CN107662699A - Fire-fighting unmanned plane and fire-extinguishing - Google Patents
Fire-fighting unmanned plane and fire-extinguishing Download PDFInfo
- Publication number
- CN107662699A CN107662699A CN201610606238.8A CN201610606238A CN107662699A CN 107662699 A CN107662699 A CN 107662699A CN 201610606238 A CN201610606238 A CN 201610606238A CN 107662699 A CN107662699 A CN 107662699A
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- Prior art keywords
- fire
- unmanned plane
- extinguishing
- control device
- acoustic wave
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- 238000001931 thermography Methods 0.000 claims abstract description 36
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 17
- 230000005540 biological transmission Effects 0.000 claims description 10
- 230000005611 electricity Effects 0.000 claims description 5
- 238000004880 explosion Methods 0.000 claims description 3
- 230000005484 gravity Effects 0.000 claims description 3
- 238000005516 engineering process Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 238000012790 confirmation Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000003063 flame retardant Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C37/00—Control of fire-fighting equipment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Mechanical Engineering (AREA)
- Alarm Systems (AREA)
Abstract
A kind of fire-fighting unmanned plane and fire-extinguishing, including unmanned plane body, thermal imaging system and acoustic wave device；The thermal imaging system and the acoustic wave device are separately positioned on the unmanned plane body bottom portion；Control device and the first wireless module are provided with the unmanned plane body；The thermal imaging system is connected with the control device, for being shot to target area to obtain the thermal image information of target area；The control device is used to the thermal image information being sent to monitor terminal by first wireless module；The control device is additionally operable to the fire extinguishing control signal for receiving the monitor terminal by first wireless module and sending；The acoustic wave device is connected with the control device；The acoustic wave device is used under the control of the fire extinguishing control signal work, to produce sound wave to eliminate fire.Above-mentioned fire-fighting can control fire dangerous situation in time with unmanned plane and fire-extinguishing and operating efficiency is higher.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to a kind of fire-fighting unmanned plane and fire-extinguishing.
Background technology
In recent years, fire incident takes place frequently.Because management and control is not in place, manpower can not be reached when fire occurs, and cause fire-fighting work
It is difficult to.In addition, with the development of modern city construction industry, the height of skyscraper constantly refreshes, to fire-fighting and rescue
Also many troubles are brought.Especially when disposal fire of high-rise building, inflammable and explosive grade fire fighting problem, because fireman can not
It is close or cannot be introduced into disaster accident scene, cause in time fire dangerous situation can not be controlled to be stopped loss.
The content of the invention
Based on this, it is necessary to which providing a kind of can control fire dangerous situation in time and operating efficiency higher fire-fighting fire extinguishing nothing
It is man-machine.
A kind of fire-fighting unmanned plane and fire-extinguishing, including unmanned plane body, thermal imaging system and acoustic wave device；The thermal imaging system
The unmanned plane body bottom portion is separately positioned on the acoustic wave device；Control device and are provided with the unmanned plane body
One wireless module；The thermal imaging system is connected with the control device, for being shot target area to obtain target area
The thermal image information in domain；The control device is used to the thermal image information being sent to monitoring by first wireless module
Terminal；The control device is additionally operable to the fire extinguishing control letter for receiving the monitor terminal by first wireless module and sending
Number；The acoustic wave device is connected with the control device；The acoustic wave device is used under the control of the fire extinguishing control signal
Work, to produce sound wave to eliminate fire.
In one of the embodiments, the thermal imaging system is anti-explosion thermal-imaging instrument.
In one of the embodiments, the acoustic wave device is used to produce the sound wave that frequency is 30~60 hertz.
In one of the embodiments, the acoustic wave device is to be detachably connected with the unmanned plane body.
In one of the embodiments, the thermal imaging system and the acoustic wave device are symmetricly set on the unmanned plane body
Center of gravity both sides.
