CN206007850U - Air-to-surface missile fire extinguisher - Google Patents
Air-to-surface missile fire extinguisher Download PDFInfo
- Publication number
- CN206007850U CN206007850U CN201620635910.1U CN201620635910U CN206007850U CN 206007850 U CN206007850 U CN 206007850U CN 201620635910 U CN201620635910 U CN 201620635910U CN 206007850 U CN206007850 U CN 206007850U
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- air
- rocket
- fire
- fire extinguisher
- launcher
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Abstract
This utility model is related to air attack technical field, discloses a kind of air-to-surface missile fire extinguisher, including：Multi-rotor aerocraft, rocket fire-extinguishing bullet, rocket launcher, the multi-rotor aerocraft Lower mounting hole 8 are evenly equipped with rocket fire-extinguishing bullet 15 by being connected with rocket launcher in rocket launcher.This utility model can from multiple orientation, multiple angles, set distance interval, degree of precision, from air-launched high-effect fire-extinguishing bullet, overcome completely impact of the factors such as impact to putting out a fire and rescue is gone because of ground faciostenosis, building, and the development rate that works is fast, fold, launch conveniently, the amount for carrying rocket fire-extinguishing bullet is big, and the air-to-surface missile fire extinguisher will become the newborn air power of domestic fire-extinguishing apparatus.
Description
Technical field
This utility model is related to air attack technical field, more particularly to a kind of air-to-surface missile fire extinguisher.
Background technology
High-rise, Super High scale is built more and more at present, builds bigger and bigger, and the fire-extinguishing apparatus of the present country have certain lacking
Fall into：1st, attack approach is limited.When rescue works are carried out, attack approach is all confined in the plane formula expansion on ground, but also will
Limited by above ground structure；2nd, upper act limited height.Domestic or even equipment highest of ascending a height in the world also simply at 72 meters, root
Originally the needs of current high-rise rescue are can not meet, and equipment of ascending a height is slow to development rate during scene（Highly 72 meters
Ladder truck, rises and wants 10 minutes or so in place）；3rd, on the scene of a fire, air stream is unstable.Huge manned helicopter is due to by live air-flow
Impact, be easy to fall machine near scene of a fire field overhead；4th, high-rise, Super High scale is big.National high-rise, Super High（100 meters are
Boundary）Architectural development is swift and violent, and high-rise fire is puted out a fire to save life and property and has become the difficult problem in the world with rescue works.5th, lack extinguishing chemical means of delivery.
Oil tank catches fire or using foam fire-fighting in the past now（There is after waiting oil product burning pasta to decline and on pasta the space just can be with
Implement）, have the extinguishing chemical that extinguishing effect is extremely strong, can not use due to a lack of accurately instrument is delivered.Fire of high-rise building although
There is certain selfrescue equipment, often fire attack is undesirable, be sought after the equipment of an outside attack to supplement control force.
Content of the invention
For overcoming the deficiencies in the prior art, this utility model to provide a kind of air-to-surface missile fire extinguisher.
For achieving the above object, this utility model is adopted the following technical scheme that：
A kind of air-to-surface missile fire extinguisher, including：Multi-rotor aerocraft, rocket fire-extinguishing bullet, rocket launcher, many rotations
Rotor aircraft Lower mounting hole 8 is evenly equipped with rocket fire-extinguishing bullet 15 with rocket launcher by being connected, in rocket launcher.
A kind of air-to-surface missile fire extinguisher, the rocket launcher by launcher 11, transmitting tube 12, head 13 and execute machine
Structure 14 is constituted, and the launcher 11 is constituted for the combination of transmitting tube 12 for uniformly arranging, and 11 bottom of launcher is provided with undercarriage 17.
A kind of air-to-surface missile fire extinguisher, the rocket fire-extinguishing bullet 15 by time-delay trigger, body, charge tube, wire, lead
Fiery rope, rocket engine composition, the structure that structure that body is made for frangible plastic, the shell of charge tube are made for plastics are fried
Pencil is built-in with explosive.
A kind of air-to-surface missile fire extinguisher, the rocket engine 16 is by shell, fuse cord hole, electrode stake, bocca, fire
Medicine is constituted, and the structure that shell is made for woollen goods, shell are built-in with gunpowder.
A kind of air-to-surface missile fire extinguisher, the multi-rotor aerocraft include：Machine disk 7, machine cap 3, horn 5, propeller 4,
The machine disk 7 is uniformly distributed on peripheries with horn 5, is equipped with motor cabinet 2 on horn 5, is equipped with spiral shell in motor cabinet 2 on fixed motor 1
Rotation oar 4, the top of the machine disk 7 are equipped with machine cap 3, are fixed with battery 9 in machine cap 3, and machine disk 7 is built-in with flight control system 10, flies control
The signal end of system 10 is connected by the wireless transceiver 6 that holding wire is communicated with ground remote control device, and the power of flight control system 10 is defeated
Go out end to be connected by the wire motor 1 uniform with 7 surrounding of machine disk, the bottom of machine disk 7 is equipped with rocket launcher 11.
A kind of air-to-surface missile fire extinguisher, described machine disk 7 are aluminum alloy materials structure.Described machine disk 7 with horn is
Folded piece structure.
A kind of air-to-surface missile fire extinguisher, carbon fibre material structure or engineering plastic that described horn is integrated with motor cabinet
Material structure, in the motor cabinet, fixed propeller on motor is carbon fibre material structure.
A kind of air-to-surface missile fire extinguisher, described flight control system have：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 the function of automatically and manually finding target and transmitting.
There is following superiority due to adopting technical scheme as above, this utility model：
A kind of air-to-surface missile fire extinguisher, can make up the shortcoming of more than background technology five problems, and its advantage is：
1st, work development rate is fast, can complete in one minute.Preparation is operated in advance can, by its moment in war
Standby state.
2nd, there is certain carrying amount, as the increase of the carrying amount of aircraft can increase to several equipped with high-effect fire-extinguishing
The rocket fire-extinguishing bullet of agent.
3rd, can from multiple orientation, multiple angles, a certain distance interval, degree of precision, from air-launched high-effect fire-extinguishing
Bullet, overcomes completely and goes the impacts of the factor to fire fighting and rescue such as impact because of ground faciostenosis, building.
4th, there are real-time recording, image constantly to transmit, video data can be provided for assessing extinguishing effect.
5th, can fold, facilitate air to surface rocket fire extinguisher to enter narrow area, be also convenient for the transport and transition of equipment, this
Bright will become the newborn air power of domestic fire-extinguishing apparatus.
Description of the drawings
Structural representations of the Fig. 1 for air-to-surface missile fire extinguisher；
Structural representations of the Fig. 2 for rocket fire-extinguishing bullet；
Structural representations of the Fig. 3 for rocket engine；
Structural representations of the Fig. 4 for rocket launcher.
Specific embodiment
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, fire
Arrow emitter, the multi-rotor aerocraft Lower mounting hole 8 are evenly equipped with fire by being connected with rocket launcher in rocket launcher
Arrow fire extinguisher bomb 15.
The rocket launcher is made up of launcher 11, transmitting tube 12, head 13 and actuator 14, the launcher 11
The combination of transmitting tube 12 for uniformly arranging is constituted, and 11 bottom of launcher is provided with undercarriage 17.As shown in Figure 4.
The rocket fire-extinguishing bullet 15 is made up of time-delay trigger, body, charge tube, wire, fuse cord, rocket engine,
The structure that structure that body is made for frangible plastic, the shell of charge tube are made for plastics, charge tube are built-in with explosive.Such as Fig. 2
Shown.
The rocket engine 16 is made up of shell, fuse cord hole, electrode stake, bocca, gunpowder, and shell is made up of woollen goods
Structure, shell is built-in with gunpowder.
The multi-rotor aerocraft includes：Machine disk 7, machine cap 3, horn 5, propeller 4, the machine disk 7 are uniformly distributed on peripheries with
Horn 5, is equipped with motor cabinet 2 on horn 5, is equipped with propeller 4, the top of the machine disk 7 in motor cabinet 2 on fixed motor 1
Machine cap 3 is equipped with, battery 9 in machine cap 3, is fixed with, machine disk 7 is built-in with flight control system 10, and the signal end of flight control system 10 passes through signal
The wireless transceiver 6 that line is communicated with ground remote control device is connected, and the clutch end of flight control system 10 is by wire and 7 surrounding of machine disk
Uniform motor 1 is connected, and the bottom of machine disk 7 is equipped with rocket launcher 11.
Described machine disk 7 is aluminum alloy materials structure.Described machine disk 7 is folded piece structure with horn.Described horn
The carbon fibre material structure being integrated with motor cabinet or engineering plastic structure, in the motor cabinet, fixed propeller on motor 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 at, launching effect are commented
Estimate transmission function；And have the function of automatically and manually finding target and transmitting.
The automatic control system of the control system has Automatic-searching burning things which may cause a fire disaster, far infrared tracking, detection transmitting range, laser
The function that range finding and far infrared night vision, far infrared are aimed at；Manual control system can also be adopted, manual control system has seeks manually
Look for target and transmitting operating function.
The work of the air to surface rocket fire extinguisher includes：The fire extinguishing of high-rise, high-rise building, oil tank, oil pipe fire extinguishing, and high-altitude are rescued
Help.And can fold, be readily transported；The also basic function such as VTOL, hovering, advance, retrogressing, turning.
Embodiment 1
A kind of method of work of air-to-surface missile fire extinguisher, carries out executive information systems fire extinguishing, and air to surface rocket is put out a fire
Ground placed by device, or is placed directly in roof, is in combat readiness, launches horn → correction magnetic compass, outer apart from 50 kilometers of original place
→ check that battery, the connection → actuating remote control → air to air rocket fire extinguisher of rocket projectile take off → fly to the scene of a fire → aircraft hovering
→ adjustment emitter angle, or adjust automatically → startups emission switch → control system be connected to order → to electrode stake transmission electric current
→ electrode stake propellant ignition → electromotor flame → promotion body of striking sparks → cause goes out transmitting tube → body and flies to the scene of a fire, and body breaks
Split three kinds of approach；
（1）Run into glass pane, wall, tube inner wall → whole body crushing → extinguishing chemical to leak → stamp out a fire；
（2）Trigger action, body crushes → and anterior ignition charge pipe → body crushing → extinguishing chemical leaks → put out fire
Calamity；
（3）Electromotor work → light fuse cord → ignition charge pipe → body crushing → extinguishing chemical leak → put out fire
Calamity；Return → land → flame-out → → vanning is folded, it is in war preparedness position；
（4）Recruitment evaluation, the aircraft carry video camera and working condition are shot with video-corder comprehensively, and earth station receives winged simultaneously
The image transmitting of row device, according to the live fire extinguishing situation that figure is passed, can 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, carries out oil tank and oil pipe fire extinguishing, and air to surface rocket fire extinguisher is placed
Ground, or roof is placed directly in, it is in combat readiness：Launch horn → correction magnetic compass, apart from the outer → inspection in 50 kilometers of original place
Battery, rocket projectile are that the connection → actuating remote control → air to air rocket fire extinguisher of high-efficiency fire-extinguishant takes off → fly to the scene of a fire → flight
Device hovers → adjusts emitter angle, or adjust automatically → startup emission switch → control system is connected to order → pass to electrode stake
Pass electric current → electrode stake propellant ignition → electromotor flame → promotion body of striking sparks → cause to go out transmitting tube → body and fly to the scene of a fire,
Body ruptures three kinds of approach；
（1）Run into tube inner wall → whole body crushing → extinguishing chemical to leak → stamp out a fire；
（2）Trigger action make body crush → anterior ignition charge pipe → body crushing → extinguishing chemical leaks → put out fire
Calamity；
（3）Electromotor work → light fuse cord → ignition charge pipe → body crushing → extinguishing chemical leak → put out fire
Calamity.Return → land → flame-out → → vanning is folded, it is in war preparedness position；
Embodiment 3
A kind of method of work of air-to-surface missile fire extinguisher, carries out height rescue, in scene of fire or earthquake-stricken area, has
When personnel are trapped in interior high level, high-rise building or mountain area complex area, when other equipment can not complete this task.Air to surface fire
Arrow fire extinguisher filling messenger is that kite string can complete this task, working procedure：Air to surface rocket fire extinguisher placement ground, or directly
Roof is placed on, locates combat readiness：
Launch horn → correction magnetic compass, apart from 50 kilometers of original place outer → inspection battery → repacking rocket projectile → vacate sky
Between, it is that launch hole → actuating put into by kite string → closing body → body to take out charge tube, extinguishing chemical, fuse cord → filling messenger
Remote control → take off → fly to scene → hovering → receipts rope target → adjustment emitter → startup emission switch → control system connects
To order → set out to electrode stake transmission electric current → electrode stake propellant ignition → electromotor flame → promotion body of striking sparks → cause
Penetrate that pipe → body flies to scene → run into wall or other obstacle → bodies fall or crush → take out that lead → being sued and laboured continues
Lead ends are connected to lead ends to ground → rescuer；
Rescuer fastens life line → retracted life line → fixed life line → quilt by rescuer by rescuer
Rescuer skids off → is rescued safely along life line；
Rescuer fastens descending lifeline → retracted descending lifeline → fixed descending lifeline → quilt by rescuer by rescuer
Rescuer is rescued → descending lifeline withdrawal, life line withdrawal → aircraft return → land → flame-out along descending lifeline landing → personnel
→ → vanning is folded, it is in war preparedness position.
Above-described embodiment can carry out recruitment evaluation, and aircraft carries video camera and working condition is shot with video-corder comprehensively,
Earth station receives the image transmitting of aircraft simultaneously.The live fire extinguishing situation passed according to figure can be passed back with scene photo and put capable fire extinguishing into
Recruitment evaluation, launching effect assessment.
Claims (8)
1. a kind of air-to-surface missile fire extinguisher, is characterized in that：Including：Multi-rotor aerocraft, rocket fire-extinguishing bullet, rocket launcher,
The multi-rotor aerocraft Lower mounting hole（8）By being connected with rocket launcher, rocket fire extinguishing in rocket launcher, is evenly equipped with
Bullet（15）.
2. a kind of air-to-surface missile fire extinguisher as claimed in claim 1, is characterized in that：The rocket launcher is by launcher
（11）, transmitting tube（12）, head（13）And actuator（14）Constitute, the launcher（11）For the transmitting tube for uniformly arranging
（12）Combination is constituted, launcher（11）Bottom is provided with undercarriage（17）.
3. a kind of air-to-surface missile fire extinguisher as claimed in claim 1, is characterized in that：The rocket fire-extinguishing bullet（15）By time delay
Trigger, body, charge tube, wire, fuse cord, rocket engine composition, structure that body is made for frangible plastic, charge tube
The structure made for plastics of shell, 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：The rocket engine（16）By outer
Shell, fuse cord hole, electrode stake, bocca, gunpowder composition, the structure that shell is made for woollen goods, shell are built-in with gunpowder.
5. a kind of air-to-surface missile fire extinguisher as claimed in claim 1, is characterized in that：The multi-rotor aerocraft includes：Machine
Disk（7）, machine cap（3）, horn（5）, propeller（4）, the machine disk（7）Be uniformly distributed on peripheries with horn（5）, horn（5）On put
There is motor cabinet（2）, motor cabinet（2）The motor of interior fixation（1）On be equipped with propeller（4）, the machine disk（7）Top be equipped with machine cap
（3）, machine cap（3）Battery is inside fixed with（9）, machine disk（7）It is built-in with flight control system（10）, flight control system（10）Signal end pass through
The wireless transceiver that holding wire is communicated with ground remote control device（6）It is connected, flight control system（10）Clutch end by wire with
Machine disk（7）The uniform motor of surrounding（1）It is connected, machine disk（7）Bottom be equipped with rocket launcher.
6. a kind of air-to-surface missile fire extinguisher as claimed in claim 5, is characterized in that：Described machine disk（7）For aluminium alloy material
Material structure, described machine disk 7 is folded piece structure with horn.
7. a kind of air-to-surface missile fire extinguisher as claimed in claim 5, is characterized in that：Described horn is integrated with motor cabinet
Carbon fibre material structure or engineering plastic structure, in the motor cabinet, fixed propeller on motor is carbon fibre material knot
Structure.
8. a kind of air-to-surface missile fire extinguisher as claimed in claim 5, is characterized in that：Described flight control system has：Automatic seeking
Look for burning things which may cause a fire disaster, detection attack distance, night vision, the function of aiming at, launching effect assessment transmission function；And have automatically and manually searching mesh
Mark and the function of transmitting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620635910.1U CN206007850U (en) | 2016-06-24 | 2016-06-24 | Air-to-surface missile fire extinguisher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620635910.1U CN206007850U (en) | 2016-06-24 | 2016-06-24 | Air-to-surface missile fire extinguisher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206007850U true CN206007850U (en) | 2017-03-15 |
Family
ID=58243695
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620635910.1U Expired - Fee Related CN206007850U (en) | 2016-06-24 | 2016-06-24 | Air-to-surface missile fire extinguisher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206007850U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105963882A (en) * | 2016-06-24 | 2016-09-28 | 河南沃野智能科技有限公司 | Air-to-surface rocket fire extinguisher and method |
| CN107021224A (en) * | 2017-04-28 | 2017-08-08 | 深圳市轻准科技有限公司 | Hang down and throw howitzer unmanned plane |
| CN107364578A (en) * | 2017-08-17 | 2017-11-21 | 顾瑶池 | A kind of tour unmanned plane for forest farm |
| CN108016618A (en) * | 2017-12-28 | 2018-05-11 | 深圳城际快机科技有限公司 | A kind of ammunition emitter and system |
-
2016
- 2016-06-24 CN CN201620635910.1U patent/CN206007850U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105963882A (en) * | 2016-06-24 | 2016-09-28 | 河南沃野智能科技有限公司 | Air-to-surface rocket fire extinguisher and method |
| CN105963882B (en) * | 2016-06-24 | 2022-03-04 | 河南沃野智能科技有限公司 | Air-to-ground rocket fire extinguisher and method |
| CN107021224A (en) * | 2017-04-28 | 2017-08-08 | 深圳市轻准科技有限公司 | Hang down and throw howitzer unmanned plane |
| CN107364578A (en) * | 2017-08-17 | 2017-11-21 | 顾瑶池 | A kind of tour unmanned plane for forest farm |
| CN107364578B (en) * | 2017-08-17 | 2019-01-25 | 顾瑶池 | A kind of tour unmanned plane for forest farm |
| CN108016618A (en) * | 2017-12-28 | 2018-05-11 | 深圳城际快机科技有限公司 | A kind of ammunition emitter and system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170315 Termination date: 20170624 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |