CN105963882A - Air-to-surface rocket fire extinguisher and method - Google Patents
Air-to-surface rocket fire extinguisher and method Download PDFInfo
- Publication number
- CN105963882A CN105963882A CN201610467691.5A CN201610467691A CN105963882A CN 105963882 A CN105963882 A CN 105963882A CN 201610467691 A CN201610467691 A CN 201610467691A CN 105963882 A CN105963882 A CN 105963882A
- Authority
- CN
- China
- Prior art keywords
- fire
- air
- rocket
- fire extinguisher
- extinguishing
- 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.)
- Granted
Links
Classifications
-
- 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
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62B—DEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
- A62B1/00—Devices for lowering persons from buildings or the like
- A62B1/06—Devices for lowering persons from buildings or the like by making use of rope-lowering devices
- A62B1/16—Life-saving ropes or belts
-
- 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
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/46—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances
Abstract
The invention relates to the technical field of air attack, and discloses an air-to-surface rocket fire extinguisher and method. The air-to-surface rocket fire extinguisher involved in the method comprises a multi-rotor aircraft, rocket fire-extinguishing bombs, and a rocket launcher. The air-to-surface rocket fire extinguisher is connected to the rocket launcher by means of a bottom mounting hole 8. The rocket fire-extinguishing bombs 15 are uniformly distributed in the rocket launcher. The air-to-surface rocket fire extinguisher is capable of completely overcoming the influence of such factors as narrow surface and buildings on fire extinguishment and rescue by launching high-efficiency fire-extinguishing bombs in high accuracy at set distances from multiple directions and multiple angles, and is quick in action, and convenient to fold and unfold; a large number of fire-extinguishing bombs can be carried; therefore, the air-to-surface rocket fire extinguisher will become a new emerging air power for fire extinguishing equipment in China.
Description
Technical field
The present invention relates to air attack technical field, particularly relate to a kind of air-to-surface missile fire extinguisher and method.
Background technology
The most high-rise, Super High scale is built more and more, builds bigger and bigger, and present domestic fire-extinguishing apparatus has certain defect: 1, attack approach is limited.When rescue work is carried out, attack approach is all confined in the plane formula expansion on ground, but also to be limited by above ground structure；2, upper act limited height.Domestic or even in the world equipment of ascending a height is the highest is also at 72 meters, can not meet the needs of current high-rise rescue at all, and equipment of ascending a height is to development rate time on-the-spot slowly (ladder truck of highly 72 meters, liter puts in place and wants about 10 minutes)；3, overhead, scene of a fire air-flow is unstable.Huge manned helicopter, owing to being affected by on-the-spot air-flow, is easy to fall machine near overhead, field, the scene of a fire；4, high-rise, Super High scale is big.The whole nation is high-rise, Super High (100 meters be boundary) architectural development swift and violent, and high-rise fire is puted out a fire to save life and property and rescue work has become as the difficult problem in the world.5, extinguishing chemical means of delivery is lacked.Oil tank catches fire or uses foam fire-fighting in the past (having space just can implement after waiting oil product burning pasta decline and on pasta) now, has the extinguishing chemical that extinguishing effect is extremely strong, delivers instrument the most accurately and can not use.Fire of high-rise building is despite certain selfrescue equipment, and often fire attack is undesirable, is sought after the equipment of an outside attack to supplement control force.
Summary of the invention
For overcoming the deficiencies in the prior art, the present invention provides a kind of air-to-surface missile fire extinguisher and method.
For achieving the above object, the present invention adopts the following technical scheme that
A kind of air-to-surface missile fire extinguisher, including: multi-rotor aerocraft, rocket fire-extinguishing bullet, rocket launcher, described multi-rotor aerocraft Lower mounting hole 8, by being connected with rocket launcher, is evenly equipped with rocket fire-extinguishing bullet 15 in rocket launcher.
A kind of air-to-surface missile fire extinguisher, described rocket launcher is made up of launcher 11, transmitting tube 12, The Cloud Terrace 13 and actuator 14, and described launcher 11 is that transmitting tube 12 combination of uniform arrangement is constituted, and is provided with undercarriage 17. bottom launcher 11
A kind of air-to-surface missile fire extinguisher, described rocket fire-extinguishing bullet 15 is made up of time-delay trigger, body, charge tube, wire, fuse cord, rocket engine, body be the structure made of frangible plastic, the shell of charge tube be the structure that plastics are made, charge tube is built-in with explosive.
A kind of air-to-surface missile fire extinguisher, described rocket engine 16 is made up of shell, fuse cord hole, electrode stake, bocca, gunpowder, and shell is the structure that woollen goods are made, and shell is built-in with gunpowder.
A kind of air-to-surface missile fire extinguisher, described multi-rotor aerocraft includes: machine dish 7, machine cap 3, horn 5, propeller 4, described machine dish 7 be uniformly distributed on peripheries with horn 5, it is equipped with motor cabinet 2 on horn 5, it is equipped with propeller 4 on motor 1 fixing in motor cabinet 2, the top of described machine dish 7 is equipped with machine cap 3, battery 9 it is fixed with in machine cap 3, machine dish 7 is built-in with flight control system 10, the signal end of flight control system 10 is connected with the wireless transceiver 6 of ground remote control device communication by holding wire, the clutch end of flight control system 10 is connected by the motor 1 that wire is uniform with machine dish 7 surrounding, the bottom of machine dish 7 is equipped with rocket launcher 11.
A kind of air-to-surface missile fire extinguisher, described machine dish 7 is aluminum alloy materials structure.Described machine dish 7 is folded piece structure with horn.
A kind of air-to-surface missile fire extinguisher, carbon fibre material structure that described horn and motor cabinet are integrated or engineering plastic structure, the propeller fixed on motor in described motor cabinet is carbon fibre material structure.
A kind of air-to-surface missile fire extinguisher, described flight control system has: Automatic-searching burning things which may cause a fire disaster, detection attack distance, night vision, the function of aiming, launching effect assessment transmission function；And have and automatically and manually find target and the function of transmitting.
A kind of method of work of air-to-surface missile fire extinguisher, including: executive information systems is put out a fire, oil tank and oil pipe fire extinguishing, and height rescue；
1), carrying out executive information systems fire extinguishing, ground placed by air to surface rocket fire extinguisher, or is placed directly in roof, is in combat readiness；
Launch horn → correction magnetic compass, 50 kilometers of original place of distance is outer → check that battery, the connection → actuating remote controller → air to air rocket fire extinguisher of the rocket projectile scene of a fire → aircraft that takes off → fly to hovers → adjust emitter angle, or automatically adjust → start emission switch → control system and receive order → go out transmitting tube → body fly to the scene of a fire to electrode stake transmission electric current → electrode stake propellant ignition → electromotor flame → promotion body of striking sparks → cause, body ruptures three kinds of approach；
(1) run into glass pane, wall, tube inner wall → whole body pulverizing → extinguishing chemical leak → stamp out a fire；
(2) trigger action, body pulverizing → anterior ignition charge pipe → body pulverizing → extinguishing chemical leaks → stamps out a fire；
(3) the electromotor fuse cord → ignition charge pipe → body pulverizing → extinguishing chemical that works → light leaks → stamps out a fire；Return → land → flame-out → fold → vanning, it is in war preparedness position；
(4) recruitment evaluation, this aircraft carries video camera shoot with video-corder duty comprehensively, and earth station receives the image transmitting of aircraft simultaneously, the on-the-spot fire extinguishing situation passed according to figure, it is possible to play back and carry out the assessment of extinguishing effect；
2), carrying out oil tank and oil pipe fire extinguishing, air to surface rocket fire extinguisher is placed ground, or is placed directly in roof, is in combat readiness:
Launch horn → correction magnetic compass, 50 kilometers of original place of distance is outer → check that the connection → actuating remote controller → air to air rocket fire extinguisher of the i.e. high-efficiency fire-extinguishant of battery, the rocket projectile scene of a fire → aircraft that takes off → fly to hovers → adjust emitter angle, or automatically adjust → start emission switch → control system and receive order → go out transmitting tube → body fly to the scene of a fire to electrode stake transmission electric current → electrode stake propellant ignition → electromotor flame → promotion body of striking sparks → cause, body ruptures three kinds of approach；
(1) run into tube inner wall → whole body pulverizing → extinguishing chemical to leak → stamp out a fire；
(2) trigger action makes body pulverizing → anterior ignition charge pipe → body pulverizing → extinguishing chemical leak → stamp out a fire；
(3) the electromotor fuse cord → ignition charge pipe → body pulverizing → extinguishing chemical that works → light leaks → stamps out a fire.Return → land → flame-out → fold → vanning, it is in war preparedness position；
3), height rescue is carried out, in scene of fire or earthquake-stricken area, during in having personnel to be trapped in high level, high-rise building or complex area, mountain area, air-to-surface missile fire extinguisher filling messenger i.e. kite string can complete this task, working procedure: ground placed by air to surface rocket fire extinguisher, or it is placed directly in roof, place's combat readiness:
Launch horn → correction magnetic compass, outside 50 kilometers of original place of distance → check battery → repacking rocket projectile → vacating space, take out charge tube, extinguishing chemical, fuse cord → filling messenger i.e. kite string → closing body → body is put into launch hole → actuating remote controller → scene → hovering of taking off → fly to → receipts rope target → adjustment emitter → startup emission switch → control system and is received order → transmit electric current → electrode stake propellant ignition → electromotor flame → promotion body of striking sparks → cause to electrode stake and go out transmitting tube → body and fly to scene → run into wall or other obstacle → bodies fall or pulverize → take out lead-in wire → sued and laboured and continue lead ends and receive lead ends to ground → rescuer；
Rescuer fasten life line → by rescuer retract life line → by rescuer fix life line → by rescuer along life line skid off → safety rescued；
Rescuer fasten descending lifeline → by rescuer retract descending lifeline → by rescuer fix descending lifeline → by rescuer along descending lifeline land → personnel are rescued → descending lifeline regains, life line withdrawal → aircraft returns → lands → flame-out → folding → vanning, is in war preparedness position.
Owing to using technical scheme as above, the present invention has a following superiority:
A kind of air-to-surface missile fire extinguisher and method, it is possible to make up the shortcoming of five problems of more than background technology, the invention have the advantage that
1, work development rate is fast, can complete in one minute.Preparation can be operated in advance, by its moment combat ready/readiness.
2, there is certain carrying amount, along with the increase of the carrying amount of aircraft can increase to several rocket fire-extinguishing bullets equipped with high-efficiency fire-extinguishant.
3, can from multiple orientation, multiple angle, a certain distance interval, degree of precision, from air-launched high-effect fire-extinguishing bullet, overcome completely because of ground faciostenosis, building go the impact on fire fighting and rescue of the factors such as impact.
4, there are real-time recording, image to transmit constantly, can be that assessment extinguishing effect provides video data.
5, can fold, facilitate air to surface rocket fire extinguisher to enter narrow area, be also convenient for transport and the transition of equipment, this invention will become the newborn air power of domestic fire-extinguishing apparatus.
Accompanying drawing explanation
Fig. 1 is the structural representation of air-to-surface missile fire extinguisher；
Fig. 2 is the structural representation of rocket fire-extinguishing bullet；
Fig. 3 is the structural representation of rocket engine；
Fig. 4 is the structural representation of rocket launcher.
Detailed description of the invention
As shown in Figure 1,2,3, 4, a kind of air-to-surface missile fire extinguisher, including: multi-rotor aerocraft, rocket fire-extinguishing bullet, rocket launcher, described multi-rotor aerocraft Lower mounting hole 8, by being connected with rocket launcher, is evenly equipped with rocket fire-extinguishing bullet 15 in rocket launcher.
Described rocket launcher is made up of launcher 11, transmitting tube 12, The Cloud Terrace 13 and actuator 14, and described launcher 11 is that transmitting tube 12 combination of uniform arrangement is constituted, and is provided with undercarriage 17 bottom launcher 11.As shown in Figure 4.
Described rocket fire-extinguishing bullet 15 is made up of time-delay trigger, body, charge tube, wire, fuse cord, rocket engine, body be the structure made of frangible plastic, the shell of charge tube be the structure that plastics are made, charge tube is built-in with explosive.As shown in Figure 2.
Described rocket engine 16 is made up of shell, fuse cord hole, electrode stake, bocca, gunpowder, and shell is the structure that woollen goods are made, and shell is built-in with gunpowder.
Described multi-rotor aerocraft includes: machine dish 7, machine cap 3, horn 5, propeller 4, described machine dish 7 be uniformly distributed on peripheries with horn 5, it is equipped with motor cabinet 2 on horn 5, it is equipped with propeller 4 on motor 1 fixing in motor cabinet 2, the top of described machine dish 7 is equipped with machine cap 3, battery 9 it is fixed with in machine cap 3, machine dish 7 is built-in with flight control system 10, the signal end of flight control system 10 is connected with the wireless transceiver 6 of ground remote control device communication by holding wire, the clutch end of flight control system 10 is connected by the motor 1 that wire is uniform with machine dish 7 surrounding, the bottom of machine dish 7 is equipped with rocket launcher 11.
Described machine dish 7 is aluminum alloy materials structure.Described machine dish 7 is folded piece structure with horn.Carbon fibre material structure that described horn and motor cabinet are integrated or engineering plastic structure, propeller fixing on motor in described motor cabinet is carbon fibre material structure.As shown in Figure 1.
Described flight control system has: Automatic-searching burning things which may cause a fire disaster, detection attack distance, night vision, the function of aiming, launching effect assessment transmission function；And have and automatically and manually find target and the function of transmitting.
The automatic control system of described control system has the function that the tracking of Automatic-searching burning things which may cause a fire disaster, far infrared, detection transmitting range, laser ranging and far infrared night vision, far infrared aim at；Can also use manual control system, manual control system has manually to be found target and launches operating function.
The work of this air to surface rocket fire extinguisher includes: high-rise, high-rise building fire extinguishing, oil tank, oil pipe are put out a fire, and height rescue.And can fold, it is simple to transport；Also have VTOL, hover, advance, retreat, the basic function such as turning.