In one of the embodiments, it is additionally provided with wireless image transmission module on the unmanned plane body；The wireless image transmission
Module is connected with the thermal imaging system, and for being connected with the monitor terminal；The wireless image transmission module is used for the heat
Image information is exported to the monitor terminal, and receives the shooting control signal of the monitor terminal output.
In one of the embodiments, the unmanned plane body includes supply unit；The supply unit includes sequentially connecting
Engine, generator, battery and the electric power source distribution device connect；The engine is used to drive the generator operation, to produce electricity
It can be charged to the battery；The battery is set by the electric power source distribution device with the fire-fighting with each electricity consumption of unmanned plane and fire-extinguishing again
It is standby to connect and power.
In one of the embodiments, the unmanned plane body includes aircraft base, undercarriage, support shaft, propeller
Pedestal and propeller；The control device is arranged in the aircraft base；The undercarriage and the support shaft are solid
It is scheduled on the aircraft base；The support shaft is multiple, and is symmetrically distributed in the aircraft base surrounding；The spiral
Oar pedestal is fixed on one end away from the aircraft base in the support shaft；The propeller is fixed on the propeller base
On seat.
In one of the embodiments, motor and electron speed regulator are included in the propeller pedestal；The control dress
Put and be connected with the electron speed regulator；The electron speed regulator and the motor connection；The electron speed regulator is used for motor
Rotating speed be controlled, so as to control the rotating speed of propeller.
In one of the embodiments, range sensor is also included in the propeller pedestal；The range sensor is used
In the distance for perceiving the propeller pedestal and exterior object and export to the control device；The control device is additionally operable to
When the distance is less than warning value, the flying height and flying speed of unmanned plane are adjusted.
Above-mentioned fire-fighting unmanned plane and fire-extinguishing, thermal imaging system can be shot to target area to obtain the thermal map of target area
As being exported after information by control module by the first wireless module to monitor terminal, made for staff according to the thermal image information
Go out decision-making, to send fire extinguishing control signal.Control device can also receive fire extinguishing control signal by the first wireless module, from
And control acoustic wave device to work, to produce sound wave to eliminate fire, and when control fire dangerous situation.Produced simultaneously by acoustic wave device
Sound wave is given birth to eliminate fire, the materials such as addition extinguishing chemical are come and gone without unmanned plane, so as to greatly save the part-time,
Fire-fighting efficiency is improved, further ensures that fire dangerous situation can be controlled in time.
Brief description of the drawings
Fig. 1 is the front view of the fire-fighting unmanned plane and fire-extinguishing in an embodiment；
Fig. 2 is the side view of the fire-fighting unmanned plane and fire-extinguishing in Fig. 1；
Fig. 3 is the top view of the fire-fighting unmanned plane and fire-extinguishing in Fig. 1；
Fig. 4 is the upward view of the fire-fighting unmanned plane and fire-extinguishing in Fig. 1；
Fig. 5 is the structured flowchart of the intrinsic supply unit of unmanned plane in Fig. 1.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, it is right below in conjunction with drawings and Examples
The present invention is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and
It is not used in the restriction present invention.
Fig. 1 is the front view of the fire-fighting unmanned plane and fire-extinguishing in an embodiment, and Fig. 2 is Fig. 1 side view, and Fig. 3 is Fig. 1's
Top view, Fig. 4 are Fig. 1 upward view.The fire-fighting in the present embodiment is made in detail of unmanned plane and fire-extinguishing with reference to Fig. 1~Fig. 4
Explanation.Because unmanned plane has the characteristics of small volume, therefore the fire-fighting unmanned plane and fire-extinguishing can be used for open air, can also enter
The region for waiting fire fighter to be difficult to arrive in skyscraper carries out fire-fighting work.The fire-fighting includes unmanned plane with unmanned plane and fire-extinguishing
Body 100, thermal imaging system 200 and acoustic wave device 300.Wherein, thermal imaging system 200 and acoustic wave device 300 are arranged at nobody
The bottom of machine body 100.
Unmanned plane body 100 is used for the common function for realizing unmanned plane, is such as flown according to predetermined paths.Unmanned plane
Body 100 includes aircraft base 110, undercarriage 120, support shaft 130, propeller pedestal 140 and propeller 150.Wherein,
Undercarriage 120 and support shaft 130 are each attached on aircraft base 110.Be provided with aircraft base 110 supply unit and
Control device.Supply unit is used for for each power supply for electrical equipment in unmanned plane body 100.Control device is then used for unmanned plane
The flight of body 100 is controlled, and is adjusted with the flying speed to unmanned plane 100 and height etc..Specific adjustment technology
Belong to technology commonly used in the art, do not repeat herein.In the present embodiment, supply unit is carried out using the indirect power supply mode of generator
Power supply.Specifically, the structured flowchart of supply unit is as shown in Figure 5.Supply unit includes engine 510, the generating being sequentially connected with
Machine 520, battery 530 and electric power source distribution device 540.Electric power source distribution device 540 is used to be connected with each electrical equipment.Pass through engine
510 drive generator 520, and generator 520 charges to battery 530, and battery 530 reconnects electric power source distribution device 540 and set to each electricity consumption
Standby such as control device is powered.This power supply mode can give unmanned plane for traditional pure battery powered mode
More stable endurance is provided.In the present embodiment, the first wireless module is additionally provided with aircraft base 110.First
Wireless module can be integrated in control device.First wireless module is used to be connected with monitor terminal, to receive monitor terminal hair
The control signal sent.Meanwhile the data message that can also be monitored by the first wireless module of control device and from
Operational factor of body etc. is sent to monitor terminal, is easy to the user of monitor terminal to understand its working condition.
Support shaft 130 is multiple, and is symmetrically distributed on aircraft base 110, so that it is guaranteed that unmanned plane body 100 is flying
Stationarity during row.In the present embodiment, support shaft 130 is four.Four support shafts 130 are symmetrically distributed in winged at equal intervals
The surrounding of row device base 110.Propeller pedestal 140 is fixed on one end away from aircraft base 110 in support shaft 130.Spiral
Oar 150 is fixed on propeller pedestal 140.In the present embodiment, electron speed regulator and electricity are provided with propeller pedestal 140
Machine.Electron speed regulator is used to be adjusted the rotating speed of motor, and then controls the rotating speed of the rotor of propeller 150.Specifically, it is electric
Sub- speed regulator is connected by wire with the control device in aircraft base 110, so as under control of the control means to motor
Rotating speed is controlled, and final realize is adjusted to the state of flight of unmanned plane.In the present embodiment, in propeller pedestal 140
It is additionally provided with range sensor.Range sensor is used to perceive the distance of propeller pedestal 140 and exterior object and passes through transmission
Line is exported to control device.Control device can be monitored in real time to the distance, i.e., by it compared with warning value, when the distance
During less than warning value, the flying height and flying speed of unmanned plane are adjusted, to enable unmanned plane body 100 to keep away
Open barrier, it is ensured that the flight safety of unmanned plane body 100.
Thermal imaging system 200 is used to shoot target area, to obtain the thermal image information of target area.Thermal imaging system
200 shooting area scope can be carried out according to unmanned plane apart from the height of shooting area and the shooting angle scope of unmanned plane
It is determined that.In the present embodiment, thermal imaging system 200 is anti-explosion thermal-imaging instrument, so as to suitable for hot environment.Thermal imaging system
200 are connected by data wire with control device, so as to which obtained thermal imaging information is sent into control device.The control device meeting
The thermal imaging information that graphic images obtain is sent to the monitor terminal of ground surface end by the first wireless module.Staff can
Judgement decision-making is carried out with the thermal imaging information received according to monitor terminal, so as to which the region has fire dangerous situation needs in confirmation
Fire extinguishing control signal is sent when being put out a fire.Control device receives the fire extinguishing control signal by the first wireless module, and by its
Export to the acoustic wave device 300 being attached thereto.In the present embodiment, wireless image transmission module is additionally provided with unmanned plane body 100.
Wireless image transmission module is connected with thermal imaging system 200, and for being connected with the monitor terminal of ground surface end, thermal image information is sent
To monitor terminal, while the shooting control signal that monitor terminal is sent can also be received, with the shooting angle to thermal imaging system 200
Degree and scope are adjusted.Wireless image transmission module can also be directly integrated on thermal imaging system 200.
Acoustic wave device 300 is used to work under the control of the fire extinguishing control signal, produces sound wave to eliminate fire.In this reality
Apply in example, acoustic wave device 300 can produce sound wave of the frequency between 30~60Hz.The sound wave of the frequency range can produce most suitable
The energy of fire extinguishing, combustible and oxygen can be separated, so as to realize that anoxic is fire-retardant, to eliminate the little fire of some intensity of a fire
Feelings.Sound wave is produced by acoustic wave device to eliminate fire, the materials such as addition extinguishing chemical are come and gone without unmanned plane, so as to very big
The saving part-time, improve fire-fighting work efficiency.Simultaneously as the sound wave frequency range low frequency, will not be produced to surrounding body
Acoustic jamming.In the present embodiment, acoustic wave device 300 and thermal imaging system 200 are symmetricly set on the two of the center of gravity of unmanned plane body 100
Side, to improve the stability of unmanned plane during flying.Also, thermal imaging system 200 and acoustic wave device 300 are along perpendicular to undercarriage 120
Length direction is set gradually.It is to be detachably connected between thermal imaging system 200 and acoustic wave device 300 and unmanned plane body 100, from
And maintenance replacing conveniently is carried out to thermal imaging system 200 and acoustic wave device 300.
Above-mentioned fire-fighting unmanned plane and fire-extinguishing, thermal imaging system 200 can be shot to obtain target area to target area
Exported to monitor terminal by the first wireless module by control module after thermal image information, believed for staff according to the thermal image
Breath makes decisions, to send fire extinguishing control signal.Control device can also receive fire extinguishing control letter by the first wireless module
Number, so as to control acoustic wave device 300 to work, to produce sound wave to eliminate fire, and when control fire dangerous situation.Pass through sound simultaneously
Wave device 300 produces sound wave to eliminate fire, the materials such as addition extinguishing chemical is come and gone without unmanned plane, so as to greatly save
The part-time, fire-fighting work efficiency is improved, further ensures that fire dangerous situation can be controlled in time.Above-mentioned fire-fighting fire extinguishing
Unmanned plane is highly suitable for fire threat caused by the outdoor campfire that nobody looks after and opened in high-rise for fireman
The situations such as the fire extinguishing passage warded off.
Each technical characteristic of embodiment described above can be combined arbitrarily, to make description succinct, not to above-mentioned reality
Apply all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, the scope that this specification is recorded all is considered to be.
Embodiment described above only expresses the several embodiments of the present invention, and its description is more specific and detailed, but simultaneously
Can not therefore it be construed as limiting the scope of the patent.It should be pointed out that come for one of ordinary skill in the art
Say, without departing from the inventive concept of the premise, various modifications and improvements can be made, these belong to the protection of the present invention
Scope.Therefore, the protection domain of patent of the present invention should be determined by the appended claims.
Claims (10)
1. a kind of fire-fighting unmanned plane and fire-extinguishing, it is characterised in that including unmanned plane body, thermal imaging system and acoustic wave device；Institute
State thermal imaging system and the acoustic wave device is separately positioned on the unmanned plane body bottom portion；Control is provided with the unmanned plane body
Device processed and the first wireless module；The thermal imaging system is connected with the control device, for target area is shot with
Obtain the thermal image information of target area；The control device is used to the thermal image information passing through first wireless module
It is sent to monitor terminal；The control device is additionally operable to receive what the monitor terminal was sent by first wireless module
Fire extinguishing control signal；The acoustic wave device is connected with the control device；The acoustic wave device is used in the fire extinguishing control letter
Number control under work, to produce sound wave to eliminate fire.
