedal 7, infrared camera 8, rotor system 9, power 10, controller 11 and mounting panel 12, its characterized in that: the main body of the high-altitude fire rescue unmanned aerial vehicle is arranged on a support plate 12, six groups of rotor wing systems 9 are arranged at the upper side position of the support plate 12, six groups of rotor wing systems 9 are arranged at the tail end of the support, control circuit lines of the rotor wing systems 9 are connected to a controller 11 on the support plate through the inside of the support, and the rotor wing systems provide power for equipment; the carbon dioxide storage device 2 is arranged on a support plate 12 in the support mounting position of the rotor wing system 9, two groups of carbon dioxide injection devices 3 are symmetrically arranged on the upper part of the carbon dioxide storage device 2, and the carbon dioxide injection devices 3 realize the carbon dioxide injection fire extinguishing through a controller 11; the upper end of the middle part of the carbon dioxide injection device 3 is provided with a UWB radar 1 which can detect whether a person is trapped in a high-altitude fire area; a power supply 10 is arranged at the rear part of a support plate arranged on the carbon dioxide storage device 2 and provides power for the whole device, and a controller 11 is arranged at the front end of the power supply 10; two groups of fire extinguishing bombs 4 are arranged on the lower side of the support plate 12, the fire extinguishing bombs 4 are arranged in the launching device, the launching of the fire extinguishing bombs is controlled by the controller 11, and the unmanned aerial vehicle has two fire extinguishing modes; an infrared camera 8 is arranged on the lower side of a support plate in the middle of the two groups of fire extinguishing bombs 4, and through the data acquisition of a fire scene, a visual angle is provided for control and management personnel, and meanwhile, an accurate fire extinguishing position is provided for a fire extinguishing device; a rescue device is arranged on the lower side of the periphery of the support plate 12, the rescue device is of a frame structure, the bottom of a frame of the rescue device is closed, a pedal plate 7 is arranged at the front end of the frame, a back plate 6 is arranged on the rear side of the frame, protection plates are arranged on the left side and the right side of the frame, and a handrail pull ring 5 hung down from the middle of the support plate is arranged in the middle of the rescue device; the support rods on the periphery of the rescue device are fixed to the lower sides of the four corners of the support plate, the rescue device is made of heat-resistant materials, air rescue can be provided for people trapped in high-altitude fire, the key difficulty of high-altitude fire extinguishment rescue is solved through reasonable mechanical design, and life and property safety of people is guaranteed.
As a specific embodiment of the utility model, the utility model provides a show as in fig. 1-3 that is a high altitude fire rescue unmanned aerial vehicle overall structure schematic diagram, the main equipment of the high altitude fire rescue unmanned aerial vehicle is installed on a support plate 13, six groups of rotor systems 9 of the support are installed at the position of the upper side of the support plate 13, the support is spread all around, the support has the function of telescopic rotation, six groups of rotor systems 9 are installed at the end of the support, the control circuit line of the rotor systems 9 is connected to the controller on the support plate through the inside of the support 12, the rotor systems 9 provide power for the unmanned aerial vehicle equipment; the carbon dioxide storage devices 2 are arranged on a support plate 12 in the support mounting position of the rotor wing system 9, the number of the storage devices is two, two groups of carbon dioxide injection devices 3 are symmetrically arranged on the upper part of the carbon dioxide storage devices 2, and the carbon dioxide injection devices 3 realize carbon dioxide injection for extinguishing fire through the controller 12; the upper end of the middle part of the carbon dioxide injection device 3 is provided with a UWB radar 1 which can detect whether a person is trapped in a high-altitude fire area or not and position the trapped person; a power supply 10 is arranged at the rear part of a support plate arranged on the carbon dioxide storage device 2 and provides power for the whole device, a controller 12 is arranged at the front end of the power supply 10, and a wireless remote communication device is arranged on the controller 12 and can remotely control and process information; two groups of fire extinguishing bombs 4 are arranged on the lower side of the support plate 12, the fire extinguishing bombs 4 are arranged in the launching device, the launching of the fire extinguishing bombs is controlled by the controller 12, and the fire extinguishing bombs 4 efficiently extinguish fire in a small area; the carbon dioxide fire extinguishing device and the fire extinguishing bomb which are installed in the way enable the unmanned aerial vehicle to have two fire extinguishing modes, and can conduct fire extinguishing treatment on different fire-catching objects; an infrared camera 8 is arranged on the lower side of a support plate in the middle of the two groups of fire extinguishing bombs 4, and through the collection of fire scene data, a visual angle is provided for control and management personnel, the scene data is analyzed, and meanwhile, an accurate fire extinguishing position is provided for a fire extinguishing device, so that effective fire extinguishing is implemented; a rescue device is arranged on the lower side of the periphery of the support plate 12, the rescue device is of a frame type structure, the bottom of a frame of the rescue device is closed, a pedal plate 7 is arranged at the front end of the frame, a back plate 6 is arranged on the rear side of the frame, protection plates are arranged on the left side and the right side of the frame, and a handrail pull ring 5 hung down from the middle of the support plate is arranged in the middle of the rescue device; the supporting rods on the periphery of the rescue device are fixed to the lower sides of the four corners of the support plate, the rescue device is made of heat-resistant materials, internal personnel are effectively protected, the rotor system provides strong power, and high-altitude manned rescue can be carried out. The unmanned aerial vehicle solves the key difficult points of high-altitude fire extinguishment and rescue through reasonable mechanical design, and guarantees the life and property safety of people.
The six corresponding groups of rotor system brackets are arranged at the upper side of the bracket plate, and a six-rotor unmanned aerial vehicle is generally used in consideration of the transportation capacity requirement.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in any way, but also to cover any modifications or equivalent changes made in the technical spirit of the present invention, which fall within the scope of the present invention.
Claims (4)
1. The utility model provides a high altitude fire rescue unmanned aerial vehicle, includes carbon dioxide storage device (2), carbon dioxide injection apparatus (3), fire extinguishing bomb (4), handrail pull ring (5), back board (6), pedal board (7), rotor system (9), power (10), controller (11) and mounting panel (12), its characterized in that: the main body of the high-altitude fire rescue unmanned aerial vehicle is arranged on a support plate (12), a corresponding rotor system (9) support is arranged at the upper side position of the support plate (12), a corresponding rotor system (9) is arranged at the tail end of the support, a control circuit line of the rotor system (9) is connected to a controller (11) on the support plate (12) through the inside of the support, a carbon dioxide storage device (2) is arranged on the support plate (12) in the support mounting position of the rotor system (9), and two groups of carbon dioxide injection devices (3) are symmetrically arranged on the upper part of the carbon dioxide storage device (2); a power supply (10) is arranged at the rear part of a support plate arranged on the carbon dioxide storage device (2), and a controller (11) is arranged at the front end of the power supply; two groups of fire extinguishing bombs (4) are arranged on the lower side of the support plate (12), the fire extinguishing bombs (4) are arranged in a launching device, rescue devices are arranged on the lower sides of the periphery of the support plate (12), the rescue devices are of a frame type structure, the bottom of a frame of the rescue devices is closed, a pedal plate (7) is arranged at the front end of the frame, a back plate (6) is arranged on the rear side of the frame, protection plates are arranged on the left side and the right side of the frame, and a handrail pull ring (5) hung down from the middle of the support plate (12) is arranged in the middle of the rescue devices; the supporting rods on the periphery of the rescue device are fixed to the lower sides of the four corners of the support plate (12).
2. A high altitude fire rescue unmanned aerial vehicle of claim 1, characterized in that: the upper end of the middle part of the carbon dioxide injection device (3) is provided with a UWB radar (1).
3. A high altitude fire rescue unmanned aerial vehicle of claim 1, characterized in that: an infrared camera (8) is arranged on the lower side of the support plate (12) in the middle of the two groups of fire extinguishing bombs (4).
4. A high altitude fire rescue unmanned aerial vehicle of claim 1, characterized in that: and the upper side position of the bracket plate (12) is provided with six corresponding groups of brackets of the rotor system (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120118494.9U CN214216144U (en) | 2021-01-18 | 2021-01-18 | High altitude conflagration rescue unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120118494.9U CN214216144U (en) | 2021-01-18 | 2021-01-18 | High altitude conflagration rescue unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214216144U true CN214216144U (en) | 2021-09-17 |
Family
ID=77689917
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120118494.9U Active CN214216144U (en) | 2021-01-18 | 2021-01-18 | High altitude conflagration rescue unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214216144U (en) |
-
2021
- 2021-01-18 CN CN202120118494.9U patent/CN214216144U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| KR102149586B1 (en) | Unmanned aerial vehicle for fire fighting and rescue | |
| KR101566341B1 (en) | A multi- purpose fire fighting drone | |
| CN106828899B (en) | Rescue unmanned aerial vehicle and regulation and control fire control system thereof | |
| CN206345001U (en) | Rescue unmanned plane, rescue unmanned aerial vehicle group and its regulation and control fire-fighting system | |
| CN112093050B (en) | Modularized unmanned aerial vehicle fire engine | |
| CN206378951U (en) | A kind of fire safety defense monitoring system of the residential building based on internet | |
| CN108371767A (en) | A kind of police multi-functional flight rescue system of fire-fighting | |
| CN104200600A (en) | Fire analysis based firefighting monitoring system | |
| KR20080013088A (en) | The forest fire surveillance device and the device use forest fire surveillance system | |
| CN204979225U (en) | Ground -to -air fire control unmanned aerial vehicle | |
| CN211705663U (en) | Visual face guard of AR individual soldier and intelligent operation commander's face guard system for fire control | |
| CN108211183A (en) | A kind of miniature fire station of flow-type | |
| CN207403932U (en) | A kind of unmanned plane precisely drops a bomb fire extinguishing system | |
| CN111268128A (en) | Mooring type fire rescue unmanned aerial vehicle system | |
| CN109263883A (en) | A kind of manned unmanned plane of composite material | |
| CN206762078U (en) | A kind of fire-fighting robot | |
| CN107651180A (en) | A kind of unmanned plane precisely drops a bomb fire extinguishing system | |
| CN205563909U (en) | Conflagration monitoring device that can throw | |
| CN214216144U (en) | High altitude conflagration rescue unmanned aerial vehicle | |
| US20240009494A1 (en) | Automatic Firefighting Gun equipped with a multifunctional flame detector | |
| CN110420424B (en) | Fire rescue method and device for super high-rise building based on missile fire engine | |
| CN207186957U (en) | Aerial fire-fighting and rescue system | |
| CN112717303B (en) | Forest fire rescue extinguishing device | |
| Tian et al. | Research on Structure and Fire Control System of Fire Fighting UAV Based on Polymer Gel Fire Bomb | |
| CN108421189A (en) | A kind of skyscraper firefighting robot |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |