CN205525015U - Multi -functional firefighting rescue unmanned aerial vehicle - Google Patents
Multi -functional firefighting rescue unmanned aerial vehicle Download PDFInfo
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- CN205525015U CN205525015U CN201620067003.1U CN201620067003U CN205525015U CN 205525015 U CN205525015 U CN 205525015U CN 201620067003 U CN201620067003 U CN 201620067003U CN 205525015 U CN205525015 U CN 205525015U
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Abstract
The utility model discloses a multi -functional firefighting rescue unmanned aerial vehicle, including organism, rotor device and self -driving appearance system, the top of organism is equipped with fixed point lighting system, the inside airborne system that is equipped with of organism, and air -drop equipment is carried on through the carry ware in the organism below, the rotor device passes through connecting rod and organism fixed connection, and wherein the rotor device comprises spiral leaf, brushless motor and electronic governor, self -driving appearance system comprises sensing system, microprocessor, actuating system. The utility model discloses use commercial unmanned aerial vehicle as the carrier, have the investigation, put out a fire, rescue and four functions such as communication to can have characteristics such as flexible, quick response according to the complexity apolegamy functional module of task, improve the ageing of firefighting rescue greatly.
Description
Technical field
This utility model relates to unmanned plane air rescue technical field, specifically a kind of Multifunctional firefighting rescue unmanned plane.
Background technology
Along with the continuous lifting of the reaching its maturity of unmanned air vehicle technique, the expansion of air photo technique and cost performance, China people
Increasingly extensive by unmanned plane application, including videographic measurment, public safety, resource exploration, urban planning etc..Current fire-fighting portion
Team faces day by day complicated fire fighting and rescue and social helping situation, rescues all kinds of earthquake rescues, the rescue of isolated island ice face, waters, lofty mountains
Help, the situation such as large span or fire of high-rise building, the limitation of conventional on-site investigation and rescue means highlights the most day by day.Therefore
The most effectively implement fire-fighting early warning and on-the-spot detecting, and rapidly, accurately dispose the condition of a disaster and be particularly important.China's unmanned plane application
The ripe utilization of technology and system scheme so that unmanned plane just becoming fire brigade's spot dispatch commander, condition of a fire detecting and
It is the newly selected that auxiliary is rescued.
At present, various fire-fighting unmanned planes progressively emerge in large numbers, and mainly concentrate on fire-fighting Drones for surveillance and fire-fighting auxiliary is gone out
Fire unmanned plane, at present, fire-fighting unmanned plane on the market is mainly based on investigation, and wherein part fire-fighting unmanned plane has fire extinguishing of dropping a bomb
Function, can effectively assist fireman's fire fighting and rescue, but the function of existing fire-fighting unmanned plane is the most single, and cannot match merit
Energy module, it is difficult to fully meet the actual demand of fireman.
Utility model content
Utility model purpose: the purpose of this utility model is to provide one many for weak point of the prior art
Function fire-fighting and rescue unmanned plane, with commercial unmanned plane as carrier, has investigation, the four big functions such as put out a fire, rescue and communicate, and can
Complexity apolegamy functional module according to task.
Technical scheme: in order to realize object above, a kind of Multifunctional firefighting rescue unmanned plane described in the utility model, bag
Including body, rotor driver and autopilot system, the top of body is provided with fixed point illuminator, and internal body is provided with mobile system,
Aerial delivery provisions is carried by carry device below body；Described rotor driver is connected by connecting rod and body are fixing, wherein rotor dress
Putting and be made up of helical-blade, brushless electric machine and electron speed regulator, described autopilot system is by sensor-based system, microprocessor, drivetrain
System composition.
Preferably, described fixed point illuminator is Laser active illuminated imaging night vision system or LED visualization electronic guide browsing system.
Preferably, during described mobile system includes video camera, digital camera, airborne communication system, infrared thermography
One or more.
Preferably, described video camera is visible light camera or thermal camera.
Preferably, described airborne communication system includes wireless speech transport module, audio frequency power amplifier module, loudspeaker, electricity
Source module, wherein the outfan of wireless speech transport module is connected with the input of audio frequency power amplifier module, audio frequency power amplifier module
Outfan connect loudspeaker, power module outlet respectively with wireless speech transport module, audio frequency power amplifier module, loudspeaker
Power input connect.
Preferably, described sensor-based system includes combustible gas sensor and inertial navigation module, described inertial navigation module
Being become with groups of acceleration sensors by gyroscope, the quantity of described gyroscope and acceleration transducer is respectively 2-3.
Preferably, the external remote wireless transmission module of described inertial navigation module, described remote wireless transmission
Module forms data link communication system with the wireless module of earth station.Preferably, described fixed point illuminator, logging system,
The outfan of sensor-based system is all connected with the input of microprocessor, the outfan of microprocessor and remote wireless transmission module
Input connect, the input of the outfan of remote wireless transmission module and the wireless module of earth station sets up wireless signal
Connecting, the input of the outfan of wireless module monitor client long-range with ground is connected.
Preferably, described rotor driver is four rotors or six rotors.
Compared with prior art, the beneficial effects of the utility model are:
1 this utility model is multiple functional, can have maneuverability, quickly according to task character reasonable selection functional module
The features such as response, are greatly improved the ageing of fire-fighting and rescue.
2, this utility model can realize visualization, thermal imaging, combustible gas sensing, emergent mapping and illumination investigation function,
Can effectively promote the ability promptly and accurately investigating the condition of a disaster, it is provided that more objectively the condition of a disaster information, improve fire-fighting command personnel macroscopic view
Control the ability of overall the condition of a disaster.
3, this utility model has fire-extinguishing function concurrently, utilizes high-altitude to throw fire extinguisher bomb fire extinguishing, can partly replace fireman's
Fire-fighting work, is especially not easy to fire fighter at transformator, high-voltage line etc. and climbs close point of origin, effectively reduce casualties
And loss.
4, this utility model has the function delivering relief goods so that rescue means are abundanter, improves rescue efficiency.
5, this utility model has communication function, it is achieved unmanned plane is aerial and the voice communication of ground staff, it is simple to special
In the case of fire fighter and by the coordination and interaction between rescue personnel, it is simple to carrying out and advancing of rescue work, improve and rescue into
Power and efficiency.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
In figure: 1 body, 11 aerial delivery provisions, 12 fixed point illuminator, 13 mobile systems, 2 rotor driver, 21 spirals
Leaf, 22 brushless electric machines, 23 electron speed regulators, 3 autopilot systems, 31 sensor-based systems, 32 microprocessors, 33 drive systems, 4 nothings
Wire module, the 5 long-range monitor clients in ground.
Detailed description of the invention
Below in conjunction with the accompanying drawings and specific embodiment, being further elucidated with this utility model, these accompanying drawings are the signal of simplification
Figure, illustrates basic structure of the present utility model the most in a schematic way, the most only shows the composition relevant with this utility model.
Embodiment one
A kind of Multifunctional firefighting rescue unmanned plane as shown in Figure 1, including body 1, rotor driver 2 and autopilot system 3,
The top of body 1 is provided with fixed point illuminator 12, and body 1 is internal is provided with mobile system 13, is carried by carry device below body 1
Aerial delivery provisions 11；Described rotor driver 2 is fixed with body 1 by connecting rod and is connected, and wherein rotor driver 2 is by helical-blade 21, brushless
Motor 22 and electron speed regulator 23 form, and described autopilot system 3 is by sensor-based system 31, microprocessor 32, drive system 33 groups
Become.
Pinpointing illuminator 12 described in the present embodiment is Laser active illuminated imaging night vision system.By strong illumination at night
Disaster field is carried out fixed point illumination, uses DSP night vision image real-time processing technique, search for trapped personnel situation.Described airborne
System 13 is video camera, airborne communication system and infrared thermography, is surveyed and drawn disaster field in overhead by video camera,
Transmission, to microprocessor, is analyzed after calculating processes being formed on-the-spot real-time imaging figure and fire fighting truck force development figure.By red
Scene of fire intensity of a fire distribution situation checked by outer thermal imaging system, accurately measures fire point position.
Video camera described in the present embodiment is thermal camera.Gathering image by the way of hovering, thermal camera is adopted
The information transmission of collection is to microprocessor 32, and long-range monitor client is monitored and analyzes to ground to use wireless way for transmitting.
Described airborne communication system includes wireless speech transport module, audio frequency power amplifier module, loudspeaker, power module, the most wireless
The outfan of voice transfer module is connected with the input of audio frequency power amplifier module, and the outfan of audio frequency power amplifier module connects high pitch loudspeaker
, power module outlet is respectively with the power input of wireless speech transport module, audio frequency power amplifier module, loudspeaker even
Connect.It is achieved in the ground that unmanned plane arrived by unmanned plane by ground staff and carries out voice communication.