2. fire-fighting unmanned plane and fire-extinguishing according to claim 1, it is characterised in that the thermal imaging system is anti-explosion thermal-imaging
Instrument.
3. fire-fighting unmanned plane and fire-extinguishing according to claim 1, it is characterised in that the acoustic wave device is used to produce frequency
For 30~60 hertz of sound wave.
4. fire-fighting unmanned plane and fire-extinguishing according to claim 1, it is characterised in that the acoustic wave device and the unmanned plane
Body is to be detachably connected.
5. fire-fighting unmanned plane and fire-extinguishing according to claim 1, it is characterised in that the thermal imaging system and the sound wave are set
The both sides of the standby center of gravity for being symmetricly set on the unmanned plane body.
6. fire-fighting unmanned plane and fire-extinguishing according to claim 1, it is characterised in that be additionally provided with the unmanned plane body
Wireless image transmission module；The wireless image transmission module is connected with the thermal imaging system, and for being connected with the monitor terminal；It is described
Wireless image transmission module is used to export the thermal image information to the monitor terminal, and receives taking the photograph for the monitor terminal output
As control signal.
7. fire-fighting unmanned plane and fire-extinguishing according to claim 1, it is characterised in that the unmanned plane body fills including power supply
Put；The supply unit includes engine, generator, battery and the electric power source distribution device being sequentially connected with；The engine is used for band
The generator operation is moved, is charged with producing electric energy to the battery；The battery again by the electric power source distribution device with it is described
Each electrical equipment of fire-fighting unmanned plane and fire-extinguishing is connected and powered.
8. fire-fighting unmanned plane and fire-extinguishing according to claim 1, it is characterised in that the unmanned plane body includes aircraft
Base, undercarriage, support shaft, propeller pedestal and propeller；The control device is arranged in the aircraft base；Institute
State undercarriage and the support shaft is each attached on the aircraft base；The support shaft is multiple, and is symmetrically distributed in institute
State aircraft base surrounding；The propeller pedestal is fixed on one end away from the aircraft base in the support shaft；Institute
Propeller is stated to be fixed on the propeller pedestal.
9. fire-fighting unmanned plane and fire-extinguishing according to claim 8, it is characterised in that include electricity in the propeller pedestal
Machine and electron speed regulator；The control device is connected with the electron speed regulator；The electron speed regulator and the motor connection；
The electron speed regulator is used to be controlled the rotating speed of motor, so as to control the rotating speed of propeller.
10. fire-fighting unmanned plane and fire-extinguishing according to claim 9, it is characterised in that also include in the propeller pedestal
Range sensor；The range sensor is used to perceive the distance of the propeller pedestal and exterior object and exported to the control
Device processed；The control device is additionally operable to when the distance is less than warning value, to the flying height and flying speed of unmanned plane
It is adjusted.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610606238.8A CN107662699A (en) | 2016-07-28 | 2016-07-28 | Fire-fighting unmanned plane and fire-extinguishing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610606238.8A CN107662699A (en) | 2016-07-28 | 2016-07-28 | Fire-fighting unmanned plane and fire-extinguishing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107662699A true CN107662699A (en) | 2018-02-06 |
Family
ID=61115240
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610606238.8A Pending CN107662699A (en) | 2016-07-28 | 2016-07-28 | Fire-fighting unmanned plane and fire-extinguishing |
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| Country | Link |
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| CN (1) | CN107662699A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108211167A (en) * | 2018-03-21 | 2018-06-29 | 齐鲁理工学院 | A kind of UAV system with sound wave fire-extinguishing function concurrently |
| CN112774058A (en) * | 2019-11-01 | 2021-05-11 | 香港理工大学深圳研究院 | Fire extinguishing system based on sound wave fire extinguishing and fire extinguishing method thereof |
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