CN104897003A - Fire-extinguishing bomb launcher - Google Patents
Fire-extinguishing bomb launcher Download PDFInfo
- Publication number
- CN104897003A CN104897003A CN201510304872.1A CN201510304872A CN104897003A CN 104897003 A CN104897003 A CN 104897003A CN 201510304872 A CN201510304872 A CN 201510304872A CN 104897003 A CN104897003 A CN 104897003A
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- China
- Prior art keywords
- gas
- carrier
- fire
- fire extinguishing
- launching device
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Abstract
The invention discloses a fire-extinguishing bomb launcher. The fire-extinguishing bomb launcher comprises a gas bottle, a gas pressure throttling valve, a gas bin, a camera device, a positioning device, a bearing rack, a control module and at least one fire-extinguishing bomb holder, wherein the gas bottle is communicated with the gas bin through a pipeline, the gas pressure throttling valve is mounted on the pipeline, the gas bin is communicated with each fire-extinguishing bomb holder, the camera device and the positioning device are disposed at the launching ends of the fire-extinguishing bomb holders, the gas bottle, the gas bin and the fire-extinguishing bomb holders are mounted on the bearing rack, and the gas pressure throttling valve, the camera device, the positioning device and the fire-extinguishing bomb holders are connected with the control module. During use, the gas pressure throttling valve is used to control the pressure of gas flowing out of the gas bottle, the gas bin stores the gas, the camera device monitors in real time, and the positioning device position a to-be-extinguished part. Compared with a traditional launcher, the launcher is small in size, accurate in launching position, simple to operate, safe and practical and fast in reaction.
Description
Technical field
The present invention relates to fire extinguisher bomb lift-off technology field, more particularly, particularly a kind of fire extinguishing bullet launching device.
Background technology
Traditional fire extinguishing bullet launching device uses support that gun barrel is supported transmitting, or the mode that gun barrel is shouldered similar rocket launcher piggyback by user of service is launched, but existing fire extinguishing bullet launching device fire accuracy is inaccurate, reaction speed slow, and fire-fighting efficiency is low.
Summary of the invention
The object of the present invention is to provide the fire extinguishing bullet launching device that a kind of transmitting site is accurate high, simple to operate, response speed is fast.
In order to achieve the above object, the technical solution used in the present invention is as follows:
A kind of fire extinguishing bullet launching device, comprise gas bullet bottle, air pressure choke valve, gas cabin, camera head, positioner, carrier, control module and at least one shoot folder, described gas bullet bottle is communicated with gas cabin by pipeline, described air pressure choke valve is arranged on pipeline, described gas cabin is communicated with shooting to press from both sides, the transmitting terminal shooting folder is located at by described camera head and positioner, and described gas bullet bottle, gas cabin and shoot folder and be installed on carrier, described air pressure choke valve, camera head, positioner with shoot folder and be all connected with control module.
Preferably, described positioner is laser orientation instru-ment.
Preferably, described camera head is minisize pick-up head.
Preferably, also comprise the aircraft for installing described carrier, this aircraft comprises main support, four travel(l)ing rests, four rotating power source and two fixed supports, described main support is fixedly connected with carrier, four described travel(l)ing rests are movably arranged on four corners of main support, two described fixed support symmetries are arranged on the both sides of main support, and four described rotating power source are all connected with control module.
Preferably, described gas bullet bottle is positioned at the side of carrier with shooting folder, the described gentle cabin of air pressure choke valve is positioned at the opposite side of carrier.
Preferably, the dismountable inner side being installed on main support of described carrier.
Compared with prior art, the invention has the advantages that: the present invention in use, adopt the air pressure of eluting gas in air pressure throttle valve control gas bullet bottle, stored by gas cabin again, camera head wherein can carry out real-time monitoring, and positioner can be real-time treat fire extinguishing position position, there is the advantage that volume is little, transmitting site is accurate, simple to operate, safe and practical and reaction speed is fast for traditional emitter.
Accompanying drawing explanation
In order to be illustrated more clearly in the embodiment of the present invention or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the structural representation of fire extinguishing bullet launching device of the present invention.
Fig. 2 is the structural representation that fire extinguishing bullet launching device of the present invention and main support are installed.
Description of reference numerals: 1, gas bullet bottle, 2, air pressure choke valve, 3, gas cabin, 4, camera head, 5, positioner, 6, shoot folder, 7, carrier, 8, pipeline, 9, main support, 10, travel(l)ing rest, 11, rotating power source, 12, fixed support.
Detailed description of the invention
Below in conjunction with accompanying drawing, the preferred embodiments of the present invention are described in detail, can be easier to make advantages and features of the invention be readily appreciated by one skilled in the art, thus more explicit defining is made to protection scope of the present invention.
Consult shown in Fig. 1, the invention provides a kind of fire extinguishing bullet launching device, comprise gas bullet bottle 1, air pressure choke valve 2, gas cabin 3, camera head 4, positioner 5, carrier 7, control module shoots folder 6 with at least one, described gas bullet bottle 1 is communicated with gas cabin 3 by pipeline 8, described air pressure choke valve 2 is arranged on pipeline 8, described gas cabin 3 with shoot folder 6 and be communicated with, the transmitting terminal shooting folder 6 is located at by described camera head 4 and positioner 5, and described gas bullet bottle 1, gas cabin 3 and shoot folder 6 and be installed on carrier 7, described air pressure choke valve 2, camera head 4, positioner 5 with shoot folder 6 and be all connected with control module.
In the present invention, described positioner 5 is preferably laser orientation instru-ment, and it also can adopt other position indicator.
In the present invention, described camera head 4 is minisize pick-up head, and it also can adopt camera etc.
Consult shown in Fig. 2, in order to make this emitter can to putting out a fire Anywhere, the present invention also comprises the aircraft (as unmanned plane) for installing described carrier 7, this emitter can be brought to any position by aircraft.And, this aircraft comprises main support 9, four travel(l)ing rests 10, four rotating power source 11 and two fixed supports 12, described main support 9 is fixedly connected with carrier 7, four described travel(l)ing rests 10 are movably arranged on four corners of main support 9, two described fixed support 12 symmetries are arranged on the both sides of main support 9, and four described rotating power source 11 are all connected with control module.
In order to save installing space, gas bullet bottle described in the present invention 1 and shoot the side that folder 6 is positioned at carrier 7, the described gentle cabin of air pressure choke valve 2 is positioned at the opposite side of carrier 7.
For the ease of dismounting, the dismountable inner side being installed on main support 9 of the carrier 7 described in the present invention.
The direction of the present invention by aircraft (unmanned plane) preposition camera head shooting input fire extinguisher bomb and height, the angle of the also required flight of calculating aircraft, given an order by control module and carry out igniting transmitting.Specifically in use, air pressure choke valve 2 is adopted to control the air pressure of eluting gas in gas bullet bottle 1, stored by gas cabin 3 again, control by control module the fire extinguisher bomb shot in folder 6 to launch, camera head 4 wherein can carry out real-time monitoring, and positioner 5 can be real-time treat fire extinguishing position position, there is the advantage that volume is little, transmitting site is accurate, simple to operate, safe and practical and reaction speed is fast for traditional emitter.
Although describe embodiments of the present invention by reference to the accompanying drawings; but patent owner can make various distortion or amendment within the scope of the appended claims; as long as be no more than the protection domain described by claim of the present invention, all should within protection scope of the present invention.
Claims (6)
1. a fire extinguishing bullet launching device, it is characterized in that: comprise gas bullet bottle (1), air pressure choke valve (2), gas cabin (3), camera head (4), positioner (5), carrier (7), control module shoots folder (6) with at least one, described gas bullet bottle (1) is communicated with gas cabin (3) by pipeline (8), described air pressure choke valve (2) is arranged on pipeline (8), described gas cabin (3) is pressed from both sides (6) and is communicated with shooting, the transmitting terminal shooting folder (6) is located at by described camera head (4) and positioner (5), and described gas bullet bottle (1), gas cabin (3) and shoot folder (6) and be installed on carrier (7), described air pressure choke valve (2), camera head (4), positioner (5) with shoot folder (6) and be all connected with control module.
2. fire extinguishing bullet launching device according to claim 1, is characterized in that: described positioner (5) is laser orientation instru-ment.
3. fire extinguishing bullet launching device according to claim 1, is characterized in that: described camera head (4) is minisize pick-up head.
4. the fire extinguishing bullet launching device according to claim 1 or 2 or 3, it is characterized in that: also comprise the aircraft for installing described carrier (7), this aircraft comprises main support (9), four travel(l)ing rests (10), four rotating power source (11) and two fixed supports (12), described main support (9) is fixedly connected with carrier (7), four described travel(l)ing rests (10) are movably arranged on four corners of main support (9), two described fixed support (12) symmetries are arranged on the both sides of main support (9), four described rotating power source (11) are all connected with control module.
5. fire extinguishing bullet launching device according to claim 1, it is characterized in that: described gas bullet bottle (1) and shoot the side that folder (6) is positioned at carrier (7), the gentle cabin of described air pressure choke valve (2) is positioned at the opposite side of carrier (7).
6. fire extinguishing bullet launching device according to claim 1, is characterized in that: the dismountable inner side being installed on main support (9) of described carrier (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510304872.1A CN104897003A (en) | 2015-06-04 | 2015-06-04 | Fire-extinguishing bomb launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510304872.1A CN104897003A (en) | 2015-06-04 | 2015-06-04 | Fire-extinguishing bomb launcher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104897003A true CN104897003A (en) | 2015-09-09 |
Family
ID=54029819
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510304872.1A Pending CN104897003A (en) | 2015-06-04 | 2015-06-04 | Fire-extinguishing bomb launcher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104897003A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107115610A (en) * | 2017-06-09 | 2017-09-01 | 娄文忠 | The fire extinguisher bomb jettison system and its method of jettisoninging of a kind of individual equipment |
| CN107137845A (en) * | 2017-06-09 | 2017-09-08 | 娄文忠 | A kind of integral type fire extinguisher bomb jettison system of individual equipment and method of jettisoninging |
| CN108609195A (en) * | 2018-05-30 | 2018-10-02 | 深圳市易飞方达科技有限公司 | A kind of folding wings unmanned plane emitter |
Citations (6)
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|---|---|---|---|---|
| CN2848267Y (en) * | 2005-11-09 | 2006-12-20 | 岳全生 | Support type pneumatic extinguishing gun |
| CN201145522Y (en) * | 2008-01-22 | 2008-11-05 | 陈尊山 | Compressed-air transmitting apparatus |
| CN201262536Y (en) * | 2008-04-09 | 2009-06-24 | 王昕� | Fire-extinguishing bullet for gun and its emitter |
| CN102935274A (en) * | 2012-11-16 | 2013-02-20 | 青岛科而泰环境控制技术有限公司 | Liquid projection bomb, projecting device and delivery method thereof |
| CN203777555U (en) * | 2014-04-01 | 2014-08-20 | 刘书俊 | Efficient casting type extinguishing device |
| CN203989588U (en) * | 2014-08-21 | 2014-12-10 | 国家电网公司 | The helicopter that a kind of transmission line forest fire of putting out a fire to save life and property is used carries high-pressure water-saving extinguishing water cannon |
-
2015
- 2015-06-04 CN CN201510304872.1A patent/CN104897003A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2848267Y (en) * | 2005-11-09 | 2006-12-20 | 岳全生 | Support type pneumatic extinguishing gun |
| CN201145522Y (en) * | 2008-01-22 | 2008-11-05 | 陈尊山 | Compressed-air transmitting apparatus |
| CN201262536Y (en) * | 2008-04-09 | 2009-06-24 | 王昕� | Fire-extinguishing bullet for gun and its emitter |
| CN102935274A (en) * | 2012-11-16 | 2013-02-20 | 青岛科而泰环境控制技术有限公司 | Liquid projection bomb, projecting device and delivery method thereof |
| CN203777555U (en) * | 2014-04-01 | 2014-08-20 | 刘书俊 | Efficient casting type extinguishing device |
| CN203989588U (en) * | 2014-08-21 | 2014-12-10 | 国家电网公司 | The helicopter that a kind of transmission line forest fire of putting out a fire to save life and property is used carries high-pressure water-saving extinguishing water cannon |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107115610A (en) * | 2017-06-09 | 2017-09-01 | 娄文忠 | The fire extinguisher bomb jettison system and its method of jettisoninging of a kind of individual equipment |
| CN107137845A (en) * | 2017-06-09 | 2017-09-08 | 娄文忠 | A kind of integral type fire extinguisher bomb jettison system of individual equipment and method of jettisoninging |
| CN107115610B (en) * | 2017-06-09 | 2019-08-30 | 娄文忠 | A kind of fire extinguisher bomb jettison system of individual equipment and its method of jettisoninging |
| CN107137845B (en) * | 2017-06-09 | 2019-09-17 | 娄文忠 | A kind of integral type fire extinguisher bomb jettison system of individual equipment and method of jettisoninging |
| CN108609195A (en) * | 2018-05-30 | 2018-10-02 | 深圳市易飞方达科技有限公司 | A kind of folding wings unmanned plane emitter |
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Application publication date: 20150909 |
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| RJ01 | Rejection of invention patent application after publication |