Described sensor-based system 31 includes combustible gas sensor and inertial navigation module, and described inertial navigation module is by gyro
Instrument becomes with groups of acceleration sensors, and the quantity of described gyroscope and acceleration transducer is respectively 2.Fuel gas is utilized to sense
Device measures on-the-spot combustable gas concentration, reduces fireman and enters not clear situation scene because of the unexpected casualties caused of burst.
The external remote wireless transmission module of described inertial navigation module, described remote wireless transmission module and ground
The wireless module composition data link communication system at station, face.Realize the data interaction between earth station and flight control system.
Described fixed point illuminator 12, mobile system 13, sensor-based system 31 outfan all with the input of microprocessor
Connecting, the outfan of microprocessor is connected with the input of remote wireless transmission module, remote wireless transmission module defeated
Going out end to set up wireless signal with the input of the wireless module of earth station and be connected, the outfan of wireless module 4 is remotely supervised with ground
The input of control client 5 connects.
Rotor driver 2 described in the present embodiment is four rotors.
Embodiment two
A kind of Multifunctional firefighting rescue unmanned plane as shown in Figure 1, including body 1, rotor driver 2 and autopilot system 3,
The top of body 1 is provided with fixed point illuminator 12, and body 1 is internal is provided with mobile system 13, is carried by carry device below body 1
Aerial delivery provisions 11；Described rotor driver 2 is fixed with body 1 by connecting rod and is connected, and wherein rotor driver 2 is by helical-blade 21, brushless
Motor 22 and electron speed regulator 23 form, and described autopilot system 3 is by sensor-based system 31, microprocessor 32, drive system 33 groups
Become.
Pinpoint illuminator 12 described in the present embodiment and visualize electronic guide browsing system for LED.Utilize LED illumination and communicate
Dual-use function, at night, disaster field carried out fixed point illumination by strong illumination, utilizes light radiation region to realize disaster
Fixed position transmits, and completes display and the report of corresponding setpoint information, learns trapped personnel situation.
Mobile system 13 described in the present embodiment is video camera, airborne communication system and infrared thermography, by shooting
Disaster field is surveyed and drawn by machine in overhead, and transmission, to microprocessor, is analyzed after calculating processes being formed on-the-spot real-time imaging
Figure and fire fighting truck force development figure.Check scene of fire intensity of a fire distribution situation by infrared thermography, accurately measure fire point position
Put.
Video camera described in the present embodiment is visible light camera.Image is gathered, it is seen that light images by the way of hovering
The information transmission that machine gathers is to microprocessor 32, and long-range monitor client is monitored and divides to ground to use wireless way for transmitting
Analysis.
Airborne communication system described in the present embodiment include wireless speech transport module, audio frequency power amplifier module, loudspeaker,
Power module, wherein the outfan of wireless speech transport module is connected with the input of audio frequency power amplifier module, audio frequency power amplifier module
Outfan connect loudspeaker, power module outlet respectively with wireless speech transport module, audio frequency power amplifier module, high pitch loudspeaker
Power input connects.It is achieved in the ground that unmanned plane arrived by unmanned plane by ground staff and carries out voice communication.
Sensor-based system 31 described in the present embodiment includes combustible gas sensor and inertial navigation module, described inertial navigation
Module is become with groups of acceleration sensors by gyroscope, and the quantity of described gyroscope and acceleration transducer is respectively 2.Utilization can
Combustion gas body sensor measures on-the-spot combustable gas concentration, reduces fireman and enters not clear situation scene because of the unexpected people caused of burst
Member's injures and deaths.
The external remote wireless transmission module of inertial navigation module described in the present embodiment, described remote-wireless passes
Defeated module forms data link communication system with the wireless module of earth station.Realize the data between earth station and flight control system
Alternately.
Described in the present embodiment pinpoint illuminator 12, mobile system 13, sensor-based system 31 outfan all with micro-process
The input of device connects, and the outfan of microprocessor is connected with the input of remote wireless transmission module, and remote-wireless passes
The outfan of defeated module is set up wireless signal with the input of the wireless module of earth station and is connected, the outfan of wireless module 4 with
The input of the long-range monitor client in ground 5 connects.
Rotor driver 2 described in the present embodiment is six rotors.
Embodiment three
A kind of Multifunctional firefighting rescue unmanned plane as shown in Figure 1, including body 1, rotor driver 2 and autopilot system 3,
The top of body 1 is provided with fixed point illuminator 12, and body 1 is internal is provided with mobile system 13, is carried by carry device below body 1
Aerial delivery provisions 11；Described rotor driver 2 is fixed with body 1 by connecting rod and is connected, and wherein rotor driver 2 is by helical-blade 21, brushless
Motor 22 and electron speed regulator 23 form, and described autopilot system 3 is by sensor-based system 31, microprocessor 32, drive system 33 groups
Become.
Pinpoint illuminator 12 described in the present embodiment and visualize electronic guide browsing system for LED.Utilize LED illumination and communicate
Dual-use function, at night, disaster field carried out fixed point illumination by strong illumination, utilizes light radiation region to realize disaster
Fixed position transmits, and completes display and the report of corresponding setpoint information, learns trapped personnel situation.
Described mobile system 13 is video camera, airborne communication system and infrared thermography, by video camera in overhead pair
Disaster field is surveyed and drawn, and transmission, to microprocessor, is analyzed after calculating processes being formed on-the-spot real-time imaging figure and fire fighting truck
Force development figure.Check scene of fire intensity of a fire distribution situation by infrared thermography, accurately measure fire point position.
Video camera described in the present embodiment is thermal camera.Gathering image by the way of hovering, thermal camera is adopted
The information transmission of collection is to microprocessor 32, and long-range monitor client is monitored and analyzes to ground to use wireless way for transmitting.
Airborne communication system described in the present embodiment include wireless speech transport module, audio frequency power amplifier module, loudspeaker,
Power module, wherein the outfan of wireless speech transport module is connected with the input of audio frequency power amplifier module, audio frequency power amplifier module
Outfan connect loudspeaker, power module outlet respectively with wireless speech transport module, audio frequency power amplifier module, high pitch loudspeaker
Power input connects.It is achieved in the ground that unmanned plane arrived by unmanned plane by ground staff and carries out voice communication.
Sensor-based system 31 described in the present embodiment includes combustible gas sensor and inertial navigation module, described inertial navigation
Module is become with groups of acceleration sensors by gyroscope, and the quantity of described gyroscope and acceleration transducer is respectively 3.Utilization can
Combustion gas body sensor measures on-the-spot combustable gas concentration, reduces fireman and enters not clear situation scene because of the unexpected people caused of burst
Member's injures and deaths.
The external remote wireless transmission module of inertial navigation module described in the present embodiment, described remote-wireless passes
Defeated module forms data link communication system with the wireless module of earth station.Realize the data between earth station and flight control system
Alternately.
Described in the present embodiment pinpoint illuminator 12, mobile system 13, sensor-based system 31 outfan all with micro-process
The input of device connects, and the outfan of microprocessor is connected with the input of remote wireless transmission module, and remote-wireless passes
The outfan of defeated module is set up wireless signal with the input of the wireless module of earth station and is connected, the outfan of wireless module 4 with
The input of the long-range monitor client in ground 5 connects.
Rotor driver 2 described in the present embodiment is six rotors.
Embodiment is merely to illustrate this utility model rather than limits scope of the present utility model, is reading this practicality
After novel, those skilled in the art all fall within right appended by the application and want the amendment of the various equivalent form of values of the present utility model
Seek limited range.
Claims (9)
1. a Multifunctional firefighting rescue unmanned plane, including body (1), rotor driver (2) and autopilot system (3), body (1)
Top be provided with fixed point illuminator (12), the internal mobile system (13) that is provided with of body (1), body (1) lower section is by carry device
Carry aerial delivery provisions (11)；Described rotor driver (2) is connected by connecting rod and body (1) are fixing, and wherein rotor driver (2) is by spiral shell
Vane (21), brushless electric machine (22) and electron speed regulator (23) composition, described autopilot system (3) is by sensor-based system (31), micro-
Processor (32), drive system (33) form.
A kind of Multifunctional firefighting rescue unmanned plane the most according to claim 1, it is characterised in that: described fixed point illuminator
(12) it is Laser active illuminated imaging night vision system or LED visualization electronic guide browsing system.
A kind of Multifunctional firefighting rescue unmanned plane the most according to claim 1, it is characterised in that: described mobile system (13)
One or more including in video camera, digital camera, airborne communication system, infrared thermography.
A kind of Multifunctional firefighting rescue unmanned plane the most according to claim 3, it is characterised in that: described video camera is visible
Light video camera or thermal camera.
A kind of Multifunctional firefighting rescue unmanned plane the most according to claim 1, it is characterised in that: described airborne communication system
Including wireless speech transport module, audio frequency power amplifier module, loudspeaker, power module, wherein wireless speech transport module is defeated
Going out end to be connected with the input of audio frequency power amplifier module, the outfan of audio frequency power amplifier module connects loudspeaker, and power module exports
End is connected with wireless speech transport module, audio frequency power amplifier module, the power input of loudspeaker respectively.
A kind of Multifunctional firefighting rescue unmanned plane the most according to claim 1, it is characterised in that: described sensor-based system (31)
Including combustible gas sensor and inertial navigation module, described inertial navigation module is become with groups of acceleration sensors by gyroscope,
The quantity of described gyroscope and acceleration transducer is respectively 2-3.
A kind of Multifunctional firefighting rescue unmanned plane the most according to claim 6, it is characterised in that: described inertial navigation module
An external remote wireless transmission module, described remote wireless transmission module forms Data-Link with the wireless module of earth station
Road communication system.
8. according to a kind of Multifunctional firefighting rescue unmanned plane described in claim 1 or 7, it is characterised in that: described fixed point illumination
System (12), mobile system (13), outfan all inputs with microprocessor (32) of sensor-based system (31) are connected, micro-process
The outfan of device (32) is connected with the input of remote wireless transmission module, the outfan of remote wireless transmission module and ground
The input of the wireless module (4) at station, face is set up wireless signal and is connected, and the outfan of wireless module (4) and ground remotely monitor visitor
The input of family end (5) connects.
A kind of Multifunctional firefighting rescue unmanned plane the most according to claim 1, it is characterised in that: described rotor driver (2)
It is four rotors or six rotors.
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106569506A (en) * | 2016-10-19 | 2017-04-19 | 广东容祺智能科技有限公司 | Automatic and accurate fire extinguishing system for unmanned aerial vehicle |
| CN107085436A (en) * | 2017-06-14 | 2017-08-22 | 亨利智创（北京）科技有限公司 | A kind of honeycomb rescue type unmanned plane cloud computing platform |
| CN107146363A (en) * | 2017-06-15 | 2017-09-08 | 江苏速度电子科技有限公司 | Forest fire prevention and control fire alarm and command system based on unmanned plane |
| CN107167766A (en) * | 2017-05-19 | 2017-09-15 | 江苏速度电子科技有限公司 | UAV system ULTRA-WIDEBAND RADAR fire-fighting alignment system |
| CN109125994A (en) * | 2018-09-20 | 2019-01-04 | 长沙中联消防机械有限公司 | Fire fighting truck intelligence control system and method and fire fighting truck |
| CN110302488A (en) * | 2019-06-12 | 2019-10-08 | 天府新区西南交通大学研究院 | Autonomous fire-fighting UAV system and fire-fighting method |
-
2016
- 2016-01-25 CN CN201620067003.1U patent/CN205525015U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106569506A (en) * | 2016-10-19 | 2017-04-19 | 广东容祺智能科技有限公司 | Automatic and accurate fire extinguishing system for unmanned aerial vehicle |
| CN107167766A (en) * | 2017-05-19 | 2017-09-15 | 江苏速度电子科技有限公司 | UAV system ULTRA-WIDEBAND RADAR fire-fighting alignment system |
| CN107085436A (en) * | 2017-06-14 | 2017-08-22 | 亨利智创（北京）科技有限公司 | A kind of honeycomb rescue type unmanned plane cloud computing platform |
| CN107146363A (en) * | 2017-06-15 | 2017-09-08 | 江苏速度电子科技有限公司 | Forest fire prevention and control fire alarm and command system based on unmanned plane |
| CN109125994A (en) * | 2018-09-20 | 2019-01-04 | 长沙中联消防机械有限公司 | Fire fighting truck intelligence control system and method and fire fighting truck |
| CN110302488A (en) * | 2019-06-12 | 2019-10-08 | 天府新区西南交通大学研究院 | Autonomous fire-fighting UAV system and fire-fighting method |
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Address after: No. 32 South Branch City D3 of Jiangsu province 210012 weeks in Yuhuatai District of Nanjing City Road 5 Patentee after: Nanjing Ze Ze Polytron Technologies Inc Address before: Yuhuatai District of Nanjing City Flower Avenue in Jiangsu province 210012 23 3 Building No. 5 room 506 Patentee before: Nanjing Zhengze Technology Co., Ltd. |
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