Embodiment 1
A kind of method of work of air-to-surface missile fire extinguisher, carry out executive information systems fire extinguishing, ground placed by air to surface rocket fire extinguisher, or it is placed directly in roof, it is in combat readiness, launch horn → correction magnetic compass, outside 50 kilometers of original place of distance → check battery, the connection of the rocket projectile → actuating remote controller → air to air rocket fire extinguisher scene of a fire → aircraft that takes off → fly to hovers → adjusts emitter angle, or automatically adjust → start emission switch → control system and receive order → go out transmitting tube → body fly to the scene of a fire to electrode stake transmission electric current → electrode stake propellant ignition → electromotor flame → promotion body of striking sparks → cause, body ruptures three kinds of approach；
(1) run into glass pane, wall, tube inner wall → whole body pulverizing → extinguishing chemical leak → stamp out a fire；
(2) trigger action, body pulverizing → anterior ignition charge pipe → body pulverizing → extinguishing chemical leaks → stamps out a fire；
(3) the electromotor fuse cord → ignition charge pipe → body pulverizing → extinguishing chemical that works → light leaks → stamps out a fire；Return → land → flame-out → fold → vanning, it is in war preparedness position；
(4) recruitment evaluation, this aircraft carries video camera shoot with video-corder duty comprehensively, and earth station receives the image transmitting of aircraft simultaneously, the on-the-spot fire extinguishing situation passed according to figure, it is possible to play back and carry out the assessment of extinguishing effect.
Embodiment 2
A kind of method of work of air-to-surface missile fire extinguisher, carry out oil tank and oil pipe fire extinguishing, ground placed by air to surface rocket fire extinguisher, or it is placed directly in roof, it is in combat readiness: launch horn → correction magnetic compass, outside 50 kilometers of original place of distance → check battery, the connection of the i.e. high-efficiency fire-extinguishant of the rocket projectile → actuating remote controller → air to air rocket fire extinguisher scene of a fire → aircraft that takes off → fly to hovers → adjusts emitter angle, or automatically adjust → start emission switch → control system and receive order → go out transmitting tube → body fly to the scene of a fire to electrode stake transmission electric current → electrode stake propellant ignition → electromotor flame → promotion body of striking sparks → cause, body ruptures three kinds of approach；
(1) run into tube inner wall → whole body pulverizing → extinguishing chemical to leak → stamp out a fire；
(2) trigger action makes body pulverizing → anterior ignition charge pipe → body pulverizing → extinguishing chemical leak → stamp out a fire；
(3) the electromotor fuse cord → ignition charge pipe → body pulverizing → extinguishing chemical that works → light leaks → stamps out a fire.Return → land → flame-out → fold → vanning, it is in war preparedness position；
Embodiment 3
The method of work of a kind of air-to-surface missile fire extinguisher, carries out height rescue, in scene of fire or earthquake-stricken area, during in having personnel to be trapped in high level, high-rise building or complex area, mountain area, when other equipment can not complete this task.Air-to-surface missile fire extinguisher filling messenger i.e. kite string can complete this task, working procedure: ground placed by air to surface rocket fire extinguisher, or is placed directly in roof, place's combat readiness:
Launch horn → correction magnetic compass, outside 50 kilometers of original place of distance → check battery → repacking rocket projectile → vacating space, take out charge tube, extinguishing chemical, fuse cord → filling messenger i.e. kite string → closing body → body is put into launch hole → actuating remote controller → scene → hovering of taking off → fly to → receipts rope target → adjustment emitter → startup emission switch → control system and is received order → transmit electric current → electrode stake propellant ignition → electromotor flame → promotion body of striking sparks → cause to electrode stake and go out transmitting tube → body and fly to scene → run into wall or other obstacle → bodies fall or pulverize → take out lead-in wire → sued and laboured and continue lead ends and receive lead ends to ground → rescuer；
Rescuer fasten life line → by rescuer retract life line → by rescuer fix life line → by rescuer along life line skid off → safety rescued；
Rescuer fasten descending lifeline → by rescuer retract descending lifeline → by rescuer fix descending lifeline → by rescuer along descending lifeline land → personnel are rescued → descending lifeline regains, life line withdrawal → aircraft returns → lands → flame-out → folding → vanning, is in war preparedness position.
Above-described embodiment can carry out recruitment evaluation, and aircraft carries video camera shoot with video-corder duty comprehensively, and earth station receives the image transmitting of aircraft simultaneously.The on-the-spot fire extinguishing situation passed according to figure can be passed back with scene photo and put the assessment of row extinguishing effect, launching effect assessment into.
Claims (9)
1. an air-to-surface missile fire extinguisher, is characterized in that: including: multi-rotor aerocraft, rocket fire-extinguishing bullet, rocket launcher, and described multi-rotor aerocraft Lower mounting hole 8, by being connected with rocket launcher, is evenly equipped with rocket fire-extinguishing bullet 15 in rocket launcher.
2. a kind of air-to-surface missile fire extinguisher as claimed in claim 1, it is characterized in that: described rocket launcher is made up of launcher 11, transmitting tube 12, The Cloud Terrace 13 and actuator 14, described launcher 11 is that transmitting tube 12 combination of uniform arrangement is constituted, and is provided with undercarriage 17 bottom launcher 11.
3. a kind of air-to-surface missile fire extinguisher as claimed in claim 1, it is characterized in that: described rocket fire-extinguishing bullet 15 is made up of time-delay trigger, body, charge tube, wire, fuse cord, rocket engine, body be the structure made of frangible plastic, the shell of charge tube be the structure that plastics are made, charge tube is built-in with explosive.
4. a kind of air-to-surface missile fire extinguisher as claimed in claim 1, is characterized in that: described rocket engine 16 is made up of shell, fuse cord hole, electrode stake, bocca, gunpowder, and shell is the structure that woollen goods are made, and shell is built-in with gunpowder.
5. a kind of air-to-surface missile fire extinguisher as claimed in claim 1, it is characterized in that: described multi-rotor aerocraft includes: machine dish 7, machine cap 3, horn 5, propeller 4, described machine dish 7 be uniformly distributed on peripheries with horn 5, it is equipped with motor cabinet 2 on horn 5, it is equipped with propeller 4 on motor 1 fixing in motor cabinet 2, the top of described machine dish 7 is equipped with machine cap 3, battery 9 it is fixed with in machine cap 3, machine dish 7 is built-in with flight control system 10, the signal end of flight control system 10 is connected with the wireless transceiver 6 of ground remote control device communication by holding wire, the clutch end of flight control system 10 is connected by the motor 1 that wire is uniform with machine dish 7 surrounding, the bottom of machine dish 7 is equipped with rocket launcher 11.
6. a kind of air-to-surface missile fire extinguisher as claimed in claim 1, is characterized in that: described machine dish 7 is aluminum alloy materials structure.Described machine dish 7 is folded piece structure with horn.
7. air-to-surface missile fire extinguisher as claimed in claim 1 a kind of, is characterized in that: carbon fibre material structure that described horn and motor cabinet are integrated or engineering plastic structure, the propeller fixed on motor in described motor cabinet is carbon fibre material structure.
8. a kind of air-to-surface missile fire extinguisher as claimed in claim 1, is characterized in that: described flight control system has: Automatic-searching burning things which may cause a fire disaster, detection attack distance, night vision, the function of aiming, launching effect assessment transmission function；And have and automatically and manually find target and the function of transmitting.
The method of work of a kind of air-to-surface missile fire extinguisher the most as claimed in claim 1, is characterized in that: including: executive information systems is put out a fire, oil tank and oil pipe fire extinguishing, and height rescue；
1), carrying out executive information systems fire extinguishing, ground placed by air to surface rocket fire extinguisher, or is placed directly in roof, is in combat readiness；
Launch horn → correction magnetic compass, 50 kilometers of original place of distance is outer → check that battery, the connection → actuating remote controller → air to air rocket fire extinguisher of the rocket projectile scene of a fire → aircraft that takes off → fly to hovers → adjust emitter angle, or automatically adjust → start emission switch → control system and receive order → go out transmitting tube → body fly to the scene of a fire to electrode stake transmission electric current → electrode stake propellant ignition → electromotor flame → promotion body of striking sparks → cause, body ruptures three kinds of approach；
(1) run into glass pane, wall, tube inner wall → whole body pulverizing → extinguishing chemical leak → stamp out a fire；
(2) trigger action, body pulverizing → anterior ignition charge pipe → body pulverizing → extinguishing chemical leaks → stamps out a fire；
(3) the electromotor fuse cord → ignition charge pipe → body pulverizing → extinguishing chemical that works → light leaks → stamps out a fire；Return → land → flame-out → fold → vanning, it is in war preparedness position；
(4) recruitment evaluation, this aircraft carries video camera shoot with video-corder duty comprehensively, and earth station receives the image transmitting of aircraft simultaneously, the on-the-spot fire extinguishing situation passed according to figure, it is possible to play back and carry out the assessment of extinguishing effect；
2), carrying out oil tank and oil pipe fire extinguishing, air to surface rocket fire extinguisher is placed ground, or is placed directly in roof, is in combat readiness:
Launch horn → correction magnetic compass, 50 kilometers of original place of distance is outer → check that the connection → actuating remote controller → air to air rocket fire extinguisher of the i.e. high-efficiency fire-extinguishant of battery, the rocket projectile scene of a fire → aircraft that takes off → fly to hovers → adjust emitter angle, or automatically adjust → start emission switch → control system and receive order → go out transmitting tube → body fly to the scene of a fire to electrode stake transmission electric current → electrode stake propellant ignition → electromotor flame → promotion body of striking sparks → cause, body ruptures three kinds of approach；
(1) run into tube inner wall → whole body pulverizing → extinguishing chemical to leak → stamp out a fire；
(2) trigger action makes body pulverizing → anterior ignition charge pipe → body pulverizing → extinguishing chemical leak → stamp out a fire；
(3) the electromotor fuse cord → ignition charge pipe → body pulverizing → extinguishing chemical that works → light leaks → stamps out a fire.Return → land → flame-out → fold → vanning, it is in war preparedness position；
3), height rescue is carried out, in scene of fire or earthquake-stricken area, during in having personnel to be trapped in high level, high-rise building or complex area, mountain area, air-to-surface missile fire extinguisher filling messenger i.e. kite string can complete this task, working procedure: ground placed by air to surface rocket fire extinguisher, or it is placed directly in roof, place's combat readiness:
Launch horn → correction magnetic compass, outside 50 kilometers of original place of distance → check battery → repacking rocket projectile → vacating space, take out charge tube, extinguishing chemical, fuse cord → filling messenger i.e. kite string → closing body → body is put into launch hole → actuating remote controller → scene → hovering of taking off → fly to → receipts rope target → adjustment emitter → startup emission switch → control system and is received order → transmit electric current → electrode stake propellant ignition → electromotor flame → promotion body of striking sparks → cause to electrode stake and go out transmitting tube → body and fly to scene → run into wall or other obstacle → bodies fall or pulverize → take out lead-in wire → sued and laboured and continue lead ends and receive lead ends to ground → rescuer；
Rescuer fasten life line → by rescuer retract life line → by rescuer fix life line → by rescuer along life line skid off → safety rescued；
Rescuer fasten descending lifeline → by rescuer retract descending lifeline → by rescuer fix descending lifeline → by rescuer along descending lifeline land → personnel are rescued → descending lifeline regains, life line withdrawal → aircraft returns → lands → flame-out → folding → vanning, is in war preparedness position.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610467691.5A CN105963882B (en) | 2016-06-24 | 2016-06-24 | Air-to-ground rocket fire extinguisher and method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610467691.5A CN105963882B (en) | 2016-06-24 | 2016-06-24 | Air-to-ground rocket fire extinguisher and method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105963882A true CN105963882A (en) | 2016-09-28 |
| CN105963882B CN105963882B (en) | 2022-03-04 |
Family
ID=57020553
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610467691.5A Active CN105963882B (en) | 2016-06-24 | 2016-06-24 | Air-to-ground rocket fire extinguisher and method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105963882B (en) |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106267637A (en) * | 2016-10-12 | 2017-01-04 | 江苏溧航航空科技有限公司 | UAV system fire extinguisher bomb |
| CN106847049A (en) * | 2017-03-15 | 2017-06-13 | 佛山市三水区希望火炬教育科技有限公司 | A kind of high speed fire extinguishing ship of coastal waters manufacturing products for both peacetime and wartime us |
| CN107583218A (en) * | 2017-10-09 | 2018-01-16 | 黄文佳 | A kind of fire-fighting fire-extinguishing equipment |
| CN107596604A (en) * | 2017-10-09 | 2018-01-19 | 黄文佳 | A kind of fire-fighting equipment |
| CN107670207A (en) * | 2017-10-09 | 2018-02-09 | 黄文佳 | A kind of fire-extinguishing apparatus |
| CN107899164A (en) * | 2017-10-10 | 2018-04-13 | 重庆长安工业(集团)有限责任公司 | Non-emissive medicine water-drop-shaped fire extinguisher bomb |
| CN108313294A (en) * | 2018-02-27 | 2018-07-24 | 北京汇能智源科技有限公司 | A kind of fire-fighting fire extinguishing ball emission system being equipped on unmanned plane |
| CN108357676A (en) * | 2018-04-09 | 2018-08-03 | 重庆国飞通用航空设备制造有限公司 | A kind of multifunction emergency rescue multi-rotor unmanned aerial vehicle system |
| CN108438542A (en) * | 2017-10-09 | 2018-08-24 | 黄文佳 | A kind of express delivery box |
| CN109131857A (en) * | 2018-05-04 | 2019-01-04 | 江国春 | Petrol engine drives more rotor fire extinguishment rescue manned vehicles |
| CN109436329A (en) * | 2018-12-03 | 2019-03-08 | 张家蔚 | A kind of small drone precisely emits the device and method of relief supplies in the air |
| CN111991722A (en) * | 2020-08-31 | 2020-11-27 | 熊新明 | Forest auxiliary device that puts out a fire |
| CN112915422A (en) * | 2021-03-04 | 2021-06-08 | 西北工业大学 | Solid fire extinguishing bomb fire-fighting system |
| US20230308042A1 (en) * | 2022-01-27 | 2023-09-28 | Ameristar Solar, LLC | SOLAR eVTOL DRONE TOWER |
| CN109436329B (en) * | 2018-12-03 | 2024-04-30 | 张家蔚 | Device and method for accurately transmitting rescue articles in air by small unmanned aerial vehicle |
Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101367435A (en) * | 2008-09-16 | 2009-02-18 | 广州伟韬电子科技有限公司 | Novel air injection aerial vehicle |
| CN202449208U (en) * | 2012-02-21 | 2012-09-26 | 吴泽邦 | Multipurpose unmanned aerial vehicle platform for continuously feeding water, extinguishing fire in air and rescuing |
| US8502063B1 (en) * | 2012-06-12 | 2013-08-06 | The Boeing Company | Miniature torpedo |
| CN104027909A (en) * | 2014-06-11 | 2014-09-10 | 江苏数字鹰科技发展有限公司 | Police fire-fighting unmanned aerial vehicle for high-rise building |
| CN204161623U (en) * | 2014-09-05 | 2015-02-18 | 徐伟佳 | A kind of unmanned plane air attack bullet dispenser |
| CN104554657A (en) * | 2015-01-23 | 2015-04-29 | 胡家诚 | Method for dispensing rescue equipment by utilizing unmanned plane |
| CN104590562A (en) * | 2015-02-12 | 2015-05-06 | 马鞍山市赛迪智能科技有限公司 | Anti-collision fixed-point unmanned aerial vehicle for fire control |
| CN104627366A (en) * | 2015-02-10 | 2015-05-20 | 曹兵 | Oil drive variable pitch quadrotor type multifunctional fire-fighting unmanned aerial vehicle |
| CN104875889A (en) * | 2015-06-11 | 2015-09-02 | 中国人民解放军第二军医大学东方肝胆外科医院 | Navigation type sea falling personnel rescue and salvage helicopter |
| CN105129091A (en) * | 2015-08-13 | 2015-12-09 | 王清洁 | Extinguishing device for unmanned aerial vehicle |
| CN105667795A (en) * | 2016-01-18 | 2016-06-15 | 江苏顶飞航空科技有限公司 | Fire extinguishing bomb launching system for unmanned aerial vehicle |
| CN206007850U (en) * | 2016-06-24 | 2017-03-15 | 河南沃野智能科技有限公司 | Air-to-surface missile fire extinguisher |
-
2016
- 2016-06-24 CN CN201610467691.5A patent/CN105963882B/en active Active
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101367435A (en) * | 2008-09-16 | 2009-02-18 | 广州伟韬电子科技有限公司 | Novel air injection aerial vehicle |
| CN202449208U (en) * | 2012-02-21 | 2012-09-26 | 吴泽邦 | Multipurpose unmanned aerial vehicle platform for continuously feeding water, extinguishing fire in air and rescuing |
| US8502063B1 (en) * | 2012-06-12 | 2013-08-06 | The Boeing Company | Miniature torpedo |
| CN104027909A (en) * | 2014-06-11 | 2014-09-10 | 江苏数字鹰科技发展有限公司 | Police fire-fighting unmanned aerial vehicle for high-rise building |
| CN204161623U (en) * | 2014-09-05 | 2015-02-18 | 徐伟佳 | A kind of unmanned plane air attack bullet dispenser |
| CN104554657A (en) * | 2015-01-23 | 2015-04-29 | 胡家诚 | Method for dispensing rescue equipment by utilizing unmanned plane |
| CN104627366A (en) * | 2015-02-10 | 2015-05-20 | 曹兵 | Oil drive variable pitch quadrotor type multifunctional fire-fighting unmanned aerial vehicle |
| CN104590562A (en) * | 2015-02-12 | 2015-05-06 | 马鞍山市赛迪智能科技有限公司 | Anti-collision fixed-point unmanned aerial vehicle for fire control |
| CN104875889A (en) * | 2015-06-11 | 2015-09-02 | 中国人民解放军第二军医大学东方肝胆外科医院 | Navigation type sea falling personnel rescue and salvage helicopter |
| CN105129091A (en) * | 2015-08-13 | 2015-12-09 | 王清洁 | Extinguishing device for unmanned aerial vehicle |
| CN105667795A (en) * | 2016-01-18 | 2016-06-15 | 江苏顶飞航空科技有限公司 | Fire extinguishing bomb launching system for unmanned aerial vehicle |
| CN206007850U (en) * | 2016-06-24 | 2017-03-15 | 河南沃野智能科技有限公司 | Air-to-surface missile fire extinguisher |
Non-Patent Citations (1)
| Title |
|---|
| 黄儒虎 等: "《标准信息大全》", 31 January 2005, 知识产权出版社 * |
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106267637B (en) * | 2016-10-12 | 2022-08-19 | 江苏溧航航空科技有限公司 | Unmanned aerial vehicle carries fire extinguishing bomb |
| CN106267637A (en) * | 2016-10-12 | 2017-01-04 | 江苏溧航航空科技有限公司 | UAV system fire extinguisher bomb |
| CN106847049A (en) * | 2017-03-15 | 2017-06-13 | 佛山市三水区希望火炬教育科技有限公司 | A kind of high speed fire extinguishing ship of coastal waters manufacturing products for both peacetime and wartime us |
| CN107583218B (en) * | 2017-10-09 | 2020-04-17 | 山东久泰煤安装备有限公司 | Fire-fighting equipment |
| CN107583218A (en) * | 2017-10-09 | 2018-01-16 | 黄文佳 | A kind of fire-fighting fire-extinguishing equipment |
| CN107596604A (en) * | 2017-10-09 | 2018-01-19 | 黄文佳 | A kind of fire-fighting equipment |
| CN107670207A (en) * | 2017-10-09 | 2018-02-09 | 黄文佳 | A kind of fire-extinguishing apparatus |
| CN107596604B (en) * | 2017-10-09 | 2020-07-21 | 浙江企信检测有限公司 | Fire fighting equipment |
| CN108438542A (en) * | 2017-10-09 | 2018-08-24 | 黄文佳 | A kind of express delivery box |
| CN107670207B (en) * | 2017-10-09 | 2020-05-05 | 北京市巨龙工程有限公司 | Fire extinguishing equipment |
| CN107899164A (en) * | 2017-10-10 | 2018-04-13 | 重庆长安工业(集团)有限责任公司 | Non-emissive medicine water-drop-shaped fire extinguisher bomb |
| CN108313294A (en) * | 2018-02-27 | 2018-07-24 | 北京汇能智源科技有限公司 | A kind of fire-fighting fire extinguishing ball emission system being equipped on unmanned plane |
| CN108357676A (en) * | 2018-04-09 | 2018-08-03 | 重庆国飞通用航空设备制造有限公司 | A kind of multifunction emergency rescue multi-rotor unmanned aerial vehicle system |
| CN109131857A (en) * | 2018-05-04 | 2019-01-04 | 江国春 | Petrol engine drives more rotor fire extinguishment rescue manned vehicles |
| CN109436329A (en) * | 2018-12-03 | 2019-03-08 | 张家蔚 | A kind of small drone precisely emits the device and method of relief supplies in the air |
| CN109436329B (en) * | 2018-12-03 | 2024-04-30 | 张家蔚 | Device and method for accurately transmitting rescue articles in air by small unmanned aerial vehicle |
| CN111991722A (en) * | 2020-08-31 | 2020-11-27 | 熊新明 | Forest auxiliary device that puts out a fire |
| CN112915422A (en) * | 2021-03-04 | 2021-06-08 | 西北工业大学 | Solid fire extinguishing bomb fire-fighting system |
| CN112915422B (en) * | 2021-03-04 | 2022-05-31 | 西北工业大学 | Solid fire extinguishing bomb fire-fighting system |
| US20230308042A1 (en) * | 2022-01-27 | 2023-09-28 | Ameristar Solar, LLC | SOLAR eVTOL DRONE TOWER |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105963882B (en) | 2022-03-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105963882A (en) | Air-to-surface rocket fire extinguisher and method | |
| CN102785778B (en) | A kind of tubular type launches fire extinguishing unmanned plane and fire extinguishing control method | |
| CN107161328B (en) | Projectile type disaster rescue and fire extinguishing unmanned aerial vehicle | |
| CN109383806B (en) | Triggering method for launching fire monitor of fire-fighting unmanned aerial vehicle | |
| US7121353B2 (en) | Airborne vehicle for firefighting | |
| CN206007850U (en) | Air-to-surface missile fire extinguisher | |
| CN107670201A (en) | UAV system type fire extinguishing system | |
| CN104027909A (en) | Police fire-fighting unmanned aerial vehicle for high-rise building | |
| CN104590562A (en) | Anti-collision fixed-point unmanned aerial vehicle for fire control | |
| US9795812B2 (en) | Fire retardant delivery method and apparatus | |
| US20160325127A1 (en) | Laser System Module-Equipped Firefighting Aircraft | |
| CN203944052U (en) | The police fire extinguishing unmanned plane of high building | |
| CN109305364B (en) | Aiming method of fire-fighting unmanned aerial vehicle | |
| CN108619641B (en) | Fire extinguishing system and method for vertical emission guidance fire extinguishing body | |
| KR20170133619A (en) | The drone with fire extinguisher material kamikaze landing at the fire place, and the remote control and monitoring device or the firefighting system | |
| CN108771803A (en) | Control system and fire extinguishing system for the fire extinguishing of skyscraper rotor wing unmanned aerial vehicle | |
| CN109310056A (en) | The aircraft and system changed for weather | |
| US11542002B1 (en) | Unmanned aerial vehicle and control systems and methods | |
| CN103112385A (en) | Fire rescue device based on unmanned aerial vehicle | |
| WO2023070787A1 (en) | Airdrop forest fire extinguishing bomb | |
| CN110816843A (en) | Fire extinguishing system for high-rise building | |
| US20160339280A1 (en) | Fire Extinguishing Pod | |
| US20230106432A1 (en) | Unmanned system maneuver controller systems and methods | |
| CN112618992B (en) | Low-cost suicide networking fire extinguishing method and unmanned aerial vehicle system | |
| CN114432625A (en) | Remote accurate guidance fire extinguishing bomb |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |